command: 
 /usr/local/libexec/code_saturne/cs_solver --param VPR-G000-R000-S000.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 4.0.0


  Copyright (C) 1998-2015 EDF S.A., France

  revision 4.0.0
  build Thu 28 May 2015 10:25:02 PM MSK
  MPI version 2.1 (Open MPI 1.4.3)


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

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

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


Local case configuration:

  Date:                Tue 30 Jun 2015 11:55:27 PM MSK
  System:              Linux 3.13.0-55-generic
  Machine:             AntechPC
  Processor:           model name	: Intel(R) Core(TM) i7-2600K CPU @ 3.40GHz
  Memory:              15965 MB
  User:                antech (Antech)
  Directory:           /home/antech/CodeSaturne/Bundle/RESU/20150630-2355
  MPI ranks:           4 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

 Reading metadata from file: "mesh_input"

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

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


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



@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@
@ @@ WARNING:       IN THE DATA SPECIFICATION
@    ========
@
@  The k-omega turbulence model has been chosen. In order to
@    have a correct calculation restart, the ICDPAR indicator
@    has been set to 1 (read the wall distance in the restart
@    file).
@  If this initialization raises any issue (modification of,
@    the number and position of the wall faces since the
@    previous calcuation), force ICDPAR=1 (there might be,
@    a small shift in the turbulent viscosity at the,
@    first time-step).,
@
@  The calculation will be run.
@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@


 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 )
       NPROCE =              6 (Nb cell properties          )


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


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

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

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

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

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

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

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


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

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


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


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

   - Commons
       ITHERM =              1 (0: no thermal model         )
                               (1: temperature              )
                               (2: enthalpy                 )
                               (3: total energy             )
       ITPSCL =              2 (0: none                     )
                               (1: temperature in Kelvin    )
                               (2: temperature in Celsius   )
       ISCALT =              1 (Thermal scalar number       )


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

 --- Continuous phase:

   - Commons
       ITURB  =             60 (Turbulence model            )
       IDEUCH =              1 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - k-omega SST         (ITURB = 60)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )
       RELAXV =    0.10000E+01 for k      (Relaxation)
       RELAXV =    0.10000E+01 for omega  (Relaxation)

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

 --- Constants

   - Commons
       XKAPPA =    0.42000E+00 (Von Karman constant         )
       CSTLOG =    0.52000E+01 (U+=Log(y+)/kappa +CSTLOG    )
       APOW   =    0.83000E+01 (U+=APOW (y+)**BPOW (W&W law))
       BPOW   =    0.14286E+00 (U+=APOW (y+)**BPOW (W&W law))

   - k-omega SST         (ITURB = 60)
       CKWSK1 =    0.11765E+01 (sigma_k1 constant           )
       CKWSK2 =    0.10000E+01 (sigma_k2 constant           )
       CKWSW1 =    0.20000E+01 (sigma_omega1 constant       )
       CKWSW2 =    0.11682E+01 (sigma_omega2 constant       )
       CKWBT1 =    0.75000E-01 (beta1 constant              )
       CKWBT2 =    0.82800E-01 (beta2 constant              )
       CKWGM1 =    0.53933E+00 (gamma1 constant             )
       CKWGM2 =    0.41667E+00 (gamma2 constant             )
       CKWA1  =    0.31000E+00 (a1 constant to compute mu_t )
       CKWC1  =    0.10000E+02 (c1 const. for prod. limiter )
       CMU    =    0.90000E-01 (Cmu (or Beta*) constant for )
                                    omega/epsilon conversion)


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.10000E-04 (Minimum time step           )
       DTMAX  =    0.10000E+00 (Maximum time step           )
       DTREF  =    0.10000E-03 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

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

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

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

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


 ** CONVECTION - DIFFUSION
    ----------------------

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Velocity              1      1      1      1      0 0.10E+01 0.10E+01
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 k                     1      1      1      1      0 0.00E+00 0.10E+01
 omega                 1      1      1      1      0 0.00E+00 0.10E+01
 TempC                 1      1      1      1      0 0.10E+01 0.10E+01
-------------------------------------------------------------

       ICONV  =  0 ou  1       (1 for convection active     )
       IDIFF  =  0 ou  1       (1 for total diffusion active)
       IDIFFT =  0 ou  1       (1 for turbulent diff. active)
       ISCHCV =  0 ou  1       (SOLU or CD                  )
       ISSTPC =  0 ou  1       (1: no slope test            )
       BLENCV =  [0.;1.]       (1-upwind proportion         )
       THETAV =  [0.;1.]       (0.5 Crank-Nicolson/AB       )
                               (theta for convection-       )
                               (diffusion terms uses        )
                               ((1-theta).old+theta.new     )


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


 ** STOKES
    ------
       IDILAT =              1 (1 : without unsteady term
                                    in the continuity equation
                                2 : with unsteady term in 
                                    the continuity equation)
       IPOROS =              0 (0 : without porous media
                                1 : with porous media)
       IPHYDR =              0 (1: account for explicit
                                   balance between pressure
                                   gradient, gravity source
                                   terms, and head losses     )
       ICALHY =              0 (1: compute hydrastatic
                                   pressure for Dirichlet
                                   conditions for pressure
                                   on outlet                  )
       IPRCO  =              1 (1: pressure-continuity        )
       IPUCOU =              0 (1: reinforced U-P coupling    )
       NTERUP =              1 (n: n sweeps on navsto for
                                   velocity/pressure coupling )

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

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

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


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


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

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

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Velocity            100      1  0.1000E-04  0.1000E-03  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-03  0.0000E+00
 k                   100      1  0.1000E-04  0.1000E-03  0.0000E+00
 omega               100      1  0.1000E-04  0.1000E-06  0.0000E+00
 TempC               100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Velocity              1     -1  0.1500E+01
 Pressure              1     -1  0.1500E+01
 k                     1     -1  0.1500E+01
 omega                 1     -1  0.1500E+01
 TempC                 1     -1  0.1500E+01
-----------------------------------

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


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


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


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


 ** 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-07      1
 TempC             0.1000E-07      1
------------------------------------

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


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


 ** SCALARS
    -------

       ITBRRB =              0 (T or H reconstruction at bdy)

-------------------------------------------------------------
 Variable         Number ISCACP ITURT      VISLS0      SIGMAS
-------------------------------------------------------------
 TempC                 1      1      0  0.2495E-01  0.1000E+01
---------------------------------------------------------------------

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

-------------------------------------------------------
 Variable         Number ICLVFL      SCAMIN      SCAMAX
-------------------------------------------------------
 TempC                 1     -1 -0.1000E+13  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 =              1 (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 )

 --- Post-processed variables


Velocity
Pressure
k
omega
TempC
Density
Boundary Density
TurbVisc
CourantNb
FourierNb
total_pressure
         --           --

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

       Number Name                  Nb. probes (-1: all)
         2 Velocity[X]                   -1
         3 Velocity[Y]                   -1
         4 Velocity[Z]                   -1
         5 Pressure                      -1
         6 k                             -1
         7 omega                         -1
         8 TempC                         -1
         9 Density                       -1
        10 LamVisc                       -1
        11 TurbVisc                      -1
        12 CourantNb                     -1
        13 FourierNb                     -1
        14 total_pressure                -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 k                              0
         7 omega                          0
         8 TempC                          0
         9 Density                     -999
        11 TurbVisc                    -999
        12 CourantNb                   -999
        13 FourierNb                   -999
        14 total_pressure              -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              1 (Force exerted by the
                                     fluid on the boundary)
       ipstft =              1 (Thermal flux   at boundary)
       ipsttb =              1 (Temperature    at boundary)
       ipstnu =              0 (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


 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):
    [     464386 ;     464386 ] =          4

 Partitioning finished (16.6 s)


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

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

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

 Histogram of the number of cells per rank:

    minimum value =             464386
    maximum value =             464386

      1 : [     464386 ;     464386 ] =          4

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

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

    minimum value =             488731
    maximum value =             510416

      1 : [     488731 ;     493068 [ =          2
      2 : [     493068 ;     497405 [ =          0
      3 : [     497405 ;     501742 [ =          0
      4 : [     501742 ;     506079 [ =          0
      5 : [     506079 ;     510416 ] =          2

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

 Histogram of the number of ghost cells per rank:

    minimum value =              24345
    maximum value =              46030

      1 : [      24345 ;      28682 [ =          2
      2 : [      28682 ;      33019 [ =          0
      3 : [      33019 ;      37356 [ =          0
      4 : [      37356 ;      41693 [ =          0
      5 : [      41693 ;      46030 ] =          2

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

 Histogram of the number of interior faces per rank:

    minimum value =             878026
    maximum value =             920528

      1 : [     878026 ;     886526 [ =          1
      2 : [     886526 ;     895026 [ =          0
      3 : [     895026 ;     903527 [ =          1
      4 : [     903527 ;     912027 [ =          0
      5 : [     912027 ;     920528 ] =          2

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

 Histogram of the number of boundary faces per rank:

    minimum value =              48519
    maximum value =             136182

      1 : [      48519 ;      66051 [ =          1
      2 : [      66051 ;      83584 [ =          0
      3 : [      83584 ;     101116 [ =          1
      4 : [     101116 ;     118649 [ =          1
      5 : [     118649 ;     136182 ] =          1

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

 Histogram of the number of interior faces per cell:

    minimum value =                  1
    maximum value =                  4

      1 : [          1 ;          2 [ =         26
      2 : [          2 ;          3 [ =      11751
      3 : [          3 ;          4 ] =    1845767

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

 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

 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 =             486203
    maximum value =             508698

      1 : [     486203 ;     490702 [ =          2
      2 : [     490702 ;     495201 [ =          0
      3 : [     495201 ;     499700 [ =          0
      4 : [     499700 ;     504199 [ =          0
      5 : [     504199 ;     508698 ] =          2

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =             247531
    maximum value =             252364

      1 : [     247531 ;     248497 [ =          1
      2 : [     248497 ;     249464 [ =          0
      3 : [     249464 ;     250430 [ =          0
      4 : [     250430 ;     251397 [ =          1
      5 : [     251397 ;     252364 ] =          2

 Mesh coordinates:               minimum    and maximum
                       X : -1.1400000e+00  3.0000000e-01
                       Y : -1.9250000e-03  1.7325000e-02
                       Z : -5.5000000e-02  1.3500000e-01
 Mesh
     Number of cells:          1857544
     Number of interior faces: 3524036
     Number of boundary faces: 382104
     Number of vertices:       409688

 Groups:
    "Group_Of_All_Faces"
       boundary faces:       382104
    "Group_Of_All_Volumes"
       cells:               1857544
    "Inlet"
       boundary faces:          876
    "Outlet"
       boundary faces:         1874
    "SideBottom"
       boundary faces:        73223
    "SideLeft"
       boundary faces:         6722
    "SideRight"
       boundary faces:         7714
    "SideTop"
       boundary faces:        73389

 --- Information on the volumes
       Minimum control volume      =  7.1663409e-11
       Maximum control volume      =  1.6571738e-08
       Total volume for the domain =  5.0099010e-03

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

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 367 -->   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 (1.27 s)
                                                             
       ALMAX  =    0.17141E+00 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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

   ** READING MAIN AND AUXILIARY RESTART FILES
      ----------------------------------------


      READING THE MAIN RESTART FILE

 Start reading

  Warning: the number of variables or properties has been changed
           relative to the restart file.

  current:  5 model and 0 user variables
            13 model and 0 user properties
  previous: 4 model and 0 user variables
            11 model and 0 user properties

  The computation continues, with a partial restart.
 Reading dimensions complete
  Reading the previous time step number (restarting computation)  NTPABS =           23
  Reading the previous time step number (restarting computation)  TTPABS =   0.2300E-03
 Reading options complete
  restart/main: section "temperature::vals::0" not present.

  Warning: the following variables could not be found or read
           in restart file "restart/main", so default initializations
           will be used:

  TempC

  Read variables from restart: restart/main
 Reading complete

         READING THE AUXILIARY RESTART FILE             

 Start reading                                          
   Fin de la lecture des options                        

   Apdatation of the reference point for the total pressure  
       by reading the restart file                           
    XYZP0 =    0.30000E+00   0.76367E-03   0.19364E-01

  restart/auxiliary: section "density::vals::0" not present.
  restart/auxiliary: section "boundary_density::vals::0" not present.
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: WHEN READING THE AUXILIARY RESTART FILE        
@    =======                                                 
@      Lecture des proprietes physiques                      
@                                                            
@    It was not possible to read some values from the        
@      auxiliary restart file.                               
@    They will be initialized by the default values.         
@                                                            
@     This situation can occur when the restart file         
@      originates from a run realised with different         
@      options or when the file is damaged.                  
@                                                            
@    The run will continue...                                
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

   Fin de la lecture des proprietes physiques           
   Fin de la lecture du pas de temps                    
   Fin de la lecture des flux de masse                  
  restart/auxiliary: section "temperature::bc_coeffs::a" not present.
  restart/auxiliary: section "temperature::bc_coeffs::b" not present.
  restart/auxiliary: section "temperature::bc_coeffs::af" not present.
  restart/auxiliary: section "temperature::bc_coeffs::bf" not present.


Code_Saturne: ../../../code_saturne-4.0.0/src/base/cs_restart_default.c:2229: Warning

Some boundary condition coefficients could not be read from a restart file;
they will be initialized with default values.

   Fin de la lecture des conditions aux limites         
  restart/auxiliary: section "time_moments:sizes" not present.
  restart/auxiliary: section "nombre_moyennes_temps" not present.
   Fin de la lecture de la distance a la paroi          
 End reading                                            

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


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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity         -0.3368E+01  0.3951E+02
  Velocity         -0.8406E+01  0.1087E+02
  Velocity         -0.1822E+02  0.1891E+02
  Pressure         -0.1090E+04  0.9825E+03
  k                 0.5812E-07  0.7636E+00
  omega             0.8252E-01  0.3670E+06
  TempC             0.0000E+00  0.0000E+00
 ---------------------------------

                dt  0.1000E-03  0.1000E-03
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.330000000E-03   TIME STEP NUMBER              24
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1293E+01  0.1293E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.3037E-11  0.6998E-03
 -----------------------------------------

 --- Diffusivity:
 -----------------------------------------------
 Scalar           Number  Min. value  Max. value
 -----------------------------------------------
 TempC                 1  0.2495E-01  0.2495E-01
 -----------------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         876
Smooth wall               5      225028
Rough wall                6           0
Symmetry                  4      154326
Free outlet               3        1874
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.403060048E-01
Smooth wall               5      225028        -0.411282051E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.403016032E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12315E+03 0.20417E+01
   Friction velocity        uet   :  0.23154E-01 0.39239E+01
   Friction velocity        uk    :  0.22929E-01 0.15791E+01
   Dimensionless distance   yplus :  0.42625E+00 0.30111E+02
   Friction thermal sca.    tstar : -0.65120E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31803E+00 0.12065E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     223007
   Nb of faces within the viscous sub-layer     :        200
   Total number of wall faces                   :     225028
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56403E+00      32   0.41540E-01   0.56188E+04 0.74190E+03 
c  Velocity[X]                                      0.25731E+04 
c  Velocity[Y]                                      0.17014E+04 
c  Velocity[Z]                                      0.13444E+04 
c  Pressure     0.11641E-01     306   0.32350E-01   0.21325E+01 0.50306E+03 
c  k            0.20540E-02      30   0.44619E-03   0.36645E+00 0.23831E+04 
c  omega        0.68666E+03      49   0.42341E-04   0.11623E+11 0.88299E+03 
c  TempC        0.83797E+03      75   0.30633E+00   0.62334E+06 0.10000E+05 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.9522          55.276          10.332          9.8223
v  Velocity[Y]            -20.863          16.707     -0.00017687       0.0023008
v  Velocity[Z]            -21.948          22.522       -0.070512       -0.039535
v  ǁVelocityǁ             0.02915          55.409           10.69          9.9256
v  Pressure               -1064.7          1074.3          847.94          897.59
v  k                   1.0878e-08         0.84771       0.0079809       0.0035349
v  omega                  0.14228      3.9511e+05           13878          5277.5
v  TempC                  -67.952          309.06         0.56449         0.38417
v  Density                  1.293           1.293           1.293           1.293
v  TurbVisc            3.0375e-12      0.00069978      5.0816e-06       7.718e-06
v  CourantNb                    0          21.772           1.707          1.1785
v  FourierNb            0.0024507         0.29168        0.013263       0.0087455
v  total_pressure      1.0026e+05       1.024e+05      1.0217e+05      1.0222e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density           1.293           1.293           1.293           1.293


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013774          21.874          1.7203          1.1872


 TIME FOR THE TIME STEP               24:        0.78731E+02

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


 INSTANT    0.430000000E-03   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.442175291E-01
Smooth wall               5      225028        -0.472854548E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.442205377E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12479E+03 0.12717E+01
   Friction velocity        uet   :  0.27217E-01 0.42580E+01
   Friction velocity        uk    :  0.36806E-01 0.16001E+01
   Dimensionless distance   yplus :  0.77247E+00 0.30418E+02
   Friction thermal sca.    tstar : -0.34478E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57635E+00 0.12089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     222765
   Nb of faces within the viscous sub-layer     :        220
   Total number of wall faces                   :     225028
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56158E+00      40   0.53142E-01   0.23733E+06 0.92625E+04 
c  Velocity[X]                                      0.23151E+06 
c  Velocity[Y]                                      0.55142E+03 
c  Velocity[Z]                                      0.52660E+04 
c  Pressure     0.23682E-02    2699   0.26239E+00   0.62486E+00 0.10150E+05 
c  k            0.14098E-02      20   0.43740E-03   0.18913E+00 0.15121E+04 
c  omega        0.62466E+03      32   0.95945E-04   0.27718E+11 0.14457E+04 
c  TempC        0.69289E+03      49   0.21339E+00   0.28179E+06 0.41081E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.0773          40.598          5.3228          5.0919
v  Velocity[Y]            -11.955          16.088      0.00050979       0.0027475
v  Velocity[Z]            -18.883          19.114       -0.038839        -0.02064
v  ǁVelocityǁ            0.035907          40.718          5.5309          5.1521
v  Pressure                -91823          893.55          -39777          -50750
v  k                   1.5668e-07          1.2098       0.0097152       0.0039588
v  omega                 0.098141      4.7035e+05           13396          4986.9
v  TempC                  -90.049          443.18          1.0405         0.68345
v  Density                0.60662          1.7212           1.291          1.2918
v  TurbVisc            1.2111e-12      0.00074462      5.1277e-06       7.794e-06
v  CourantNb                    0           26.48          1.8827           1.295
v  FourierNb             0.002466         0.71845        0.013397        0.008845
v  total_pressure          9501.7      1.0222e+05           61548           50575

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.60662          1.7212          1.2838          1.2866


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01422          26.529          1.8961          1.3038


 TIME FOR THE TIME STEP               25:        0.23882E+03

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


 INSTANT    0.530000000E-03   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.227505612E-01
Smooth wall               5      225028        -0.668519801E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.227377149E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71650E+02 0.12911E+01
   Friction velocity        uet   :  0.24877E-02 0.30976E+01
   Friction velocity        uk    :  0.21813E-01 0.11752E+01
   Dimensionless distance   yplus :  0.44927E+00 0.22318E+02
   Friction thermal sca.    tstar : -0.59244E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33520E+00 0.11352E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     209058
   Nb of faces within the viscous sub-layer     :       1398
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41897E-01      39   0.27502E+00   0.13719E+05 0.28359E+04 
c  Velocity[X]                                      0.13068E+05 
c  Velocity[Y]                                      0.14634E+03 
c  Velocity[Z]                                      0.50433E+03 
c  Pressure     0.23672E-02    2684   0.27162E+00   0.86936E+00 0.33800E+05 
c  k            0.13221E-02      20   0.35712E-03   0.28963E+00 0.16489E+04 
c  omega        0.51189E+03      34   0.13518E-03   0.38876E+11 0.20150E+04 
c  TempC        0.66839E+03      48   0.16271E+00   0.18511E+06 0.25848E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.3937          44.223          4.1648          3.9863
v  Velocity[Y]            -11.996          17.552       0.0004086       0.0019711
v  Velocity[Z]            -22.383          23.011       -0.031362       -0.016638
v  ǁVelocityǁ            0.027552           44.23           4.341          4.0358
v  Pressure                -21157          909.16         -8935.7          -11513
v  k                    1.252e-06          1.1481       0.0088341        0.004111
v  omega                 0.071498      3.2851e+05           11467          4489.3
v  TempC                   -89.77          506.76          1.4636         0.94797
v  Density                0.49304          1.9289          1.2895          1.2912
v  TurbVisc            1.2351e-11      0.00027992       2.173e-06      3.0873e-06
v  CourantNb                    0          18.429         0.97056         0.66798
v  FourierNb            0.0024684          0.3248        0.012582       0.0074969
v  total_pressure           80168      1.0223e+05           92389           89812

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.49304          1.9289          1.2761           1.283


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014651          18.487         0.98315         0.67548


 TIME FOR THE TIME STEP               26:        0.23758E+03

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


 INSTANT    0.630000000E-03   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.180125963E-01
Smooth wall               5      225028        -0.126678540E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.180221864E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.92123E+02 0.18535E+01
   Friction velocity        uet   :  0.74018E-02 0.38016E+01
   Friction velocity        uk    :  0.17139E-01 0.13206E+01
   Dimensionless distance   yplus :  0.43550E+00 0.21523E+02
   Friction thermal sca.    tstar : -0.59684E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32493E+00 0.11266E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     203513
   Nb of faces within the viscous sub-layer     :       1928
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        289 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16549E+00      30   0.42479E-01   0.17063E+04 0.10992E+04 
c  Velocity[X]                                      0.15535E+04 
c  Velocity[Y]                                      0.47540E+02 
c  Velocity[Z]                                      0.10521E+03 
c  Pressure     0.15979E-02    2429   0.92597E-01   0.81891E+00 0.23345E+05 
c  k            0.13518E-02      20   0.41356E-03   0.30598E+00 0.14913E+04 
c  omega        0.42539E+03      37   0.12055E-03   0.20441E+11 0.16788E+04 
c  TempC        0.68232E+03      50   0.15589E+00   0.15449E+06 0.20079E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.556          48.019          3.7832          3.6155
v  Velocity[Y]            -13.679          20.515      0.00085678       0.0020687
v  Velocity[Z]            -23.957          27.311       -0.030284        -0.01558
v  ǁVelocityǁ            0.023875          48.024          3.9504          3.6617
v  Pressure               -6603.7          850.68         -2483.7           -3341
v  k                   6.8491e-07          1.1415       0.0082955       0.0043232
v  omega                  0.17053      4.5816e+05          9989.9          4080.4
v  TempC                  -114.01          516.77          1.8868          1.1994
v  Density                0.45285           1.926          1.2881          1.2906
v  TurbVisc            2.0975e-11      0.00046398      2.6234e-06      3.7726e-06
v  CourantNb                    0          25.512         0.77077         0.53044
v  FourierNb            0.0024668         0.55076        0.012805       0.0077344
v  total_pressure           94721      1.0218e+05           98841           97984

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.45285           1.926          1.2707          1.2805


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01507          25.566         0.78358         0.53817


 TIME FOR THE TIME STEP               27:        0.21960E+03

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


 INSTANT    0.730000000E-03   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.162446264E-01
Smooth wall               5      225028         0.235603050E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.162512371E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10100E+03 0.19816E+01
   Friction velocity        uet   :  0.12614E-01 0.40223E+01
   Friction velocity        uk    :  0.23350E-01 0.13664E+01
   Dimensionless distance   yplus :  0.40038E+00 0.22208E+02
   Friction thermal sca.    tstar : -0.61235E+03 0.74011E+01
   Rough dim-less th. sca.  tplus :  0.29873E+00 0.11340E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     200315
   Nb of faces within the viscous sub-layer     :       2186
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        448 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18550E+00      28   0.30473E-01   0.23434E+03 0.41624E+03 
c  Velocity[X]                                      0.17181E+03 
c  Velocity[Y]                                      0.23506E+02 
c  Velocity[Z]                                      0.39026E+02 
c  Pressure     0.11598E-02    2031   0.50437E-01   0.78141E+00 0.67263E+05 
c  k            0.14312E-02      21   0.18153E-02   0.34399E+00 0.14070E+04 
c  omega        0.36940E+03      38   0.28643E-03   0.11066E+11 0.13865E+04 
c  TempC        0.72325E+03      49   0.12911E+00   0.14234E+06 0.17174E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -52.359          49.211          3.6985          3.5321
v  Velocity[Y]            -15.601           21.31       0.0011204       0.0020564
v  Velocity[Z]            -25.171          27.406        -0.03117       -0.015867
v  ǁVelocityǁ            0.032099          53.281           3.865          3.5775
v  Pressure               -1081.7           766.5         -60.379         -251.48
v  k                   1.2439e-07          1.1561       0.0081055       0.0046056
v  omega                  0.20187      3.8356e+05          8895.2          3753.2
v  TempC                  -108.31          541.65          2.3004          1.4438
v  Density                0.44711          2.2194          1.2867          1.2901
v  TurbVisc            3.4486e-11       0.0013013      4.2442e-06      6.2718e-06
v  CourantNb                    0          25.485         0.69752         0.47917
v  FourierNb            0.0024655          1.3029         0.01341       0.0085392
v  total_pressure      1.0024e+05      1.0209e+05      1.0126e+05      1.0107e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.44711          2.0975          1.2652          1.2782


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015473          25.537         0.71093         0.48771


 TIME FOR THE TIME STEP               28:        0.19088E+03

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


 INSTANT    0.830000000E-03   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.158444290E-01
Smooth wall               5      225028         0.663923224E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.158497115E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12570E+03 0.20968E+01
   Friction velocity        uet   :  0.10844E-01 0.54553E+01
   Friction velocity        uk    :  0.13150E-01 0.14828E+01
   Dimensionless distance   yplus :  0.33297E+00 0.21903E+02
   Friction thermal sca.    tstar : -0.77644E+03 0.15811E+02
   Rough dim-less th. sca.  tplus :  0.24844E+00 0.11307E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     200127
   Nb of faces within the viscous sub-layer     :       2275
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        533 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19677E+00      28   0.26909E-01   0.11322E+03 0.29152E+03 
c  Velocity[X]                                      0.75767E+02 
c  Velocity[Y]                                      0.14993E+02 
c  Velocity[Z]                                      0.22464E+02 
c  Pressure     0.10751E-02    1348   0.32166E-01   0.88323E+00 0.18475E+05 
c  k            0.15236E-02      22   0.61291E-02   0.39134E+00 0.13538E+04 
c  omega        0.33075E+03      38   0.25942E-02   0.71808E+10 0.12255E+04 
c  TempC        0.77026E+03      49   0.11923E+00   0.13307E+06 0.15020E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -57.396          50.367          3.6669          3.5018
v  Velocity[Y]            -21.754          20.462        0.001299       0.0019909
v  Velocity[Z]            -26.551          25.954        -0.03226       -0.016249
v  ǁVelocityǁ            0.027996          57.436          3.8325          3.5466
v  Pressure               -1106.4          685.25          347.86          278.75
v  k                    8.281e-07          2.5701       0.0082061       0.0049466
v  omega                  0.21734      4.8822e+05          8100.6          3492.7
v  TempC                  -84.121          549.74          2.6935          1.6891
v  Density                0.43346          2.1426          1.2854          1.2896
v  TurbVisc             1.535e-11       0.0015405      4.9745e-06      7.3928e-06
v  CourantNb                    0          27.638          0.6818         0.46781
v  FourierNb            0.0024644          1.6403         0.01376         0.00898
v  total_pressure      1.0022e+05      1.0201e+05      1.0167e+05       1.016e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.44355          2.1426          1.2605          1.2761


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015291          27.694         0.69556         0.47679


 TIME FOR THE TIME STEP               29:        0.14515E+03

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


 INSTANT    0.930000000E-03   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.156918060E-01
Smooth wall               5      225028        -0.532949379E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.156952213E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14588E+03 0.21675E+01
   Friction velocity        uet   :  0.71734E-02 0.54320E+01
   Friction velocity        uk    :  0.17811E-01 0.18832E+01
   Dimensionless distance   yplus :  0.28978E+00 0.21852E+02
   Friction thermal sca.    tstar : -0.83982E+03 0.18163E+02
   Rough dim-less th. sca.  tplus :  0.21621E+00 0.11302E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     200073
   Nb of faces within the viscous sub-layer     :       2320
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        513 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19785E+00      27   0.26679E-01   0.74720E+02 0.23758E+03 
c  Velocity[X]                                      0.47860E+02 
c  Velocity[Y]                                      0.10863E+02 
c  Velocity[Z]                                      0.15998E+02 
c  Pressure     0.96239E-03    1022   0.31848E-01   0.90666E+00 0.40451E+04 
c  k            0.16174E-02      22   0.60148E-02   0.43896E+00 0.13119E+04 
c  omega        0.30273E+03      37   0.19592E-02   0.55070E+10 0.11541E+04 
c  TempC        0.81284E+03      50   0.11575E+00   0.12408E+06 0.13322E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -59.717          50.473          3.6536          3.4898
v  Velocity[Y]            -24.096          18.592       0.0012951       0.0018784
v  Velocity[Z]            -26.123          25.467       -0.033299       -0.016651
v  ǁVelocityǁ            0.021982          60.013          3.8155          3.5336
v  Pressure                 -1128          606.58           452.2          424.46
v  k                   3.0482e-07          3.0658       0.0084929       0.0053253
v  omega                  0.23433      4.8173e+05          7512.5          3281.8
v  TempC                  -94.515          585.05          3.0717          1.9324
v  Density                 0.4292          1.8684          1.2842          1.2891
v  TurbVisc             3.273e-11       0.0017707      5.5839e-06      8.3202e-06
v  CourantNb                    0          27.101         0.67563         0.46352
v  FourierNb            0.0024635          1.8158        0.014081       0.0093817
v  total_pressure       1.002e+05      1.0193e+05      1.0178e+05      1.0175e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.43641          1.8684          1.2562          1.2743


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014646          27.174         0.68971          0.4729


 TIME FOR THE TIME STEP               30:        0.12491E+03

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


 INSTANT    0.103000000E-02   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.156252839E-01
Smooth wall               5      225028         0.143951775E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.156268832E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18287E+03 0.23028E+01
   Friction velocity        uet   :  0.13223E-01 0.57789E+01
   Friction velocity        uk    :  0.16530E-01 0.20508E+01
   Dimensionless distance   yplus :  0.35675E+00 0.22736E+02
   Friction thermal sca.    tstar : -0.60058E+03 0.35125E+02
   Rough dim-less th. sca.  tplus :  0.26617E+00 0.11396E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     199878
   Nb of faces within the viscous sub-layer     :       2418
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        476 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19798E+00      28   0.25243E-01   0.75554E+02 0.23927E+03 
c  Velocity[X]                                      0.51824E+02 
c  Velocity[Y]                                      0.92694E+01 
c  Velocity[Z]                                      0.14461E+02 
c  Pressure     0.83190E-03     699   0.29757E-01   0.86705E+00 0.11812E+04 
c  k            0.17129E-02      21   0.46206E-02   0.49191E+00 0.12863E+04 
c  omega        0.29304E+03      36   0.22554E-02   0.31463E+12 0.68106E+04 
c  TempC        0.85482E+03      50   0.11171E+00   0.12693E+06 0.12567E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -51.068          50.234          3.6485          3.4858
v  Velocity[Y]            -21.286          17.342       0.0011519       0.0017283
v  Velocity[Z]            -26.125          25.242       -0.034341       -0.017087
v  ǁVelocityǁ            0.012203          51.088          3.8049          3.5284
v  Pressure               -1156.6          552.45           470.3          460.46
v  k                   1.4626e-06          3.7996       0.0088887       0.0057271
v  omega                  0.24927      4.0486e+07          7077.4            3107
v  TempC                  -100.14          595.58          3.4238          2.1697
v  Density                0.41154          1.9771           1.283          1.2886
v  TurbVisc            3.0994e-11       0.0019628       6.057e-06      9.0232e-06
v  CourantNb                    0          28.804         0.67239         0.46168
v  FourierNb            0.0024627          2.3771        0.014394       0.0097656
v  total_pressure      1.0017e+05      1.0188e+05       1.018e+05      1.0179e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42959          1.8441          1.2523          1.2726


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014357          28.865         0.68678         0.47144


 TIME FOR THE TIME STEP               31:        0.10267E+03

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


 INSTANT    0.113000000E-02   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155937602E-01
Smooth wall               5      225028         0.532474295E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155950704E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.91574E+02 0.26689E+01
   Friction velocity        uet   :  0.12310E-01 0.42739E+01
   Friction velocity        uk    :  0.18773E-01 0.16181E+01
   Dimensionless distance   yplus :  0.26218E+00 0.21448E+02
   Friction thermal sca.    tstar : -0.79646E+03 0.31924E+02
   Rough dim-less th. sca.  tplus :  0.19561E+00 0.11257E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     199466
   Nb of faces within the viscous sub-layer     :       2554
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        362 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19797E+00      27   0.23909E-01   0.91775E+02 0.26374E+03 
c  Velocity[X]                                      0.68081E+02 
c  Velocity[Y]                                      0.89812E+01 
c  Velocity[Z]                                      0.14713E+02 
c  Pressure     0.66432E-03     571   0.26134E-01   0.74817E+00 0.73364E+03 
c  k            0.18111E-02      21   0.16871E-02   0.53381E+00 0.12523E+04 
c  omega        0.13662E+05      26   0.24954E-04   0.80181E+11 0.44369E+04 
c  TempC        0.89864E+03      49   0.10154E+00   0.13105E+06 0.12036E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -42.227          49.327            3.65          3.4877
v  Velocity[Y]            -17.684          15.987      0.00096983       0.0015664
v  Velocity[Z]            -25.532          24.573       -0.035365       -0.017573
v  ǁVelocityǁ            0.012656          49.328          3.7994          3.5289
v  Pressure               -1179.9          499.15          474.28          477.73
v  k                   2.0485e-07          4.8219        0.009361       0.0061467
v  omega                  0.26418      2.0244e+07          6695.8          2957.8
v  TempC                  -95.494          606.87          3.7545          2.4025
v  Density                0.40655          2.0414          1.2819          1.2881
v  TurbVisc            2.4333e-11       0.0021273      6.4282e-06      9.5679e-06
v  CourantNb                    0          27.199         0.67011         0.46083
v  FourierNb             0.002462          2.8194        0.014668        0.010096
v  total_pressure      1.0015e+05      1.0182e+05       1.018e+05       1.018e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42087          2.0414          1.2487           1.271


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016911          27.285         0.68478         0.47092


 TIME FOR THE TIME STEP               32:        0.93649E+02

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


 INSTANT    0.123000000E-02   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155881828E-01
Smooth wall               5      225028         0.788416215E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155890194E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88301E+02 0.30018E+01
   Friction velocity        uet   :  0.93292E-02 0.42451E+01
   Friction velocity        uk    :  0.91832E-02 0.14772E+01
   Dimensionless distance   yplus :  0.28805E+00 0.23470E+02
   Friction thermal sca.    tstar : -0.86846E+03 0.50073E+02
   Rough dim-less th. sca.  tplus :  0.21491E+00 0.11472E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     199068
   Nb of faces within the viscous sub-layer     :       2668
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        312 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19821E+00      27   0.22688E-01   0.90877E+02 0.26233E+03 
c  Velocity[X]                                      0.70414E+02 
c  Velocity[Y]                                      0.78690E+01 
c  Velocity[Z]                                      0.12594E+02 
c  Pressure     0.52230E-03     588   0.22869E-01   0.63287E+00 0.51374E+03 
c  k            0.19101E-02      20   0.10254E-02   0.57317E+00 0.12232E+04 
c  omega        0.34462E+04      29   0.51343E-04   0.21349E+11 0.25935E+04 
c  TempC        0.94531E+03      49   0.95387E-01   0.12953E+06 0.11347E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -29.644          49.465          3.6526          3.4913
v  Velocity[Y]            -16.616           15.51      0.00068293       0.0014023
v  Velocity[Z]            -24.791          23.746       -0.036518       -0.018074
v  ǁVelocityǁ           0.0073031          49.472          3.7959          3.5312
v  Pressure               -1204.9           468.4          448.64          456.02
v  k                   5.1847e-08          4.4681       0.0098521       0.0065743
v  omega                  0.27974      1.0117e+07          6384.5          2829.3
v  TempC                  -101.24          605.91          4.0672          2.6333
v  Density                0.40134           1.988          1.2809          1.2876
v  TurbVisc            3.6494e-12        0.002165      6.8071e-06      1.0106e-05
v  CourantNb           1.0011e-08           28.84         0.66881         0.46075
v  FourierNb            0.0024614          3.0744        0.014983        0.010476
v  total_pressure      1.0012e+05      1.0179e+05      1.0177e+05      1.0178e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42021          1.7961          1.2455          1.2696


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016705          28.908         0.68379         0.47122


 TIME FOR THE TIME STEP               33:        0.94905E+02

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


 INSTANT    0.133000000E-02   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155882899E-01
Smooth wall               5      225028        -0.119447223E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155910541E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86815E+02 0.38796E+01
   Friction velocity        uet   :  0.59305E-02 0.41525E+01
   Friction velocity        uk    :  0.59752E-02 0.12828E+01
   Dimensionless distance   yplus :  0.19669E+00 0.25973E+02
   Friction thermal sca.    tstar : -0.13317E+04 0.41593E+02
   Rough dim-less th. sca.  tplus :  0.14675E+00 0.11713E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     198539
   Nb of faces within the viscous sub-layer     :       2815
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        216 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19831E+00      26   0.21667E-01   0.67384E+02 0.22574E+03 
c  Velocity[X]                                      0.52190E+02 
c  Velocity[Y]                                      0.53454E+01 
c  Velocity[Z]                                      0.98489E+01 
c  Pressure     0.40437E-03     714   0.19314E-01   0.52198E+00 0.84625E+03 
c  k            0.20017E-02      19   0.88378E-03   0.61713E+00 0.12048E+04 
c  omega        0.89545E+03      32   0.11545E-03   0.63884E+10 0.15186E+04 
c  TempC        0.98924E+03      49   0.91376E-01   0.12916E+06 0.10794E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.495           48.55          3.6546          3.4948
v  Velocity[Y]            -12.609          11.009      0.00051144       0.0012621
v  Velocity[Z]            -24.886          22.805       -0.037664       -0.018565
v  ǁVelocityǁ           0.0046991          48.552           3.793          3.5338
v  Pressure               -1226.4          432.31          413.37          420.43
v  k                   3.0077e-07          5.9648        0.010364       0.0070051
v  omega                  0.29893      5.0493e+06          6128.3          2717.8
v  TempC                  -108.36          610.52          4.3666           2.863
v  Density                0.40178          2.0545          1.2799          1.2872
v  TurbVisc            4.2242e-13       0.0022051      7.2786e-06      1.0774e-05
v  CourantNb                    0          28.543         0.66781          0.4609
v  FourierNb            0.0024609          3.1887        0.015392         0.01099
v  total_pressure       1.001e+05      1.0176e+05      1.0174e+05      1.0175e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42496          1.8837          1.2425          1.2682


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015614          28.644          0.6832         0.47189


 TIME FOR THE TIME STEP               34:        0.10298E+03

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


 INSTANT    0.143000000E-02   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155900395E-01
Smooth wall               5      225028         0.610804826E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155926166E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88628E+02 0.46394E+01
   Friction velocity        uet   :  0.14558E-01 0.41856E+01
   Friction velocity        uk    :  0.14383E-01 0.13691E+01
   Dimensionless distance   yplus :  0.30479E+00 0.27437E+02
   Friction thermal sca.    tstar : -0.56595E+03 0.43907E+02
   Rough dim-less th. sca.  tplus :  0.22740E+00 0.11844E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     197981
   Nb of faces within the viscous sub-layer     :       2968
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        139 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19833E+00      26   0.20727E-01   0.48893E+02 0.19214E+03 
c  Velocity[X]                                      0.38190E+02 
c  Velocity[Y]                                      0.34787E+01 
c  Velocity[Z]                                      0.72239E+01 
c  Pressure     0.30907E-03     681   0.16176E-01   0.41838E+00 0.80889E+03 
c  k            0.20837E-02      18   0.73666E-03   0.65276E+00 0.11832E+04 
c  omega        0.31147E+03      34   0.14052E-03   0.25180E+10 0.99791E+03 
c  TempC        0.10271E+04      48   0.86336E-01   0.12822E+06 0.10286E+04 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.138          49.281          3.6558          3.4977
v  Velocity[Y]            -11.296          12.104      0.00035229        0.001126
v  Velocity[Z]             -24.97          22.444       -0.038887       -0.019073
v  ǁVelocityǁ           0.0068966           49.29          3.7907          3.5361
v  Pressure                 -1251          402.53          382.88          389.01
v  k                   5.3446e-08          4.4161        0.010872       0.0074369
v  omega                  0.31524       2.512e+06          5916.8          2620.6
v  TempC                  -115.41           588.9          4.6541          3.0919
v  Density                0.39968          2.1432           1.279          1.2867
v  TurbVisc            2.3853e-12       0.0022331      7.8027e-06      1.1522e-05
v  CourantNb                    0          28.543         0.66691         0.46108
v  FourierNb            0.0024603          3.3723        0.015853        0.011586
v  total_pressure      1.0007e+05      1.0173e+05      1.0171e+05      1.0171e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42244          1.8716          1.2397          1.2669


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015887          28.618         0.68276         0.47267


 TIME FOR THE TIME STEP               35:        0.10139E+03

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


 INSTANT    0.153000000E-02   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155901634E-01
Smooth wall               5      225028        -0.102233334E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155927571E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87116E+02 0.36434E+01
   Friction velocity        uet   :  0.60278E-02 0.41699E+01
   Friction velocity        uk    :  0.12749E-01 0.12352E+01
   Dimensionless distance   yplus :  0.17579E+00 0.26986E+02
   Friction thermal sca.    tstar : -0.97284E+03 0.23663E+02
   Rough dim-less th. sca.  tplus :  0.13116E+00 0.11804E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     197460
   Nb of faces within the viscous sub-layer     :       3115
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         80 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19831E+00      25   0.19190E-01   0.39786E+02 0.17318E+03 
c  Velocity[X]                                      0.31640E+02 
c  Velocity[Y]                                      0.24801E+01 
c  Velocity[Z]                                      0.56666E+01 
c  Pressure     0.24511E-03     608   0.13049E-01   0.34391E+00 0.64303E+03 
c  k            0.21591E-02      18   0.69839E-03   0.68709E+00 0.11641E+04 
c  omega        0.22054E+03      35   0.10622E-03   0.12956E+10 0.74132E+03 
c  TempC        0.10617E+04      47   0.82594E-01   0.12835E+06 0.98790E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.422          48.631          3.6562          3.5004
v  Velocity[Y]            -10.897          10.882      0.00017079       0.0010139
v  Velocity[Z]            -24.585           21.55       -0.040134       -0.019573
v  ǁVelocityǁ            0.010245           48.65          3.7889          3.5385
v  Pressure               -1268.8          379.43          359.92          365.52
v  k                   1.1139e-07          5.0354        0.011389       0.0078711
v  omega                  0.32859       1.243e+06          5741.7          2535.5
v  TempC                  -135.85          590.03          4.9409          3.3206
v  Density                 0.4097           2.239          1.2781          1.2863
v  TurbVisc            5.1407e-13       0.0022617      8.3598e-06       1.232e-05
v  CourantNb                    0          27.052         0.66609         0.46124
v  FourierNb            0.0024599           3.505        0.016348         0.01223
v  total_pressure      1.0006e+05       1.017e+05      1.0168e+05      1.0169e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41524          1.9041          1.2371          1.2657


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015264          27.128         0.68244         0.47347


 TIME FOR THE TIME STEP               36:        0.96380E+02

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


 INSTANT    0.163000000E-02   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155894623E-01
Smooth wall               5      225028        -0.144128144E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155919594E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82152E+02 0.38512E+01
   Friction velocity        uet   :  0.98296E-02 0.41362E+01
   Friction velocity        uk    :  0.96854E-02 0.12156E+01
   Dimensionless distance   yplus :  0.22930E+00 0.26989E+02
   Friction thermal sca.    tstar : -0.78761E+03 0.20218E+02
   Rough dim-less th. sca.  tplus :  0.17108E+00 0.11804E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     197032
   Nb of faces within the viscous sub-layer     :       3277
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19830E+00      26   0.19568E-01   0.34372E+02 0.16081E+03 
c  Velocity[X]                                      0.27901E+02 
c  Velocity[Y]                                      0.18797E+01 
c  Velocity[Z]                                      0.45909E+01 
c  Pressure     0.20198E-03     501   0.10957E-01   0.29002E+00 0.44134E+03 
c  k            0.22290E-02      18   0.67864E-03   0.72307E+00 0.11491E+04 
c  omega        0.20594E+03      34   0.87546E-04   0.10213E+10 0.67696E+03 
c  TempC        0.10912E+04      46   0.81710E-01   0.12932E+06 0.95507E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7573          49.055          3.6567          3.5032
v  Velocity[Y]            -10.405          11.319      2.9406e-05      0.00091157
v  Velocity[Z]            -24.281          21.208       -0.041396       -0.020072
v  ǁVelocityǁ            0.014956          49.079          3.7878          3.5409
v  Pressure                 -1290          363.35          344.39          350.07
v  k                   2.4599e-10          3.4612        0.011923       0.0083087
v  omega                  0.34677      6.1144e+05          5596.8          2460.6
v  TempC                  -123.15          588.71          5.2226          3.5489
v  Density                0.40916          2.5724          1.2772          1.2858
v  TurbVisc            1.3083e-12       0.0022756       8.926e-06      1.3135e-05
v  CourantNb                    0          29.189         0.66542         0.46141
v  FourierNb            0.0024594          3.5736         0.01685        0.012888
v  total_pressure      1.0003e+05      1.0169e+05      1.0167e+05      1.0168e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41063          2.0236          1.2346          1.2645


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014953          29.272         0.68227          0.4743


 TIME FOR THE TIME STEP               37:        0.88881E+02

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


 INSTANT    0.173000000E-02   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155888867E-01
Smooth wall               5      225028        -0.559655034E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155914020E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80926E+02 0.39393E+01
   Friction velocity        uet   :  0.11882E-01 0.41081E+01
   Friction velocity        uk    :  0.11679E-01 0.12206E+01
   Dimensionless distance   yplus :  0.24072E+00 0.26115E+02
   Friction thermal sca.    tstar : -0.78085E+03 0.20032E+02
   Rough dim-less th. sca.  tplus :  0.17960E+00 0.11726E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     196575
   Nb of faces within the viscous sub-layer     :       3452
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19831E+00      26   0.19689E-01   0.32496E+02 0.15620E+03 
c  Velocity[X]                                      0.27000E+02 
c  Velocity[Y]                                      0.15886E+01 
c  Velocity[Z]                                      0.39079E+01 
c  Pressure     0.17158E-03     464   0.92783E-02   0.25054E+00 0.38850E+03 
c  k            0.22954E-02      17   0.65193E-03   0.75883E+00 0.11359E+04 
c  omega        0.19857E+03      34   0.11952E-03   0.23095E+10 0.10384E+04 
c  TempC        0.11180E+04      47   0.76185E-01   0.12942E+06 0.92245E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6237            48.5          3.6571          3.5058
v  Velocity[Y]             -9.767          11.283     -3.5617e-05       0.0008382
v  Velocity[Z]            -24.351          20.453       -0.042632        -0.02056
v  ǁVelocityǁ            0.018998          48.519           3.787          3.5434
v  Pressure               -1305.7           350.1          331.44          336.98
v  k                    9.553e-09          2.9209        0.012474       0.0087496
v  omega                  0.37063      1.3866e+06          5479.6          2394.4
v  TempC                  -129.04          588.35          5.5015          3.7776
v  Density                0.40979          2.3545          1.2764          1.2854
v  TurbVisc              4.68e-14       0.0022781      9.4923e-06      1.3963e-05
v  CourantNb                    0          27.305         0.66484         0.46161
v  FourierNb             0.002459          3.6374         0.01735        0.013551
v  total_pressure      1.0002e+05      1.0168e+05      1.0166e+05      1.0166e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41888           1.953          1.2323          1.2634


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013975          27.387         0.68219         0.47516


 TIME FOR THE TIME STEP               38:        0.86029E+02

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


 INSTANT    0.183000000E-02   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155881319E-01
Smooth wall               5      225028        -0.582706231E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155904207E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75360E+02 0.39881E+01
   Friction velocity        uet   :  0.17804E-01 0.41058E+01
   Friction velocity        uk    :  0.17376E-01 0.12015E+01
   Dimensionless distance   yplus :  0.25430E+00 0.26799E+02
   Friction thermal sca.    tstar : -0.53902E+03 0.15941E+02
   Rough dim-less th. sca.  tplus :  0.18974E+00 0.11788E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     196156
   Nb of faces within the viscous sub-layer     :       3572
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19831E+00      25   0.17936E-01   0.31179E+02 0.15283E+03 
c  Velocity[X]                                      0.26335E+02 
c  Velocity[Y]                                      0.13724E+01 
c  Velocity[Z]                                      0.34711E+01 
c  Pressure     0.15362E-03     378   0.82221E-02   0.22804E+00 0.26569E+03 
c  k            0.23601E-02      17   0.64879E-03   0.79755E+00 0.11266E+04 
c  omega        0.19665E+03      33   0.11510E-03   0.17873E+10 0.93251E+03 
c  TempC        0.11438E+04      47   0.75756E-01   0.12717E+06 0.88459E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2155          49.432          3.6576          3.5085
v  Velocity[Y]            -9.1535          11.425     -0.00011205      0.00076771
v  Velocity[Z]            -23.908           20.23       -0.043872       -0.021044
v  ǁVelocityǁ            0.017732          49.465          3.7867           3.546
v  Pressure               -1324.4          341.03          322.64          328.25
v  k                   1.9591e-09          2.9045        0.013037       0.0091918
v  omega                  0.40134      1.2301e+06          5379.4          2335.4
v  TempC                  -137.92           595.1          5.7807          4.0074
v  Density                0.40996          2.4507          1.2756          1.2849
v  TurbVisc             7.431e-14       0.0022804      1.0055e-05      1.4786e-05
v  CourantNb                    0          29.323         0.66434         0.46181
v  FourierNb            0.0024586          3.6746        0.017846        0.014207
v  total_pressure           1e+05      1.0167e+05      1.0165e+05      1.0165e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4157          2.1246          1.2301          1.2623


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013548          29.411         0.68219         0.47602


 TIME FOR THE TIME STEP               39:        0.79961E+02

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


 INSTANT    0.193000000E-02   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155875108E-01
Smooth wall               5      225028        -0.268382344E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155899185E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.73116E+02 0.38239E+01
   Friction velocity        uet   :  0.93041E-02 0.41046E+01
   Friction velocity        uk    :  0.13281E-01 0.12065E+01
   Dimensionless distance   yplus :  0.21845E+00 0.26890E+02
   Friction thermal sca.    tstar : -0.73114E+03 0.16548E+02
   Rough dim-less th. sca.  tplus :  0.16299E+00 0.11796E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     195857
   Nb of faces within the viscous sub-layer     :       3757
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19834E+00      25   0.18458E-01   0.29775E+02 0.14918E+03 
c  Velocity[X]                                      0.25481E+02 
c  Velocity[Y]                                      0.12139E+01 
c  Velocity[Z]                                      0.30802E+01 
c  Pressure     0.14326E-03     355   0.75829E-02   0.21457E+00 0.23516E+03 
c  k            0.24244E-02      17   0.66624E-03   0.83637E+00 0.11185E+04 
c  omega        0.18909E+03      34   0.10071E-03   0.12144E+10 0.78256E+03 
c  TempC        0.11680E+04      47   0.74786E-01   0.12830E+06 0.86160E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1575          49.421          3.6582          3.5112
v  Velocity[Y]            -8.1244          11.898     -0.00019463      0.00070194
v  Velocity[Z]            -24.482          19.992       -0.045102       -0.021513
v  ǁVelocityǁ            0.011061          49.452          3.7866          3.5486
v  Pressure               -1337.2           333.5          315.14          320.71
v  k                   3.1933e-09           3.011        0.013611       0.0096365
v  omega                  0.44041      6.3946e+05          5295.6          2282.6
v  TempC                  -122.67           605.7            6.06          4.2372
v  Density                0.40678          2.6118          1.2748          1.2845
v  TurbVisc             2.326e-14       0.0022822      1.0598e-05      1.5577e-05
v  CourantNb                    0          27.709         0.66397         0.46204
v  FourierNb            0.0024583          3.6976        0.018327         0.01484
v  total_pressure           99988      1.0166e+05      1.0164e+05      1.0165e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42032          2.2252           1.228          1.2612


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014206          27.794         0.68229         0.47688


 TIME FOR THE TIME STEP               40:        0.78465E+02

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


 INSTANT    0.203000000E-02   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155868767E-01
Smooth wall               5      225028         0.489269557E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155890494E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75193E+02 0.40065E+01
   Friction velocity        uet   :  0.16317E-01 0.41080E+01
   Friction velocity        uk    :  0.16148E-01 0.12144E+01
   Dimensionless distance   yplus :  0.22354E+00 0.27698E+02
   Friction thermal sca.    tstar : -0.77215E+03 0.91863E+01
   Rough dim-less th. sca.  tplus :  0.16679E+00 0.11866E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     195495
   Nb of faces within the viscous sub-layer     :       3927
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19835E+00      26   0.18391E-01   0.29545E+02 0.14842E+03 
c  Velocity[X]                                      0.25570E+02 
c  Velocity[Y]                                      0.10987E+01 
c  Velocity[Z]                                      0.28763E+01 
c  Pressure     0.13991E-03     304   0.73728E-02   0.21130E+00 0.17439E+03 
c  k            0.24895E-02      17   0.68407E-03   0.87199E+00 0.11088E+04 
c  omega        0.18284E+03      33   0.11614E-03   0.21323E+10 0.10492E+04 
c  TempC        0.11912E+04      48   0.74464E-01   0.12974E+06 0.84186E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2469          50.094          3.6589          3.5139
v  Velocity[Y]            -7.7899          11.501     -0.00029813      0.00063631
v  Velocity[Z]             -24.35            19.8       -0.046323       -0.021991
v  ǁVelocityǁ             0.01347          50.129          3.7868          3.5513
v  Pressure               -1353.3          327.82          309.61          315.21
v  k                   7.1741e-08          2.9387        0.014195        0.010085
v  omega                  0.47465      1.5167e+06          5225.8          2235.2
v  TempC                  -124.86          593.77          6.3342          4.4667
v  Density                0.40187          2.3471           1.274           1.284
v  TurbVisc             3.703e-14         0.00228      1.1127e-05      1.6348e-05
v  CourantNb                    0          30.082         0.66367         0.46228
v  FourierNb             0.002458          3.7134          0.0188        0.015462
v  total_pressure           99972      1.0165e+05      1.0163e+05      1.0164e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40187          2.1451          1.2259          1.2602


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015141          30.173         0.68247         0.47774


 TIME FOR THE TIME STEP               41:        0.75135E+02

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


 INSTANT    0.213000000E-02   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155863511E-01
Smooth wall               5      225028         0.314034444E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155884962E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72721E+02 0.36537E+01
   Friction velocity        uet   :  0.11757E-01 0.41135E+01
   Friction velocity        uk    :  0.11970E-01 0.12044E+01
   Dimensionless distance   yplus :  0.23278E+00 0.26778E+02
   Friction thermal sca.    tstar : -0.81024E+03 0.13905E+02
   Rough dim-less th. sca.  tplus :  0.17368E+00 0.11786E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     195169
   Nb of faces within the viscous sub-layer     :       4097
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19837E+00      25   0.17585E-01   0.28983E+02 0.14683E+03 
c  Velocity[X]                                      0.25330E+02 
c  Velocity[Y]                                      0.10090E+01 
c  Velocity[Z]                                      0.26434E+01 
c  Pressure     0.13557E-03     296   0.71730E-02   0.20635E+00 0.15931E+03 
c  k            0.25532E-02      18   0.67907E-03   0.90658E+00 0.10994E+04 
c  omega        0.18314E+03      33   0.35547E-03   0.21573E+11 0.32164E+04 
c  TempC        0.12139E+04      47   0.69468E-01   0.13065E+06 0.82218E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1298          49.498          3.6597          3.5166
v  Velocity[Y]            -7.9546          11.713     -0.00038772      0.00057896
v  Velocity[Z]            -24.675          19.546       -0.047508        -0.02245
v  ǁVelocityǁ             0.01241          49.508          3.7872          3.5541
v  Pressure               -1363.4           322.5          304.58          310.27
v  k                   1.2269e-07          2.9809        0.014787        0.010536
v  omega                  0.40738      7.1795e+06          5169.1          2192.4
v  TempC                  -126.62          602.05          6.6076          4.6963
v  Density                 0.4074          2.3817          1.2732          1.2836
v  TurbVisc            5.4984e-13       0.0022808      1.1655e-05      1.7117e-05
v  CourantNb                    0          28.227         0.66339         0.46253
v  FourierNb            0.0024577          3.7241        0.019276        0.016088
v  total_pressure           99962      1.0165e+05      1.0163e+05      1.0164e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41322          2.1966           1.224          1.2591


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015224          28.315         0.68267         0.47861


 TIME FOR THE TIME STEP               42:        0.74522E+02

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


 INSTANT    0.223000000E-02   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155860628E-01
Smooth wall               5      225028         0.423063655E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155879430E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71317E+02 0.39109E+01
   Friction velocity        uet   :  0.54695E-02 0.41141E+01
   Friction velocity        uk    :  0.60084E-02 0.12011E+01
   Dimensionless distance   yplus :  0.12240E+00 0.26880E+02
   Friction thermal sca.    tstar : -0.18485E+04 0.19902E+02
   Rough dim-less th. sca.  tplus :  0.91325E-01 0.11795E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     194829
   Nb of faces within the viscous sub-layer     :       4258
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19840E+00      25   0.17358E-01   0.28624E+02 0.14574E+03 
c  Velocity[X]                                      0.25120E+02 
c  Velocity[Y]                                      0.94959E+00 
c  Velocity[Z]                                      0.25542E+01 
c  Pressure     0.13485E-03     279   0.71666E-02   0.20668E+00 0.14023E+03 
c  k            0.26158E-02      17   0.67525E-03   0.94456E+00 0.10931E+04 
c  omega        0.82064E+03      30   0.42783E-04   0.58807E+10 0.17630E+04 
c  TempC        0.12365E+04      46   0.68234E-01   0.12835E+06 0.79384E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.0301           50.72          3.6605          3.5194
v  Velocity[Y]            -7.9485          10.702       -0.000472      0.00052636
v  Velocity[Z]            -23.857          19.395       -0.048693       -0.022915
v  ǁVelocityǁ            0.013961          50.759          3.7877          3.5568
v  Pressure                 -1377          318.15          300.22          305.99
v  k                   1.3116e-07          3.0351        0.015385        0.010988
v  omega                  0.54711       3.614e+06          5115.3          2153.1
v  TempC                  -115.79           592.5          6.8776          4.9271
v  Density                0.40355          2.4103          1.2724          1.2831
v  TurbVisc            8.9842e-13       0.0022833      1.2172e-05      1.7874e-05
v  CourantNb                    0           30.32         0.66319         0.46279
v  FourierNb            0.0024574          3.7313        0.019746        0.016705
v  total_pressure           99948      1.0164e+05      1.0163e+05      1.0163e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40951          2.1013          1.2221          1.2581


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016258          30.412         0.68293         0.47949


 TIME FOR THE TIME STEP               43:        0.73166E+02

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


 INSTANT    0.233000000E-02   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155858367E-01
Smooth wall               5      225028         0.218548550E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876984E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72165E+02 0.41899E+01
   Friction velocity        uet   :  0.15641E-01 0.42114E+01
   Friction velocity        uk    :  0.16947E-01 0.12144E+01
   Dimensionless distance   yplus :  0.29242E+00 0.26694E+02
   Friction thermal sca.    tstar : -0.67650E+03 0.26368E+02
   Rough dim-less th. sca.  tplus :  0.21818E+00 0.11778E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     194479
   Nb of faces within the viscous sub-layer     :       4391
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19843E+00      25   0.17651E-01   0.27980E+02 0.14391E+03 
c  Velocity[X]                                      0.24639E+02 
c  Velocity[Y]                                      0.88902E+00 
c  Velocity[Z]                                      0.24524E+01 
c  Pressure     0.13396E-03     286   0.70472E-02   0.20590E+00 0.15272E+03 
c  k            0.26765E-02      17   0.67645E-03   0.98415E+00 0.10887E+04 
c  omega        0.26776E+03      32   0.91986E-04   0.20611E+10 0.10641E+04 
c  TempC        0.12586E+04      48   0.67395E-01   0.12805E+06 0.77347E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2874           50.19          3.6614          3.5222
v  Velocity[Y]            -8.0934          11.245     -0.00054665      0.00048078
v  Velocity[Z]            -24.316          19.093       -0.049869       -0.023379
v  ǁVelocityǁ            0.010611          50.225          3.7883          3.5597
v  Pressure               -1384.8          313.27          295.55          301.39
v  k                   1.1471e-08          3.0387        0.015988        0.011439
v  omega                 0.046537        1.83e+06          5069.6          2117.2
v  TempC                  -98.968          593.78          7.1454           5.158
v  Density                  0.408          2.2445          1.2716          1.2826
v  TurbVisc            8.5973e-13        0.002285      1.2696e-05      1.8642e-05
v  CourantNb                    0           28.63         0.66299         0.46306
v  FourierNb            0.0024572          3.7362        0.020223        0.017336
v  total_pressure           99940      1.0164e+05      1.0162e+05      1.0163e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41895          2.1758          1.2202          1.2572


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017035          28.719         0.68321         0.48039


 TIME FOR THE TIME STEP               44:        0.73948E+02

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


 INSTANT    0.243000000E-02   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155856886E-01
Smooth wall               5      225028         0.931858731E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155877617E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71111E+02 0.43033E+01
   Friction velocity        uet   :  0.12185E-01 0.41406E+01
   Friction velocity        uk    :  0.18890E-01 0.12141E+01
   Dimensionless distance   yplus :  0.29996E+00 0.27626E+02
   Friction thermal sca.    tstar : -0.54334E+03 0.31446E+02
   Rough dim-less th. sca.  tplus :  0.22381E+00 0.11860E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     194097
   Nb of faces within the viscous sub-layer     :       4530
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19846E+00      26   0.17574E-01   0.27880E+02 0.14347E+03 
c  Velocity[X]                                      0.24599E+02 
c  Velocity[Y]                                      0.84643E+00 
c  Velocity[Z]                                      0.24346E+01 
c  Pressure     0.13674E-03     304   0.72744E-02   0.21120E+00 0.18238E+03 
c  k            0.27361E-02      17   0.66805E-03   0.10208E+01 0.10830E+04 
c  omega        0.17734E+03      32   0.18777E-03   0.81742E+10 0.21000E+04 
c  TempC        0.12804E+04      46   0.67392E-01   0.12942E+06 0.75958E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.0092          50.819          3.6623           3.525
v  Velocity[Y]            -7.6342          11.154     -0.00060761      0.00044245
v  Velocity[Z]            -24.059          18.887       -0.051021       -0.023834
v  ǁVelocityǁ            0.012356          50.865          3.7891          3.5625
v  Pressure               -1396.3          307.97          290.13          295.99
v  k                    7.449e-08          3.0774        0.016598        0.011891
v  omega                  0.64825      3.2872e+06          5035.1          2084.7
v  TempC                  -105.02          596.51          7.4103          5.3883
v  Density                0.40739          2.0277          1.2708          1.2822
v  TurbVisc            7.5323e-14       0.0022866      1.3217e-05       1.941e-05
v  CourantNb                    0          30.859         0.66284         0.46334
v  FourierNb             0.002457          3.7397        0.020702        0.017972
v  total_pressure           99929      1.0163e+05      1.0162e+05      1.0162e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41566          2.0277          1.2185          1.2562


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014838          30.951         0.68355         0.48131


 TIME FOR THE TIME STEP               45:        0.75114E+02

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


 INSTANT    0.253000000E-02   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855969E-01
Smooth wall               5      225028        -0.206878053E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876975E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70650E+02 0.43563E+01
   Friction velocity        uet   :  0.15540E-01 0.41296E+01
   Friction velocity        uk    :  0.15392E-01 0.12030E+01
   Dimensionless distance   yplus :  0.16395E+00 0.26348E+02
   Friction thermal sca.    tstar : -0.78514E+03 0.36855E+02
   Rough dim-less th. sca.  tplus :  0.12232E+00 0.11747E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     193836
   Nb of faces within the viscous sub-layer     :       4671
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19850E+00      25   0.17433E-01   0.28004E+02 0.14361E+03 
c  Velocity[X]                                      0.24886E+02 
c  Velocity[Y]                                      0.81938E+00 
c  Velocity[Z]                                      0.22985E+01 
c  Pressure     0.13398E-03     304   0.73469E-02   0.20734E+00 0.18044E+03 
c  k            0.27930E-02      17   0.66166E-03   0.10528E+01 0.10752E+04 
c  omega        0.24154E+03      31   0.10505E-03   0.26240E+10 0.12156E+04 
c  TempC        0.13017E+04      47   0.65510E-01   0.13078E+06 0.74676E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3428          50.075          3.6631          3.5278
v  Velocity[Y]             -7.456          10.679     -0.00065228      0.00040694
v  Velocity[Z]            -24.194           18.77       -0.052181       -0.024285
v  ǁVelocityǁ            0.013612          50.115          3.7898          3.5654
v  Pressure               -1403.9          302.65          284.92          290.74
v  k                   2.8376e-08          3.0702        0.017217        0.012345
v  omega                  0.47418      1.6659e+06          4998.5          2054.3
v  TempC                     -111          604.68           7.673          5.6183
v  Density                0.40612          2.1006          1.2701          1.2817
v  TurbVisc            3.8339e-13       0.0022876      1.3718e-05      2.0151e-05
v  CourantNb                    0          28.913         0.66272         0.46363
v  FourierNb            0.0024568          3.7422        0.021166         0.01859
v  total_pressure           99921      1.0163e+05      1.0161e+05      1.0162e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40887          2.1006          1.2167          1.2552


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016855          29.002         0.68389         0.48222


 TIME FOR THE TIME STEP               46:        0.74969E+02

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


 INSTANT    0.263000000E-02   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855519E-01
Smooth wall               5      225028        -0.104202704E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876460E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71090E+02 0.43074E+01
   Friction velocity        uet   :  0.97479E-02 0.41336E+01
   Friction velocity        uk    :  0.96261E-02 0.12214E+01
   Dimensionless distance   yplus :  0.19820E+00 0.26525E+02
   Friction thermal sca.    tstar : -0.10264E+04 0.41738E+02
   Rough dim-less th. sca.  tplus :  0.14788E+00 0.11763E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     193373
   Nb of faces within the viscous sub-layer     :       4779
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19853E+00      26   0.17205E-01   0.27948E+02 0.14328E+03 
c  Velocity[X]                                      0.24859E+02 
c  Velocity[Y]                                      0.79053E+00 
c  Velocity[Z]                                      0.22984E+01 
c  Pressure     0.14148E-03     302   0.75710E-02   0.22022E+00 0.18296E+03 
c  k            0.28476E-02      18   0.67402E-03   0.10862E+01 0.10687E+04 
c  omega        0.17026E+03      32   0.15822E-03   0.14708E+10 0.91873E+03 
c  TempC        0.13227E+04      47   0.62036E-01   0.13057E+06 0.73034E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4224          51.057           3.664          3.5306
v  Velocity[Y]            -7.3789          10.835     -0.00070889      0.00037461
v  Velocity[Z]             -23.23          18.721       -0.053356       -0.024739
v  ǁVelocityǁ            0.014598          51.109          3.7907          3.5683
v  Pressure               -1414.1          297.43          279.65          285.51
v  k                   1.1619e-08          3.0746        0.017846          0.0128
v  omega                  0.77537       8.541e+05          4968.1          2026.3
v  TempC                  -126.17          606.86          7.9312          5.8484
v  Density                0.40234          2.1781          1.2693          1.2813
v  TurbVisc            2.4159e-13        0.002288      1.4223e-05      2.0899e-05
v  CourantNb                    0          30.793         0.66263         0.46391
v  FourierNb            0.0024566          3.7439        0.021639         0.01922
v  total_pressure           99911      1.0162e+05       1.016e+05      1.0161e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40931          1.9977          1.2151          1.2543


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016842          30.886         0.68427         0.48313


 TIME FOR THE TIME STEP               47:        0.75029E+02

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


 INSTANT    0.273000000E-02   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855268E-01
Smooth wall               5      225028        -0.727940749E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155877075E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70673E+02 0.41607E+01
   Friction velocity        uet   :  0.75751E-02 0.42082E+01
   Friction velocity        uk    :  0.15957E-01 0.12150E+01
   Dimensionless distance   yplus :  0.16986E+00 0.26250E+02
   Friction thermal sca.    tstar : -0.70085E+03 0.43249E+02
   Rough dim-less th. sca.  tplus :  0.12673E+00 0.11738E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     192818
   Nb of faces within the viscous sub-layer     :       4889
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19856E+00      25   0.16958E-01   0.27756E+02 0.14261E+03 
c  Velocity[X]                                      0.24715E+02 
c  Velocity[Y]                                      0.78287E+00 
c  Velocity[Z]                                      0.22587E+01 
c  Pressure     0.14300E-03     338   0.76254E-02   0.22336E+00 0.22915E+03 
c  k            0.28992E-02      17   0.69012E-03   0.11241E+01 0.10651E+04 
c  omega        0.16221E+03      32   0.13633E-03   0.13385E+10 0.88097E+03 
c  TempC        0.13438E+04      47   0.61720E-01   0.12868E+06 0.71012E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.395          50.468          3.6648          3.5334
v  Velocity[Y]            -7.3692          10.469     -0.00072346      0.00035471
v  Velocity[Z]            -23.363          18.488       -0.054495       -0.025184
v  ǁVelocityǁ            0.014013          50.494          3.7915          3.5711
v  Pressure               -1419.8          290.87          273.26          279.11
v  k                   3.8892e-09           3.052        0.018482        0.013254
v  omega                   0.8554      7.8181e+05          4942.5          2000.5
v  TempC                  -136.66          602.85          8.1915          6.0792
v  Density                0.40134           2.403          1.2686          1.2808
v  TurbVisc            9.7356e-14       0.0022886      1.4731e-05      2.1652e-05
v  CourantNb                    0          29.172         0.66251          0.4642
v  FourierNb            0.0024564          3.7452        0.022118        0.019858
v  total_pressure           99905      1.0162e+05       1.016e+05       1.016e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40707          2.1404          1.2135          1.2534


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018549          29.261         0.68463         0.48406


 TIME FOR THE TIME STEP               48:        0.77205E+02

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


 INSTANT    0.283000000E-02   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855142E-01
Smooth wall               5      225028        -0.110017531E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155877322E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70115E+02 0.41052E+01
   Friction velocity        uet   :  0.16868E-01 0.41524E+01
   Friction velocity        uk    :  0.17648E-01 0.12081E+01
   Dimensionless distance   yplus :  0.17096E+00 0.27375E+02
   Friction thermal sca.    tstar : -0.68643E+03 0.39623E+02
   Rough dim-less th. sca.  tplus :  0.12755E+00 0.11838E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     192050
   Nb of faces within the viscous sub-layer     :       4932
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19860E+00      25   0.17279E-01   0.27320E+02 0.14130E+03 
c  Velocity[X]                                      0.24353E+02 
c  Velocity[Y]                                      0.75116E+00 
c  Velocity[Z]                                      0.22157E+01 
c  Pressure     0.13653E-03     320   0.75326E-02   0.21383E+00 0.21790E+03 
c  k            0.29492E-02      17   0.70189E-03   0.11636E+01 0.10626E+04 
c  omega        0.16016E+03      32   0.11442E-03   0.97679E+09 0.75682E+03 
c  TempC        0.13640E+04      45   0.62143E-01   0.12937E+06 0.69807E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4503          51.269          3.6657          3.5362
v  Velocity[Y]            -8.0584          11.144     -0.00074654       0.0003334
v  Velocity[Z]            -23.093           18.54       -0.055623       -0.025624
v  ǁVelocityǁ            0.014563          51.328          3.7924           3.574
v  Pressure               -1428.9          285.18          267.33          273.16
v  k                   1.8618e-08          3.0782        0.019127        0.013708
v  omega                  0.39554      6.6293e+05          4916.6          1976.2
v  TempC                  -144.35           615.7          8.4494          6.3096
v  Density                0.40318          2.5876          1.2679          1.2804
v  TurbVisc            2.9808e-14       0.0022892      1.5238e-05      2.2408e-05
v  CourantNb                    0          31.265         0.66244          0.4645
v  FourierNb            0.0024563          3.7575        0.022601        0.020506
v  total_pressure           99896      1.0161e+05      1.0159e+05       1.016e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40776          2.0068          1.2119          1.2525


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01795          31.358         0.68505         0.48501


 TIME FOR THE TIME STEP               49:        0.75912E+02

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


 INSTANT    0.293000000E-02   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855162E-01
Smooth wall               5      225028         0.367920703E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876699E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71071E+02 0.42729E+01
   Friction velocity        uet   :  0.79408E-02 0.41436E+01
   Friction velocity        uk    :  0.11669E-01 0.12288E+01
   Dimensionless distance   yplus :  0.24949E+00 0.26341E+02
   Friction thermal sca.    tstar : -0.79617E+03 0.31822E+02
   Rough dim-less th. sca.  tplus :  0.18614E+00 0.11747E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     191225
   Nb of faces within the viscous sub-layer     :       4975
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19864E+00      25   0.17341E-01   0.27380E+02 0.14128E+03 
c  Velocity[X]                                      0.24499E+02 
c  Velocity[Y]                                      0.73812E+00 
c  Velocity[Z]                                      0.21427E+01 
c  Pressure     0.13550E-03     306   0.73146E-02   0.21239E+00 0.20007E+03 
c  k            0.29962E-02      17   0.70220E-03   0.11964E+01 0.10570E+04 
c  omega        0.15791E+03      33   0.11966E-03   0.76936E+09 0.67535E+03 
c  TempC        0.13837E+04      47   0.60156E-01   0.13130E+06 0.69004E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.427          50.456          3.6666           3.539
v  Velocity[Y]            -7.8214          10.568      -0.0007458      0.00032042
v  Velocity[Z]            -23.095          18.108       -0.056738       -0.026063
v  ǁVelocityǁ           0.0061928          50.508          3.7934          3.5769
v  Pressure               -1433.2           279.9          261.93           267.8
v  k                   1.6256e-08          3.1593        0.019781        0.014164
v  omega                   1.0423      5.1245e+05          4892.3          1953.5
v  TempC                  -149.92          598.43          8.7048          6.5396
v  Density                0.39735           2.742          1.2671          1.2799
v  TurbVisc            7.1795e-14       0.0022893       1.572e-05      2.3127e-05
v  CourantNb                    0          29.393         0.66239          0.4648
v  FourierNb            0.0024562          3.8038         0.02307        0.021132
v  total_pressure           99892       1.016e+05      1.0159e+05      1.0159e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41091          2.0137          1.2103          1.2516


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017824          29.482         0.68546         0.48593


 TIME FOR THE TIME STEP               50:        0.75284E+02

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


 INSTANT    0.303000000E-02   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855204E-01
Smooth wall               5      225028        -0.186131794E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155877487E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69755E+02 0.44335E+01
   Friction velocity        uet   :  0.11085E-01 0.41351E+01
   Friction velocity        uk    :  0.18611E-01 0.12205E+01
   Dimensionless distance   yplus :  0.21733E+00 0.26580E+02
   Friction thermal sca.    tstar : -0.57601E+03 0.25399E+02
   Rough dim-less th. sca.  tplus :  0.16215E+00 0.11768E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     190386
   Nb of faces within the viscous sub-layer     :       5021
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19867E+00      25   0.16845E-01   0.27549E+02 0.14153E+03 
c  Velocity[X]                                      0.24701E+02 
c  Velocity[Y]                                      0.72411E+00 
c  Velocity[Z]                                      0.21238E+01 
c  Pressure     0.13476E-03     320   0.73807E-02   0.21237E+00 0.22393E+03 
c  k            0.30403E-02      17   0.70268E-03   0.12283E+01 0.10512E+04 
c  omega        0.15597E+03      32   0.13408E-03   0.10288E+10 0.78375E+03 
c  TempC        0.14031E+04      45   0.57508E-01   0.13057E+06 0.67560E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4113          51.171          3.6675          3.5418
v  Velocity[Y]             -7.399          11.464     -0.00077463      0.00030797
v  Velocity[Z]            -22.605          18.016       -0.057873       -0.026501
v  ǁVelocityǁ             0.01074          51.232          3.7945          3.5798
v  Pressure               -1441.1           273.9          256.11          261.93
v  k                    1.475e-09          3.3137        0.020443        0.014622
v  omega                   1.1534      7.7944e+05          4871.2          1932.3
v  TempC                   -152.8          595.45          8.9605          6.7697
v  Density                0.40522          2.8661          1.2664          1.2795
v  TurbVisc            1.0509e-13       0.0022893      1.6178e-05       2.381e-05
v  CourantNb                    0          31.369         0.66234          0.4651
v  FourierNb            0.0024561          3.8369        0.023522        0.021738
v  total_pressure           99884       1.016e+05      1.0158e+05      1.0159e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40522          2.1022          1.2089          1.2508


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015599          31.462         0.68586         0.48683


 TIME FOR THE TIME STEP               51:        0.75921E+02

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


 INSTANT    0.313000000E-02   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855248E-01
Smooth wall               5      225028        -0.168778485E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155877043E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69414E+02 0.43025E+01
   Friction velocity        uet   :  0.10413E-01 0.42336E+01
   Friction velocity        uk    :  0.14195E-01 0.12106E+01
   Dimensionless distance   yplus :  0.15032E+00 0.26057E+02
   Friction thermal sca.    tstar : -0.69347E+03 0.19443E+02
   Rough dim-less th. sca.  tplus :  0.11215E+00 0.11721E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     189587
   Nb of faces within the viscous sub-layer     :       5078
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19871E+00      25   0.17511E-01   0.27355E+02 0.14086E+03 
c  Velocity[X]                                      0.24552E+02 
c  Velocity[Y]                                      0.72003E+00 
c  Velocity[Z]                                      0.20831E+01 
c  Pressure     0.13297E-03     319   0.73892E-02   0.21008E+00 0.21953E+03 
c  k            0.30813E-02      17   0.71376E-03   0.12644E+01 0.10477E+04 
c  omega        0.15466E+03      32   0.13291E-03   0.78827E+09 0.68907E+03 
c  TempC        0.14222E+04      46   0.57556E-01   0.12946E+06 0.66092E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3844          50.645          3.6684          3.5446
v  Velocity[Y]            -6.8686          10.694     -0.00076697      0.00029963
v  Velocity[Z]            -22.965          17.664       -0.058997       -0.026935
v  ǁVelocityǁ            0.011024          50.698          3.7955          3.5827
v  Pressure               -1444.9          268.22          250.51           256.3
v  k                   2.6575e-08          3.4802         0.02111        0.015079
v  omega                  0.30483      5.1734e+05            4851          1912.3
v  TempC                  -138.53          619.82          9.2172          6.9999
v  Density                0.40661          2.9347          1.2657           1.279
v  TurbVisc            1.4596e-14       0.0022893      1.6627e-05       2.449e-05
v  CourantNb                    0          29.477         0.66232          0.4654
v  FourierNb             0.002456          3.8605        0.023975        0.022348
v  total_pressure           99880      1.0159e+05      1.0158e+05      1.0158e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4079          2.3551          1.2074          1.2499


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016103          29.566         0.68629         0.48775


 TIME FOR THE TIME STEP               52:        0.75868E+02

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


 INSTANT    0.323000000E-02   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855302E-01
Smooth wall               5      225028        -0.558043991E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876107E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68952E+02 0.41052E+01
   Friction velocity        uet   :  0.93770E-02 0.41573E+01
   Friction velocity        uk    :  0.93062E-02 0.12314E+01
   Dimensionless distance   yplus :  0.20433E+00 0.26434E+02
   Friction thermal sca.    tstar : -0.10561E+04 0.19344E+02
   Rough dim-less th. sca.  tplus :  0.15245E+00 0.11755E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     188872
   Nb of faces within the viscous sub-layer     :       5014
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19873E+00      25   0.16432E-01   0.27370E+02 0.14072E+03 
c  Velocity[X]                                      0.24552E+02 
c  Velocity[Y]                                      0.69995E+00 
c  Velocity[Z]                                      0.21189E+01 
c  Pressure     0.13199E-03     301   0.73395E-02   0.20915E+00 0.20015E+03 
c  k            0.31214E-02      18   0.72571E-03   0.12991E+01 0.10438E+04 
c  omega        0.15287E+03      32   0.12115E-03   0.65227E+09 0.62963E+03 
c  TempC        0.14405E+04      47   0.57439E-01   0.13040E+06 0.65211E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3813          51.152          3.6693          3.5474
v  Velocity[Y]            -6.9394           11.29     -0.00076698      0.00029122
v  Velocity[Z]            -22.293          17.762       -0.060065       -0.027352
v  ǁVelocityǁ            0.010046           51.22          3.7968          3.5855
v  Pressure               -1451.4          263.29          245.46          251.27
v  k                   3.2808e-08          3.6586        0.021779        0.015536
v  omega                  0.39962      5.1446e+05          4829.7          1893.4
v  TempC                  -149.13          635.33          9.4713          7.2294
v  Density                0.39551          2.6236           1.265          1.2786
v  TurbVisc            1.8293e-13       0.0022893      1.7068e-05      2.5165e-05
v  CourantNb                    0          31.566         0.66231         0.46571
v  FourierNb            0.0024559          3.8774        0.024426        0.022959
v  total_pressure           99874      1.0159e+05      1.0157e+05      1.0158e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42217          2.6236           1.206           1.249


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014905          31.659         0.68674         0.48867


 TIME FOR THE TIME STEP               53:        0.74805E+02

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


 INSTANT    0.333000000E-02   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855350E-01
Smooth wall               5      225028         0.432775000E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875744E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69760E+02 0.42508E+01
   Friction velocity        uet   :  0.16529E-01 0.42043E+01
   Friction velocity        uk    :  0.17526E-01 0.12280E+01
   Dimensionless distance   yplus :  0.22603E+00 0.25603E+02
   Friction thermal sca.    tstar : -0.59419E+03 0.17608E+02
   Rough dim-less th. sca.  tplus :  0.16864E+00 0.11679E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     188171
   Nb of faces within the viscous sub-layer     :       5014
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19877E+00      25   0.16087E-01   0.27027E+02 0.13965E+03 
c  Velocity[X]                                      0.24365E+02 
c  Velocity[Y]                                      0.68082E+00 
c  Velocity[Z]                                      0.19812E+01 
c  Pressure     0.13289E-03     302   0.73501E-02   0.21079E+00 0.20279E+03 
c  k            0.31603E-02      17   0.72995E-03   0.13336E+01 0.10402E+04 
c  omega        0.15132E+03      32   0.11513E-03   0.57113E+09 0.59181E+03 
c  TempC        0.14584E+04      46   0.55793E-01   0.13017E+06 0.64096E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3193          50.491          3.6703          3.5502
v  Velocity[Y]            -6.9277          10.978     -0.00075441      0.00028638
v  Velocity[Z]            -23.168          17.422       -0.061143       -0.027776
v  ǁVelocityǁ           0.0095337           50.55           3.798          3.5884
v  Pressure               -1454.1          258.08          240.41          246.27
v  k                   3.5096e-09          3.9753        0.022447        0.015993
v  omega                   1.4741       3.051e+05          4809.3          1875.5
v  TempC                  -156.98          601.14          9.7264          7.4586
v  Density                0.38876          2.8478          1.2643          1.2781
v  TurbVisc            1.6151e-13       0.0022892       1.749e-05      2.5812e-05
v  CourantNb                    0          29.649         0.66233         0.46602
v  FourierNb            0.0024558          3.8894        0.024861        0.023554
v  total_pressure           99871      1.0158e+05      1.0157e+05      1.0157e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41752          2.8478          1.2046          1.2482


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014136          29.738         0.68719         0.48957


 TIME FOR THE TIME STEP               54:        0.74722E+02

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


 INSTANT    0.343000000E-02   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855386E-01
Smooth wall               5      225028        -0.503219445E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876431E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68857E+02 0.46627E+01
   Friction velocity        uet   :  0.92878E-02 0.41812E+01
   Friction velocity        uk    :  0.97117E-02 0.12548E+01
   Dimensionless distance   yplus :  0.11262E+00 0.26362E+02
   Friction thermal sca.    tstar : -0.74719E+03 0.18794E+02
   Rough dim-less th. sca.  tplus :  0.84030E-01 0.11748E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     187564
   Nb of faces within the viscous sub-layer     :       4991
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19881E+00      25   0.16947E-01   0.26670E+02 0.13855E+03 
c  Velocity[X]                                      0.24074E+02 
c  Velocity[Y]                                      0.66479E+00 
c  Velocity[Z]                                      0.19310E+01 
c  Pressure     0.12972E-03     302   0.72934E-02   0.20652E+00 0.21259E+03 
c  k            0.31999E-02      17   0.72980E-03   0.13717E+01 0.10383E+04 
c  omega        0.14998E+03      32   0.12567E-03   0.72693E+09 0.66993E+03 
c  TempC        0.14756E+04      46   0.53990E-01   0.13033E+06 0.63131E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2675           51.27          3.6713           3.553
v  Velocity[Y]            -6.7258            11.3     -0.00075076      0.00027972
v  Velocity[Z]            -23.378          17.605       -0.062216       -0.028192
v  ǁVelocityǁ           0.0076599           51.34          3.7994          3.5913
v  Pressure               -1460.5           253.1          235.29          241.14
v  k                   1.4501e-08          4.1077        0.023111        0.016451
v  omega                   1.1845      4.2572e+05            4791          1858.6
v  TempC                  -154.25          608.22          9.9805          7.6875
v  Density                0.40397          3.0403          1.2636          1.2777
v  TurbVisc            2.0239e-14       0.0022893      1.7906e-05      2.6459e-05
v  CourantNb                    0          31.564         0.66237         0.46633
v  FourierNb            0.0024558           3.898        0.025296        0.024154
v  total_pressure           99865      1.0158e+05      1.0156e+05      1.0157e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4124          3.0403          1.2033          1.2474


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01599          31.657         0.68767         0.49049


 TIME FOR THE TIME STEP               55:        0.74808E+02

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


 INSTANT    0.353000000E-02   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855412E-01
Smooth wall               5      225028        -0.125778790E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876813E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68667E+02 0.47084E+01
   Friction velocity        uet   :  0.11580E-01 0.42414E+01
   Friction velocity        uk    :  0.15525E-01 0.12537E+01
   Dimensionless distance   yplus :  0.17936E+00 0.26105E+02
   Friction thermal sca.    tstar : -0.59768E+03 0.13977E+02
   Rough dim-less th. sca.  tplus :  0.13382E+00 0.11725E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     186970
   Nb of faces within the viscous sub-layer     :       4983
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19884E+00      25   0.16486E-01   0.27164E+02 0.13965E+03 
c  Velocity[X]                                      0.24503E+02 
c  Velocity[Y]                                      0.68133E+00 
c  Velocity[Z]                                      0.19804E+01 
c  Pressure     0.12691E-03     305   0.70868E-02   0.20297E+00 0.22022E+03 
c  k            0.32406E-02      17   0.73758E-03   0.14096E+01 0.10366E+04 
c  omega        0.14882E+03      32   0.12965E-03   0.62374E+09 0.62279E+03 
c  TempC        0.14930E+04      45   0.52817E-01   0.12953E+06 0.61975E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2659           50.67          3.6724          3.5557
v  Velocity[Y]            -6.8559          10.954     -0.00070389      0.00028713
v  Velocity[Z]            -22.761          17.207       -0.063266       -0.028606
v  ǁVelocityǁ            0.010136          50.729          3.8008          3.5942
v  Pressure               -1461.5          247.94          230.13          235.94
v  k                   3.4744e-08          4.3443        0.023765        0.016907
v  omega                 0.077524      3.0606e+05          4774.2          1842.7
v  TempC                  -148.73          615.46          10.232          7.9165
v  Density                0.40072          2.9703          1.2629          1.2772
v  TurbVisc            7.2775e-14       0.0022892      1.8311e-05      2.7096e-05
v  CourantNb                    0          30.054         0.66243         0.46665
v  FourierNb            0.0024557          3.9042        0.025722        0.024747
v  total_pressure           99864      1.0157e+05      1.0156e+05      1.0156e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40789          2.9703           1.202          1.2466


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017065          30.143         0.68815          0.4914


 TIME FOR THE TIME STEP               56:        0.74266E+02

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


 INSTANT    0.363000000E-02   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855431E-01
Smooth wall               5      225028        -0.105673662E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876597E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67993E+02 0.44112E+01
   Friction velocity        uet   :  0.13286E-01 0.42364E+01
   Friction velocity        uk    :  0.14177E-01 0.12789E+01
   Dimensionless distance   yplus :  0.16268E+00 0.26991E+02
   Friction thermal sca.    tstar : -0.64375E+03 0.15175E+02
   Rough dim-less th. sca.  tplus :  0.12138E+00 0.11805E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     186384
   Nb of faces within the viscous sub-layer     :       4958
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19888E+00      24   0.16125E-01   0.26852E+02 0.13867E+03 
c  Velocity[X]                                      0.24274E+02 
c  Velocity[Y]                                      0.66083E+00 
c  Velocity[Z]                                      0.19169E+01 
c  Pressure     0.12600E-03     283   0.70207E-02   0.20195E+00 0.19101E+03 
c  k            0.32845E-02      17   0.75442E-03   0.14489E+01 0.10356E+04 
c  omega        0.14763E+03      32   0.14126E-03   0.65537E+09 0.64023E+03 
c  TempC        0.15102E+04      44   0.53901E-01   0.12910E+06 0.60956E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2012           51.21          3.6734          3.5585
v  Velocity[Y]            -7.1008          10.892     -0.00071728      0.00028144
v  Velocity[Z]            -23.297          17.078       -0.064289       -0.029009
v  ǁVelocityǁ            0.011199          51.284          3.8022          3.5971
v  Pressure               -1467.6          243.81          225.71          231.52
v  k                   2.5297e-09          4.4531         0.02441        0.017364
v  omega                 0.049411      3.2061e+05          4758.6          1827.6
v  TempC                   -153.2          607.77          10.482          8.1456
v  Density                0.39745          2.8386          1.2622          1.2767
v  TurbVisc             1.323e-13       0.0022893      1.8708e-05       2.772e-05
v  CourantNb                    0          31.536         0.66251         0.46697
v  FourierNb            0.0024557          3.9086        0.026143        0.025336
v  total_pressure           99857      1.0157e+05      1.0155e+05      1.0156e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39745          2.2783          1.2008          1.2458


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018853          31.628         0.68865          0.4923


 TIME FOR THE TIME STEP               57:        0.72746E+02

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


 INSTANT    0.373000000E-02   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855440E-01
Smooth wall               5      225028        -0.102943627E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874972E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69013E+02 0.44455E+01
   Friction velocity        uet   :  0.13232E-01 0.42406E+01
   Friction velocity        uk    :  0.17201E-01 0.12740E+01
   Dimensionless distance   yplus :  0.20297E+00 0.25714E+02
   Friction thermal sca.    tstar : -0.56659E+03 0.12795E+02
   Rough dim-less th. sca.  tplus :  0.15144E+00 0.11689E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     185795
   Nb of faces within the viscous sub-layer     :       4933
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19891E+00      25   0.16560E-01   0.26384E+02 0.13728E+03 
c  Velocity[X]                                      0.23821E+02 
c  Velocity[Y]                                      0.64105E+00 
c  Velocity[Z]                                      0.19222E+01 
c  Pressure     0.12349E-03     283   0.68805E-02   0.19783E+00 0.19121E+03 
c  k            0.33306E-02      17   0.76482E-03   0.14835E+01 0.10329E+04 
c  omega        0.14654E+03      32   0.11655E-03   0.50551E+09 0.56423E+03 
c  TempC        0.15270E+04      45   0.52617E-01   0.12968E+06 0.60221E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1251          50.548          3.6745          3.5613
v  Velocity[Y]            -7.2074          10.448     -0.00069936      0.00027907
v  Velocity[Z]            -23.271          17.475       -0.065297       -0.029409
v  ǁVelocityǁ            0.010022           50.61          3.8037             3.6
v  Pressure               -1470.1          239.24          221.32          227.17
v  k                    2.058e-09          4.6994        0.025044        0.017821
v  omega                  0.01472      3.0654e+05          4742.8          1813.2
v  TempC                  -157.43          610.46          10.729           8.374
v  Density                0.40093          2.9445          1.2616          1.2763
v  TurbVisc            1.2658e-14       0.0022892      1.9096e-05      2.8331e-05
v  CourantNb                    0          29.636         0.66259         0.46729
v  FourierNb            0.0024557          3.9117         0.02656        0.025918
v  total_pressure           99855      1.0156e+05      1.0155e+05      1.0155e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41041           2.106          1.1995           1.245


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017191          29.724         0.68915          0.4932


 TIME FOR THE TIME STEP               58:        0.72827E+02

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


 INSTANT    0.383000000E-02   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855446E-01
Smooth wall               5      225028        -0.894139805E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874669E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68558E+02 0.42477E+01
   Friction velocity        uet   :  0.90984E-02 0.42111E+01
   Friction velocity        uk    :  0.12949E-01 0.13004E+01
   Dimensionless distance   yplus :  0.24249E+00 0.25949E+02
   Friction thermal sca.    tstar : -0.80447E+03 0.12451E+02
   Rough dim-less th. sca.  tplus :  0.18092E+00 0.11711E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     185308
   Nb of faces within the viscous sub-layer     :       4886
   Total number of wall faces                   :     225028
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19895E+00      25   0.15913E-01   0.26663E+02 0.13783E+03 
c  Velocity[X]                                      0.24080E+02 
c  Velocity[Y]                                      0.65140E+00 
c  Velocity[Z]                                      0.19318E+01 
c  Pressure     0.12473E-03     270   0.69147E-02   0.20029E+00 0.18104E+03 
c  k            0.33782E-02      17   0.75761E-03   0.15119E+01 0.10281E+04 
c  omega        0.14548E+03      32   0.12743E-03   0.47969E+09 0.55120E+03 
c  TempC        0.15439E+04      46   0.49963E-01   0.12998E+06 0.59456E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1179          51.517          3.6756           3.564
v  Velocity[Y]            -7.1403          10.499     -0.00070626      0.00028106
v  Velocity[Z]            -22.405          16.939       -0.066274       -0.029807
v  ǁVelocityǁ           0.0076495          51.591          3.8054          3.6029
v  Pressure               -1475.9          235.16          217.24          223.13
v  k                   2.1429e-08          4.7964        0.025669        0.018278
v  omega                0.0048858      3.0709e+05          4728.1          1799.5
v  TempC                  -161.37          621.03          10.971          8.6021
v  Density                0.39971          3.0521          1.2609          1.2758
v  TurbVisc            1.8789e-14       0.0022896      1.9489e-05      2.8949e-05
v  CourantNb                    0          31.661          0.6627          0.4676
v  FourierNb            0.0024557           3.914         0.02698        0.026507
v  total_pressure           99849      1.0156e+05      1.0154e+05      1.0155e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4091          2.2131          1.1983          1.2442


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020882          31.754         0.68968         0.49411


 TIME FOR THE TIME STEP               59:        0.72024E+02

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


 INSTANT    0.393000000E-02   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855451E-01
Smooth wall               5      225028         0.440466149E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876294E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68754E+02 0.42427E+01
   Friction velocity        uet   :  0.13195E-01 0.42615E+01
   Friction velocity        uk    :  0.13256E-01 0.13008E+01
   Dimensionless distance   yplus :  0.28511E+00 0.25901E+02
   Friction thermal sca.    tstar : -0.60076E+03 0.96884E+01
   Rough dim-less th. sca.  tplus :  0.21272E+00 0.11706E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     184742
   Nb of faces within the viscous sub-layer     :       4789
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19899E+00      24   0.16256E-01   0.26536E+02 0.13733E+03 
c  Velocity[X]                                      0.24015E+02 
c  Velocity[Y]                                      0.63968E+00 
c  Velocity[Z]                                      0.18813E+01 
c  Pressure     0.12237E-03     283   0.67966E-02   0.19684E+00 0.20091E+03 
c  k            0.34250E-02      17   0.75463E-03   0.15396E+01 0.10236E+04 
c  omega        0.14453E+03      33   0.15580E-03   0.57293E+09 0.60384E+03 
c  TempC        0.15611E+04      45   0.49024E-01   0.12841E+06 0.58296E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.0408          50.971          3.6766          3.5668
v  Velocity[Y]             -6.925          10.029     -0.00069003      0.00028076
v  Velocity[Z]            -22.855          17.104       -0.067285       -0.030206
v  ǁVelocityǁ            0.011751          51.038          3.8069          3.6058
v  Pressure               -1476.9          230.78          212.88          218.73
v  k                   1.4407e-08          4.8964        0.026286        0.018735
v  omega                0.0012973      9.7517e+05          4713.9          1786.4
v  TempC                   -164.9          621.61          11.214          8.8308
v  Density                0.39498          3.1597          1.2603          1.2754
v  TurbVisc            2.7624e-13       0.0022898      1.9887e-05      2.9564e-05
v  CourantNb                    0          30.239         0.66282         0.46792
v  FourierNb            0.0024557          3.9239        0.027406        0.027099
v  total_pressure           99848      1.0156e+05      1.0154e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40793          2.3656          1.1971          1.2434


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021469          30.329         0.69022         0.49502


 TIME FOR THE TIME STEP               60:        0.72768E+02

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


 INSTANT    0.403000000E-02   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855453E-01
Smooth wall               5      225028         0.129870513E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875102E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68330E+02 0.41330E+01
   Friction velocity        uet   :  0.71353E-02 0.42589E+01
   Friction velocity        uk    :  0.11981E-01 0.13112E+01
   Dimensionless distance   yplus :  0.24440E+00 0.26850E+02
   Friction thermal sca.    tstar : -0.73171E+03 0.15306E+02
   Rough dim-less th. sca.  tplus :  0.18235E+00 0.11792E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     184157
   Nb of faces within the viscous sub-layer     :       4730
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19902E+00      26   0.16351E-01   0.26532E+02 0.13715E+03 
c  Velocity[X]                                      0.24073E+02 
c  Velocity[Y]                                      0.62756E+00 
c  Velocity[Z]                                      0.18315E+01 
c  Pressure     0.11847E-03     269   0.66703E-02   0.19097E+00 0.18577E+03 
c  k            0.34720E-02      17   0.76554E-03   0.15730E+01 0.10213E+04 
c  omega        0.14392E+03      32   0.16879E-03   0.96336E+09 0.78426E+03 
c  TempC        0.15782E+04      45   0.49556E-01   0.12796E+06 0.57420E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1017          51.109          3.6777          3.5695
v  Velocity[Y]            -6.6703          10.453      -0.0006877      0.00028044
v  Velocity[Z]            -22.953          17.375       -0.068255       -0.030599
v  ǁVelocityǁ            0.010241          51.188          3.8086          3.6087
v  Pressure               -1482.8          226.65          208.88          214.74
v  k                   1.3794e-08          5.0293        0.026895        0.019189
v  omega               0.00029518      7.0783e+05          4701.2            1774
v  TempC                  -167.99          623.59          11.452          9.0596
v  Density                0.39472          3.2626          1.2596          1.2749
v  TurbVisc             8.923e-14       0.0022897      2.0294e-05       3.019e-05
v  CourantNb                    0          31.698         0.66296         0.46825
v  FourierNb            0.0024557          3.9313        0.027842        0.027702
v  total_pressure           99842      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39472           2.073          1.1959          1.2427


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021253          31.791          0.6908         0.49595


 TIME FOR THE TIME STEP               61:        0.72086E+02

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


 INSTANT    0.413000000E-02   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855454E-01
Smooth wall               5      225028         0.110116249E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874867E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68823E+02 0.41980E+01
   Friction velocity        uet   :  0.62367E-02 0.42517E+01
   Friction velocity        uk    :  0.11642E-01 0.13159E+01
   Dimensionless distance   yplus :  0.19765E+00 0.25893E+02
   Friction thermal sca.    tstar : -0.80742E+03 0.70880E+01
   Rough dim-less th. sca.  tplus :  0.14747E+00 0.11706E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     183611
   Nb of faces within the viscous sub-layer     :       4653
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19905E+00      26   0.15498E-01   0.26289E+02 0.13634E+03 
c  Velocity[X]                                      0.23836E+02 
c  Velocity[Y]                                      0.62277E+00 
c  Velocity[Z]                                      0.18307E+01 
c  Pressure     0.11834E-03     264   0.65698E-02   0.19141E+00 0.17773E+03 
c  k            0.35171E-02      17   0.77473E-03   0.16051E+01 0.10188E+04 
c  omega        0.14359E+03      32   0.14479E-03   0.14993E+10 0.97901E+03 
c  TempC        0.15951E+04      46   0.48862E-01   0.12763E+06 0.56602E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1163          50.688          3.6787          3.5723
v  Velocity[Y]             -7.084          10.323     -0.00066428      0.00028432
v  Velocity[Z]            -22.315          16.822       -0.069229       -0.030989
v  ǁVelocityǁ           0.0061282          50.755          3.8102          3.6116
v  Pressure                 -1485          222.92          205.16          210.98
v  k                   2.6886e-08          5.1959        0.027503        0.019643
v  omega               5.5051e-05       1.537e+06          4688.5            1762
v  TempC                  -170.76          624.98          11.687          9.2885
v  Density                0.39385          3.3587           1.259          1.2745
v  TurbVisc            2.8845e-13       0.0022896      2.0707e-05      3.0817e-05
v  CourantNb                    0          29.686          0.6631         0.46857
v  FourierNb            0.0024557          3.9366        0.028284        0.028309
v  total_pressure           99840      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41141           2.225          1.1947          1.2419


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016682          29.775         0.69139         0.49688


 TIME FOR THE TIME STEP               62:        0.71759E+02

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


 INSTANT    0.423000000E-02   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855454E-01
Smooth wall               5      225028        -0.463453508E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873938E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66742E+02 0.43681E+01
   Friction velocity        uet   :  0.56842E-02 0.42265E+01
   Friction velocity        uk    :  0.14996E-01 0.13371E+01
   Dimensionless distance   yplus :  0.22726E+00 0.26573E+02
   Friction thermal sca.    tstar : -0.49558E+03 0.80414E+01
   Rough dim-less th. sca.  tplus :  0.16956E+00 0.11767E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     183097
   Nb of faces within the viscous sub-layer     :       4577
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19909E+00      25   0.15872E-01   0.25866E+02 0.13507E+03 
c  Velocity[X]                                      0.23463E+02 
c  Velocity[Y]                                      0.60999E+00 
c  Velocity[Z]                                      0.17927E+01 
c  Pressure     0.11504E-03     242   0.64840E-02   0.18662E+00 0.14479E+03 
c  k            0.35608E-02      17   0.77866E-03   0.16333E+01 0.10152E+04 
c  omega        0.14662E+03      32   0.13933E-03   0.85688E+09 0.74365E+03 
c  TempC        0.16118E+04      44   0.47971E-01   0.12820E+06 0.56011E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1499          51.559          3.6798           3.575
v  Velocity[Y]            -6.9562          9.9039     -0.00066782      0.00028887
v  Velocity[Z]            -23.004          16.775       -0.070201       -0.031375
v  ǁVelocityǁ           0.0037262          51.641          3.8119          3.6145
v  Pressure               -1490.7           220.2          202.14          207.97
v  k                    3.817e-08          5.1847        0.028111        0.020096
v  omega               6.2344e-06      7.9107e+05            4675          1750.5
v  TempC                  -173.43          610.74          11.921          9.5173
v  Density                0.39324          3.4495          1.2584          1.2741
v  TurbVisc            1.7079e-13       0.0022895      2.1126e-05      3.1447e-05
v  CourantNb                    0          31.788         0.66326         0.46889
v  FourierNb            0.0024557          3.9405        0.028733         0.02892
v  total_pressure           99834      1.0155e+05      1.0153e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4091          2.3092          1.1936          1.2412


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017568          31.881         0.69199         0.49781


 TIME FOR THE TIME STEP               63:        0.70118E+02

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


 INSTANT    0.433000000E-02   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855453E-01
Smooth wall               5      225028         0.168418817E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872063E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67771E+02 0.42143E+01
   Friction velocity        uet   :  0.92219E-02 0.42727E+01
   Friction velocity        uk    :  0.14579E-01 0.13281E+01
   Dimensionless distance   yplus :  0.20546E+00 0.26361E+02
   Friction thermal sca.    tstar : -0.48850E+03 0.93035E+01
   Rough dim-less th. sca.  tplus :  0.15330E+00 0.11748E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     182501
   Nb of faces within the viscous sub-layer     :       4535
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19912E+00      25   0.16187E-01   0.26194E+02 0.13575E+03 
c  Velocity[X]                                      0.23790E+02 
c  Velocity[Y]                                      0.60624E+00 
c  Velocity[Z]                                      0.17987E+01 
c  Pressure     0.11440E-03     232   0.64123E-02   0.18586E+00 0.13994E+03 
c  k            0.36013E-02      17   0.77977E-03   0.16528E+01 0.10091E+04 
c  omega        0.14178E+03      33   0.11395E-03   0.52320E+09 0.58307E+03 
c  TempC        0.16285E+04      45   0.46650E-01   0.12843E+06 0.55369E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1624          50.935          3.6809          3.5778
v  Velocity[Y]            -7.1392          10.146     -0.00065807      0.00028973
v  Velocity[Z]            -23.045           16.97       -0.071166       -0.031764
v  ǁVelocityǁ           0.0062929          51.011          3.8137          3.6174
v  Pressure               -1490.6          217.27          199.22           205.1
v  k                   2.8002e-08          5.3174        0.028722        0.020549
v  omega               6.3515e-09      5.3858e+05          4662.9          1739.6
v  TempC                  -175.94          591.56          12.154          9.7461
v  Density                0.39958          3.5417          1.2577          1.2736
v  TurbVisc            2.4173e-13       0.0022895      2.1561e-05      3.2093e-05
v  CourantNb                    0          30.299         0.66343         0.46921
v  FourierNb            0.0024557          3.9433        0.029194        0.029542
v  total_pressure           99834      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41156          2.1679          1.1925          1.2404


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016094           30.39         0.69263         0.49876


 TIME FOR THE TIME STEP               64:        0.69442E+02

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


 INSTANT    0.443000000E-02   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855452E-01
Smooth wall               5      225028         0.666019618E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875305E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64736E+02 0.46842E+01
   Friction velocity        uet   :  0.80428E-02 0.42787E+01
   Friction velocity        uk    :  0.14699E-01 0.13459E+01
   Dimensionless distance   yplus :  0.18801E+00 0.26973E+02
   Friction thermal sca.    tstar : -0.55520E+03 0.10045E+02
   Rough dim-less th. sca.  tplus :  0.14027E+00 0.11803E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     181979
   Nb of faces within the viscous sub-layer     :       4473
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19916E+00      25   0.15973E-01   0.26240E+02 0.13569E+03 
c  Velocity[X]                                      0.23820E+02 
c  Velocity[Y]                                      0.61276E+00 
c  Velocity[Z]                                      0.18072E+01 
c  Pressure     0.11404E-03     228   0.64065E-02   0.18562E+00 0.13356E+03 
c  k            0.36388E-02      17   0.78433E-03   0.16793E+01 0.10054E+04 
c  omega        0.14052E+03      32   0.11148E-03   0.35067E+09 0.47872E+03 
c  TempC        0.16449E+04      45   0.47053E-01   0.12743E+06 0.54487E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.173          51.339          3.6821          3.5805
v  Velocity[Y]             -6.661          10.113     -0.00065375      0.00029528
v  Velocity[Z]            -22.151          16.879       -0.072085       -0.032145
v  ǁVelocityǁ           0.0098205          51.418          3.8156          3.6204
v  Pressure               -1495.8           214.5          196.52           202.4
v  k                   2.7792e-08          5.3482        0.029336           0.021
v  omega               6.4694e-10      5.3337e+05            4651            1729
v  TempC                  -178.42          607.83          12.386          9.9749
v  Density                0.40844          3.6333          1.2571          1.2732
v  TurbVisc            1.1839e-13       0.0022893      2.2008e-05      3.2754e-05
v  CourantNb                    0          31.851         0.66365         0.46955
v  FourierNb            0.0024558          3.9453        0.029663        0.030174
v  total_pressure           99829      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40925          2.2651          1.1914          1.2397


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017271          31.945         0.69331         0.49972


 TIME FOR THE TIME STEP               65:        0.69182E+02

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


 INSTANT    0.453000000E-02   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855452E-01
Smooth wall               5      225028        -0.591297760E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872139E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65974E+02 0.47915E+01
   Friction velocity        uet   :  0.44834E-02 0.42787E+01
   Friction velocity        uk    :  0.59653E-02 0.13424E+01
   Dimensionless distance   yplus :  0.20502E+00 0.27300E+02
   Friction thermal sca.    tstar : -0.13065E+04 0.12901E+02
   Rough dim-less th. sca.  tplus :  0.15297E+00 0.11832E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     181428
   Nb of faces within the viscous sub-layer     :       4390
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19919E+00      24   0.15634E-01   0.26134E+02 0.13525E+03 
c  Velocity[X]                                      0.23751E+02 
c  Velocity[Y]                                      0.61445E+00 
c  Velocity[Z]                                      0.17684E+01 
c  Pressure     0.11182E-03     214   0.61764E-02   0.18217E+00 0.12482E+03 
c  k            0.36727E-02      17   0.79088E-03   0.17134E+01 0.10042E+04 
c  omega        0.13966E+03      32   0.13972E-03   0.48532E+09 0.56440E+03 
c  TempC        0.16609E+04      46   0.45623E-01   0.12793E+06 0.53951E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1671          50.939          3.6833          3.5833
v  Velocity[Y]            -6.9584          9.9958     -0.00064857       0.0002975
v  Velocity[Z]            -22.905          16.649       -0.073052       -0.032533
v  ǁVelocityǁ            0.012891           51.01          3.8175          3.6233
v  Pressure               -1496.4          211.99             194           199.9
v  k                   2.0664e-08           5.362        0.029955        0.021449
v  omega               6.8303e-11       3.122e+05          4640.4            1719
v  TempC                   -180.9          605.27          12.618          10.204
v  Density                 0.4009          3.7285          1.2565          1.2727
v  TurbVisc            1.6042e-13       0.0022894      2.2465e-05      3.3431e-05
v  CourantNb                    0          30.208         0.66384         0.46987
v  FourierNb            0.0024558          3.9467         0.03014        0.030814
v  total_pressure           99829      1.0154e+05      1.0152e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40974          2.3314          1.1904           1.239


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018098          30.299         0.69398         0.50069


 TIME FOR THE TIME STEP               66:        0.68219E+02

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


 INSTANT    0.463000000E-02   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855451E-01
Smooth wall               5      225028        -0.104180508E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874348E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64819E+02 0.46382E+01
   Friction velocity        uet   :  0.93885E-02 0.42685E+01
   Friction velocity        uk    :  0.15357E-01 0.13463E+01
   Dimensionless distance   yplus :  0.27387E+00 0.27211E+02
   Friction thermal sca.    tstar : -0.50903E+03 0.17727E+02
   Rough dim-less th. sca.  tplus :  0.20434E+00 0.11824E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     180776
   Nb of faces within the viscous sub-layer     :       4319
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19923E+00      25   0.16042E-01   0.25874E+02 0.13440E+03 
c  Velocity[X]                                      0.23536E+02 
c  Velocity[Y]                                      0.60482E+00 
c  Velocity[Z]                                      0.17333E+01 
c  Pressure     0.11093E-03     195   0.62949E-02   0.18118E+00 0.10332E+03 
c  k            0.37036E-02      17   0.79813E-03   0.17472E+01 0.10029E+04 
c  omega        0.13904E+03      32   0.11356E-03   0.38942E+09 0.50669E+03 
c  TempC        0.16766E+04      46   0.45434E-01   0.12766E+06 0.53274E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.194          51.549          3.6845           3.586
v  Velocity[Y]            -6.6068           9.981     -0.00065026      0.00030012
v  Velocity[Z]            -22.937          17.056       -0.073989       -0.032913
v  ǁVelocityǁ           0.0090639          51.634          3.8195          3.6262
v  Pressure               -1500.9          209.94          191.97          197.86
v  k                   8.0307e-09           5.438        0.030583        0.021899
v  omega               1.6476e-11      3.0774e+05          4629.8          1709.3
v  TempC                  -183.44          606.47          12.849          10.432
v  Density                0.40207          3.8287          1.2559          1.2723
v  TurbVisc            1.2901e-13       0.0022894      2.2921e-05      3.4107e-05
v  CourantNb                    0          31.789          0.6641         0.47021
v  FourierNb            0.0024559          3.9478        0.030612        0.031449
v  total_pressure           99824      1.0153e+05      1.0152e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41542          2.4408          1.1893          1.2383


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017412          31.884         0.69471         0.50166


 TIME FOR THE TIME STEP               67:        0.67021E+02

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


 INSTANT    0.473000000E-02   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.446476427E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873912E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63936E+02 0.43748E+01
   Friction velocity        uet   :  0.73935E-02 0.42949E+01
   Friction velocity        uk    :  0.14304E-01 0.13470E+01
   Dimensionless distance   yplus :  0.19855E+00 0.27709E+02
   Friction thermal sca.    tstar : -0.57646E+03 0.23974E+02
   Rough dim-less th. sca.  tplus :  0.14814E+00 0.11867E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     180275
   Nb of faces within the viscous sub-layer     :       4262
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19926E+00      25   0.15545E-01   0.26079E+02 0.13476E+03 
c  Velocity[X]                                      0.23706E+02 
c  Velocity[Y]                                      0.60010E+00 
c  Velocity[Z]                                      0.17720E+01 
c  Pressure     0.11066E-03     195   0.61277E-02   0.18105E+00 0.97710E+02 
c  k            0.37300E-02      17   0.80350E-03   0.17780E+01 0.10006E+04 
c  omega        0.13838E+03      32   0.15648E-03   0.39708E+09 0.51264E+03 
c  TempC        0.16921E+04      45   0.44010E-01   0.12889E+06 0.52931E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1879          51.004          3.6857          3.5888
v  Velocity[Y]            -6.8641          10.153     -0.00062905      0.00030437
v  Velocity[Z]            -22.785          16.433        -0.07493       -0.033291
v  ǁVelocityǁ           0.0098459          51.084          3.8216          3.6292
v  Pressure               -1500.7          207.94          190.04          195.94
v  k                   4.9641e-09          5.5084        0.031217        0.022348
v  omega               4.3349e-12      3.0794e+05          4620.8          1700.1
v  TempC                  -185.92          611.25          13.081          10.661
v  Density                0.40152           3.937          1.2553          1.2718
v  TurbVisc            5.0507e-14       0.0022895      2.3382e-05      3.4786e-05
v  CourantNb                    0          30.393         0.66436         0.47055
v  FourierNb            0.0024559          3.9485        0.031093        0.032085
v  total_pressure           99824      1.0153e+05      1.0152e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42025          2.5208          1.1883          1.2376


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011232          30.484         0.69545         0.50263


 TIME FOR THE TIME STEP               68:        0.66955E+02

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


 INSTANT    0.483000000E-02   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.307390527E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873014E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62263E+02 0.43928E+01
   Friction velocity        uet   :  0.71861E-02 0.42889E+01
   Friction velocity        uk    :  0.18680E-01 0.13614E+01
   Dimensionless distance   yplus :  0.28696E+00 0.27554E+02
   Friction thermal sca.    tstar : -0.59508E+03 0.31774E+02
   Rough dim-less th. sca.  tplus :  0.21410E+00 0.11854E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     179662
   Nb of faces within the viscous sub-layer     :       4164
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19930E+00      24   0.15648E-01   0.26096E+02 0.13463E+03 
c  Velocity[X]                                      0.23795E+02 
c  Velocity[Y]                                      0.59676E+00 
c  Velocity[Z]                                      0.17037E+01 
c  Pressure     0.11147E-03     194   0.62664E-02   0.18240E+00 0.95094E+02 
c  k            0.37530E-02      17   0.81157E-03   0.18027E+01 0.99677E+03 
c  omega        0.13778E+03      33   0.12405E-03   0.37065E+09 0.49627E+03 
c  TempC        0.17072E+04      46   0.44540E-01   0.12788E+06 0.52140E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2375          51.588           3.687          3.5915
v  Velocity[Y]            -6.7295          9.8955      -0.0006259      0.00030767
v  Velocity[Z]            -23.043          16.871       -0.075874       -0.033673
v  ǁVelocityǁ             0.01166          51.675          3.8237          3.6321
v  Pressure               -1505.1          206.19          188.18           194.1
v  k                   1.6851e-08          5.5168        0.031857        0.022797
v  omega               1.6212e-12      3.0812e+05          4611.5          1691.1
v  TempC                  -188.45          600.49          13.313          10.889
v  Density                0.39935          4.0488          1.2547          1.2714
v  TurbVisc            3.0726e-14       0.0022893      2.3844e-05      3.5471e-05
v  CourantNb                    0          31.889         0.66463         0.47088
v  FourierNb             0.002456           3.949         0.03157        0.032721
v  total_pressure           99820      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40559          2.3337          1.1873          1.2369


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011607          31.983          0.6962         0.50361


 TIME FOR THE TIME STEP               69:        0.66858E+02

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


 INSTANT    0.493000000E-02   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.865530316E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872296E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63267E+02 0.45495E+01
   Friction velocity        uet   :  0.50218E-02 0.43042E+01
   Friction velocity        uk    :  0.11428E-01 0.13564E+01
   Dimensionless distance   yplus :  0.25722E+00 0.27753E+02
   Friction thermal sca.    tstar : -0.68765E+03 0.30892E+02
   Rough dim-less th. sca.  tplus :  0.19191E+00 0.11871E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     179063
   Nb of faces within the viscous sub-layer     :       4094
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19934E+00      25   0.16162E-01   0.25792E+02 0.13368E+03 
c  Velocity[X]                                      0.23505E+02 
c  Velocity[Y]                                      0.59132E+00 
c  Velocity[Z]                                      0.16961E+01 
c  Pressure     0.10914E-03     191   0.61442E-02   0.17861E+00 0.93019E+02 
c  k            0.37739E-02      17   0.81941E-03   0.18312E+01 0.99422E+03 
c  omega        0.13717E+03      33   0.12128E-03   0.37522E+09 0.50011E+03 
c  TempC        0.17216E+04      45   0.43594E-01   0.12864E+06 0.51733E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2922          50.809          3.6883          3.5942
v  Velocity[Y]             -6.924          9.6887     -0.00061357       0.0003084
v  Velocity[Z]            -23.027          16.879       -0.076782       -0.034046
v  ǁVelocityǁ           0.0072536          51.011          3.8258          3.6351
v  Pressure               -1505.1          204.21          186.39          192.31
v  k                   7.7756e-09          5.6149        0.032498        0.023243
v  omega                8.114e-13      3.2805e+05          4603.3          1682.5
v  TempC                  -190.78          617.31          13.547          11.117
v  Density                0.40427          4.1698          1.2541          1.2709
v  TurbVisc            8.8615e-14       0.0022896      2.4316e-05      3.6175e-05
v  CourantNb                    0          30.417         0.66491         0.47122
v  FourierNb            0.0024561          3.9494        0.032053        0.033366
v  total_pressure           99820      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41366          2.3939          1.1863          1.2362


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015974          30.508         0.69696         0.50459


 TIME FOR THE TIME STEP               70:        0.66803E+02

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


 INSTANT    0.503000000E-02   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.633421687E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870667E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61216E+02 0.44502E+01
   Friction velocity        uet   :  0.51856E-02 0.42806E+01
   Friction velocity        uk    :  0.19271E-01 0.13692E+01
   Dimensionless distance   yplus :  0.24983E+00 0.27934E+02
   Friction thermal sca.    tstar : -0.51227E+03 0.38084E+02
   Rough dim-less th. sca.  tplus :  0.18640E+00 0.11886E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     178447
   Nb of faces within the viscous sub-layer     :       4058
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19937E+00      25   0.15704E-01   0.26274E+02 0.13475E+03 
c  Velocity[X]                                      0.23862E+02 
c  Velocity[Y]                                      0.60779E+00 
c  Velocity[Z]                                      0.18042E+01 
c  Pressure     0.11046E-03     191   0.62493E-02   0.18135E+00 0.91391E+02 
c  k            0.37952E-02      17   0.82272E-03   0.18635E+01 0.99288E+03 
c  omega        0.13672E+03      32   0.15579E-03   0.84674E+09 0.75120E+03 
c  TempC        0.17357E+04      45   0.42820E-01   0.12865E+06 0.51193E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2895          51.685          3.6897           3.597
v  Velocity[Y]            -6.6508          9.6196     -0.00060496      0.00031279
v  Velocity[Z]            -22.617          16.927       -0.077699       -0.034421
v  ǁVelocityǁ            0.019119          51.774          3.8281           3.638
v  Pressure               -1509.9          202.72          184.63          190.57
v  k                   4.3213e-09          5.6006        0.033134        0.023689
v  omega               4.3853e-13       6.042e+05          4596.7          1674.4
v  TempC                  -192.67           605.9           13.78          11.345
v  Density                0.39663          4.2876          1.2535          1.2705
v  TurbVisc            2.8637e-14         0.00229      2.4791e-05       3.689e-05
v  CourantNb                    0           31.87         0.66522         0.47157
v  FourierNb            0.0024562          3.9497        0.032534        0.034011
v  total_pressure           99815      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41094          2.4612          1.1853          1.2355


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015357          31.965         0.69775         0.50558


 TIME FOR THE TIME STEP               71:        0.66453E+02

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


 INSTANT    0.513000000E-02   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.905950055E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871597E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62245E+02 0.44329E+01
   Friction velocity        uet   :  0.69353E-02 0.42997E+01
   Friction velocity        uk    :  0.18038E-01 0.13605E+01
   Dimensionless distance   yplus :  0.24049E+00 0.28636E+02
   Friction thermal sca.    tstar : -0.47490E+03 0.21889E+02
   Rough dim-less th. sca.  tplus :  0.17943E+00 0.11945E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     177850
   Nb of faces within the viscous sub-layer     :       4023
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19941E+00      25   0.15416E-01   0.26009E+02 0.13390E+03 
c  Velocity[X]                                      0.23689E+02 
c  Velocity[Y]                                      0.60435E+00 
c  Velocity[Z]                                      0.17158E+01 
c  Pressure     0.10968E-03     175   0.61684E-02   0.18028E+00 0.73626E+02 
c  k            0.38187E-02      17   0.82882E-03   0.18996E+01 0.99278E+03 
c  omega        0.13838E+03      32   0.20603E-03   0.75292E+09 0.70927E+03 
c  TempC        0.17494E+04      44   0.41778E-01   0.12755E+06 0.50452E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3339          51.143          3.6911          3.5997
v  Velocity[Y]            -6.8303          9.9939     -0.00056782      0.00032154
v  Velocity[Z]            -23.068          16.465       -0.078616       -0.034799
v  ǁVelocityǁ            0.018205          51.236          3.8304          3.6409
v  Pressure               -1509.3           201.4          183.23          189.19
v  k                   3.6684e-09          5.6488        0.033758        0.024132
v  omega               2.8812e-13      1.0373e+06          4590.4          1666.5
v  TempC                  -193.86          596.06          14.015          11.573
v  Density                0.40178          4.3883          1.2529            1.27
v  TurbVisc            2.5326e-14       0.0022899      2.5274e-05      3.7623e-05
v  CourantNb                    0          30.461         0.66554         0.47192
v  FourierNb            0.0024563          3.9499        0.033015        0.034662
v  total_pressure           99816      1.0153e+05      1.0151e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41522           2.526          1.1844          1.2348


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01149          30.552         0.69856         0.50658


 TIME FOR THE TIME STEP               72:        0.64519E+02

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


 INSTANT    0.523000000E-02   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.155127933E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871292E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60535E+02 0.49673E+01
   Friction velocity        uet   :  0.38539E-02 0.42991E+01
   Friction velocity        uk    :  0.15905E-01 0.13701E+01
   Dimensionless distance   yplus :  0.17760E+00 0.28497E+02
   Friction thermal sca.    tstar : -0.38124E+03 0.26628E+02
   Rough dim-less th. sca.  tplus :  0.13251E+00 0.11934E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     177319
   Nb of faces within the viscous sub-layer     :       4002
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19944E+00      25   0.16330E-01   0.25766E+02 0.13310E+03 
c  Velocity[X]                                      0.23484E+02 
c  Velocity[Y]                                      0.60104E+00 
c  Velocity[Z]                                      0.16810E+01 
c  Pressure     0.10841E-03     176   0.59987E-02   0.17845E+00 0.80196E+02 
c  k            0.38487E-02      17   0.83719E-03   0.19354E+01 0.99278E+03 
c  omega        0.13629E+03      32   0.16529E-03   0.53254E+09 0.59748E+03 
c  TempC        0.17631E+04      45   0.41513E-01   0.12731E+06 0.49898E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3654          51.618          3.6926          3.6024
v  Velocity[Y]            -6.5599          9.2924      -0.0005816      0.00031748
v  Velocity[Z]            -22.993          16.775       -0.079527       -0.035171
v  ǁVelocityǁ            0.018416          51.712          3.8327          3.6439
v  Pressure               -1513.9          199.77          181.71          187.68
v  k                   2.3036e-08          5.6476        0.034366        0.024571
v  omega               1.9463e-13      6.7467e+05          4584.3          1658.9
v  TempC                  -194.43          598.74          14.247          11.801
v  Density                0.40633          4.4543          1.2523          1.2696
v  TurbVisc            1.7788e-14       0.0022898      2.5762e-05      3.8374e-05
v  CourantNb                    0          32.024         0.66588         0.47226
v  FourierNb            0.0024564            3.95        0.033496        0.035318
v  total_pressure           99811      1.0152e+05      1.0151e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40916          2.6009          1.1834          1.2342


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014118          32.119         0.69938         0.50758


 TIME FOR THE TIME STEP               73:        0.64606E+02

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


 INSTANT    0.533000000E-02   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.320967479E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870659E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60425E+02 0.53768E+01
   Friction velocity        uet   :  0.36503E-02 0.43091E+01
   Friction velocity        uk    :  0.18525E-01 0.13652E+01
   Dimensionless distance   yplus :  0.37029E+00 0.28616E+02
   Friction thermal sca.    tstar : -0.42971E+03 0.34244E+02
   Rough dim-less th. sca.  tplus :  0.27628E+00 0.11944E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     176637
   Nb of faces within the viscous sub-layer     :       3940
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19947E+00      25   0.15221E-01   0.26054E+02 0.13367E+03 
c  Velocity[X]                                      0.23722E+02 
c  Velocity[Y]                                      0.58711E+00 
c  Velocity[Z]                                      0.17445E+01 
c  Pressure     0.10838E-03     173   0.60289E-02   0.17852E+00 0.76909E+02 
c  k            0.38853E-02      16   0.84328E-03   0.19669E+01 0.99178E+03 
c  omega        0.13540E+03      33   0.15773E-03   0.44392E+09 0.54628E+03 
c  TempC        0.17766E+04      46   0.42006E-01   0.12657E+06 0.49262E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4017          51.273           3.694          3.6051
v  Velocity[Y]            -6.9056          9.8875     -0.00056905      0.00031945
v  Velocity[Z]            -23.083          16.131       -0.080426       -0.035543
v  ǁVelocityǁ           0.0099115          51.356          3.8351          3.6469
v  Pressure               -1513.7          198.37          180.28          186.25
v  k                   5.6069e-08          5.6264        0.034956         0.02501
v  omega               1.5749e-13      5.6801e+05          4578.2          1651.5
v  TempC                  -169.38          597.37          14.475          12.029
v  Density                0.40508          4.4866          1.2517          1.2692
v  TurbVisc            1.1156e-13       0.0022896       2.625e-05      3.9123e-05
v  CourantNb                    0          30.464         0.66622         0.47261
v  FourierNb            0.0024565          3.9501         0.03397        0.035967
v  total_pressure           99811      1.0152e+05      1.0151e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40508          2.6818          1.1825          1.2335


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013912          30.556         0.70019         0.50858


 TIME FOR THE TIME STEP               74:        0.64485E+02

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


 INSTANT    0.543000000E-02   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.166217592E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869775E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59130E+02 0.50745E+01
   Friction velocity        uet   :  0.50142E-02 0.43027E+01
   Friction velocity        uk    :  0.12712E-01 0.13698E+01
   Dimensionless distance   yplus :  0.23333E+00 0.29430E+02
   Friction thermal sca.    tstar : -0.72958E+03 0.33282E+02
   Rough dim-less th. sca.  tplus :  0.17409E+00 0.12011E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     176056
   Nb of faces within the viscous sub-layer     :       3890
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19951E+00      25   0.15413E-01   0.25575E+02 0.13227E+03 
c  Velocity[X]                                      0.23287E+02 
c  Velocity[Y]                                      0.58622E+00 
c  Velocity[Z]                                      0.17019E+01 
c  Pressure     0.10696E-03     149   0.60435E-02   0.17641E+00 0.50957E+02 
c  k            0.39298E-02      17   0.84637E-03   0.19988E+01 0.99078E+03 
c  omega        0.13492E+03      33   0.16307E-03   0.38173E+09 0.50721E+03 
c  TempC        0.17902E+04      44   0.40592E-01   0.12769E+06 0.49009E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4392          51.695          3.6954          3.6079
v  Velocity[Y]            -6.8436          9.5401     -0.00058642       0.0003193
v  Velocity[Z]            -22.955          16.589        -0.08134       -0.035913
v  ǁVelocityǁ            0.013881          51.797          3.8375          3.6498
v  Pressure               -1517.5          197.62          179.37          185.32
v  k                   1.2446e-07          5.7565        0.035531        0.025449
v  omega               1.4227e-13      5.5209e+05          4572.2          1644.4
v  TempC                  -170.79          609.17          14.699          12.255
v  Density                0.40571          3.4034          1.2511          1.2687
v  TurbVisc            3.1418e-13       0.0022896      2.6732e-05      3.9867e-05
v  CourantNb                    0          32.121         0.66657         0.47296
v  FourierNb            0.0024567          3.9502        0.034436        0.036607
v  total_pressure           99808      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40988          2.6982          1.1816          1.2328


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011532          32.217         0.70101         0.50957


 TIME FOR THE TIME STEP               75:        0.62903E+02

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


 INSTANT    0.553000000E-02   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.352558685E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867574E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60559E+02 0.46634E+01
   Friction velocity        uet   :  0.34039E-02 0.43187E+01
   Friction velocity        uk    :  0.21338E-01 0.13771E+01
   Dimensionless distance   yplus :  0.30279E+00 0.29225E+02
   Friction thermal sca.    tstar : -0.39311E+03 0.40909E+02
   Rough dim-less th. sca.  tplus :  0.22591E+00 0.11994E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     175487
   Nb of faces within the viscous sub-layer     :       3824
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19954E+00      25   0.16513E-01   0.25780E+02 0.13263E+03 
c  Velocity[X]                                      0.23511E+02 
c  Velocity[Y]                                      0.58366E+00 
c  Velocity[Z]                                      0.16857E+01 
c  Pressure     0.10840E-03     158   0.60249E-02   0.17886E+00 0.52353E+02 
c  k            0.39794E-02      17   0.84179E-03   0.20201E+01 0.98707E+03 
c  omega        0.13444E+03      33   0.10943E-03   0.36239E+09 0.49477E+03 
c  TempC        0.18043E+04      46   0.39529E-01   0.12754E+06 0.48522E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4482          51.166          3.6968          3.6106
v  Velocity[Y]            -7.0155          9.3782     -0.00054143      0.00033177
v  Velocity[Z]            -23.371            16.8        -0.08224       -0.036278
v  ǁVelocityǁ            0.011659          51.462          3.8399          3.6528
v  Pressure               -1516.4          196.67          178.36          184.36
v  k                   6.4892e-08          5.6937        0.036091        0.025888
v  omega               1.6367e-13      5.5058e+05            4566          1637.4
v  TempC                  -171.78          622.09           14.92          12.482
v  Density                0.40029          3.4504          1.2506          1.2683
v  TurbVisc            4.5571e-13       0.0022895      2.7219e-05      4.0611e-05
v  CourantNb                    0          30.622         0.66692         0.47331
v  FourierNb            0.0024568          3.9503        0.034903        0.037246
v  total_pressure           99809      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40695          2.7071          1.1807          1.2322


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.0143          30.714         0.70182         0.51055


 TIME FOR THE TIME STEP               76:        0.63546E+02

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


 INSTANT    0.563000000E-02   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.232289951E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869068E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57779E+02 0.47402E+01
   Friction velocity        uet   :  0.46131E-02 0.43107E+01
   Friction velocity        uk    :  0.15975E-01 0.13757E+01
   Dimensionless distance   yplus :  0.25907E+00 0.29208E+02
   Friction thermal sca.    tstar : -0.46783E+03 0.24547E+02
   Rough dim-less th. sca.  tplus :  0.19329E+00 0.11993E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     174836
   Nb of faces within the viscous sub-layer     :       3749
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19957E+00      25   0.15372E-01   0.26323E+02 0.13385E+03 
c  Velocity[X]                                      0.23965E+02 
c  Velocity[Y]                                      0.59809E+00 
c  Velocity[Z]                                      0.17600E+01 
c  Pressure     0.10829E-03     157   0.60827E-02   0.17921E+00 0.51687E+02 
c  k            0.40325E-02      17   0.84441E-03   0.20401E+01 0.98325E+03 
c  omega        0.13406E+03      32   0.12024E-03   0.34964E+09 0.48653E+03 
c  TempC        0.18187E+04      45   0.39379E-01   0.12666E+06 0.47904E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4279          51.786          3.6982          3.6133
v  Velocity[Y]            -6.7344          9.4472     -0.00054163      0.00033391
v  Velocity[Z]            -23.202          16.672       -0.083153       -0.036649
v  ǁVelocityǁ           0.0099119          51.883          3.8423          3.6557
v  Pressure               -1520.2          195.64          177.38          183.43
v  k                   1.1265e-07          5.7921        0.036638        0.026325
v  omega               2.0675e-13       5.517e+05            4560          1630.7
v  TempC                  -160.98          606.35          15.136           12.71
v  Density                0.39451          3.4841            1.25          1.2678
v  TurbVisc            3.5161e-13       0.0022893      2.7727e-05       4.138e-05
v  CourantNb                    0          32.152         0.66728         0.47366
v  FourierNb            0.0024569          3.9626        0.035384        0.037903
v  total_pressure           99805      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41756          2.7143          1.1798          1.2315


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013301          32.248         0.70266         0.51156


 TIME FOR THE TIME STEP               77:        0.63409E+02

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


 INSTANT    0.573000000E-02   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.247947744E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868666E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59062E+02 0.47445E+01
   Friction velocity        uet   :  0.37040E-02 0.43192E+01
   Friction velocity        uk    :  0.19585E-01 0.13754E+01
   Dimensionless distance   yplus :  0.22992E+00 0.29282E+02
   Friction thermal sca.    tstar : -0.41840E+03 0.23021E+02
   Rough dim-less th. sca.  tplus :  0.17155E+00 0.11999E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     174273
   Nb of faces within the viscous sub-layer     :       3696
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19960E+00      24   0.15554E-01   0.25651E+02 0.13197E+03 
c  Velocity[X]                                      0.23380E+02 
c  Velocity[Y]                                      0.57876E+00 
c  Velocity[Z]                                      0.16919E+01 
c  Pressure     0.10660E-03     155   0.60900E-02   0.17632E+00 0.56540E+02 
c  k            0.40870E-02      17   0.85306E-03   0.20604E+01 0.97992E+03 
c  omega        0.13365E+03      33   0.12383E-03   0.35911E+09 0.49354E+03 
c  TempC        0.18335E+04      46   0.38992E-01   0.12556E+06 0.47257E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4263          51.309          3.6995           3.616
v  Velocity[Y]            -6.8539          9.2278     -0.00052468      0.00033702
v  Velocity[Z]            -23.421          16.456       -0.084046       -0.037013
v  ǁVelocityǁ           0.0092973          51.484          3.8446          3.6587
v  Pressure               -1519.5          194.51          176.33           182.4
v  k                    1.048e-07          5.8418        0.037175        0.026758
v  omega               3.1467e-13      5.4435e+05          4554.6          1624.1
v  TempC                  -137.04          586.93           15.35          12.938
v  Density                0.40157          3.1486          1.2495          1.2674
v  TurbVisc            5.7496e-13       0.0022893       2.825e-05      4.2171e-05
v  CourantNb                    0          30.627         0.66763           0.474
v  FourierNb            0.0024571          4.0194        0.035875        0.038574
v  total_pressure           99805      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41863           2.695           1.179          1.2309


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015184           30.72         0.70351         0.51258


 TIME FOR THE TIME STEP               78:        0.63214E+02

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


 INSTANT    0.583000000E-02   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.563276054E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868816E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58588E+02 0.47026E+01
   Friction velocity        uet   :  0.27531E-02 0.43118E+01
   Friction velocity        uk    :  0.16863E-01 0.13852E+01
   Dimensionless distance   yplus :  0.18020E+00 0.29518E+02
   Friction thermal sca.    tstar : -0.44050E+03 0.28396E+02
   Rough dim-less th. sca.  tplus :  0.13445E+00 0.12018E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     173688
   Nb of faces within the viscous sub-layer     :       3620
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19964E+00      25   0.15392E-01   0.25443E+02 0.13127E+03 
c  Velocity[X]                                      0.23171E+02 
c  Velocity[Y]                                      0.57379E+00 
c  Velocity[Z]                                      0.16981E+01 
c  Pressure     0.10645E-03     153   0.60024E-02   0.17654E+00 0.53895E+02 
c  k            0.41436E-02      17   0.85794E-03   0.20842E+01 0.97770E+03 
c  omega        0.13328E+03      32   0.17104E-03   0.47869E+09 0.57025E+03 
c  TempC        0.18484E+04      46   0.38984E-01   0.12508E+06 0.46743E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4158          52.101          3.7009          3.6187
v  Velocity[Y]             -6.534          9.7229     -0.00054897      0.00032973
v  Velocity[Z]            -23.221          16.777       -0.084953       -0.037379
v  ǁVelocityǁ           0.0092731          52.199           3.847          3.6617
v  Pressure               -1523.1          193.99          175.37          181.43
v  k                   2.2563e-08          5.8238        0.037705        0.027187
v  omega               5.5899e-13      3.6202e+05          4549.7          1617.8
v  TempC                  -131.38          604.29           15.56          13.165
v  Density                0.41064          2.5949          1.2489          1.2669
v  TurbVisc            3.5686e-13       0.0022898      2.8781e-05      4.2968e-05
v  CourantNb                    0          32.186         0.66799         0.47435
v  FourierNb            0.0024573           4.063        0.036367        0.039248
v  total_pressure           99802      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41064          2.5949          1.1781          1.2303


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013848          32.282         0.70436          0.5136


 TIME FOR THE TIME STEP               79:        0.63207E+02

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


 INSTANT    0.593000000E-02   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.112103965E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867903E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57273E+02 0.47296E+01
   Friction velocity        uet   :  0.50145E-02 0.43406E+01
   Friction velocity        uk    :  0.69605E-02 0.13794E+01
   Dimensionless distance   yplus :  0.16640E+00 0.30410E+02
   Friction thermal sca.    tstar : -0.13163E+04 0.34709E+02
   Rough dim-less th. sca.  tplus :  0.12415E+00 0.12089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     172974
   Nb of faces within the viscous sub-layer     :       3561
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19967E+00      25   0.15606E-01   0.25455E+02 0.13113E+03 
c  Velocity[X]                                      0.23162E+02 
c  Velocity[Y]                                      0.57696E+00 
c  Velocity[Z]                                      0.17166E+01 
c  Pressure     0.10500E-03     136   0.58819E-02   0.17404E+00 0.39458E+02 
c  k            0.41994E-02      16   0.84501E-03   0.21030E+01 0.97437E+03 
c  omega        0.13293E+03      33   0.15964E-03   0.37680E+09 0.50652E+03 
c  TempC        0.18635E+04      44   0.38384E-01   0.12586E+06 0.46479E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4193          51.365          3.7022          3.6214
v  Velocity[Y]            -6.7184          9.3766     -0.00053048      0.00033382
v  Velocity[Z]             -23.66          16.142       -0.085837       -0.037736
v  ǁVelocityǁ           0.0099164          51.651          3.8493          3.6647
v  Pressure               -1522.3          193.15          174.68          180.73
v  k                   5.6453e-08          5.7893        0.038232        0.027616
v  omega               1.2192e-12      3.3752e+05          4544.2          1611.6
v  TempC                   -125.4          606.48          15.766          13.392
v  Density                0.40251          2.4912          1.2484          1.2665
v  TurbVisc            7.6519e-14       0.0022901       2.932e-05      4.3771e-05
v  CourantNb                    0          30.824         0.66835          0.4747
v  FourierNb            0.0024574          4.0963        0.036864        0.039925
v  total_pressure           99803      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40361          2.4912          1.1773          1.2296


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012998          30.917         0.70522         0.51463


 TIME FOR THE TIME STEP               80:        0.62426E+02

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


 INSTANT    0.603000000E-02   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.164854019E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866143E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56611E+02 0.48834E+01
   Friction velocity        uet   :  0.88989E-03 0.43223E+01
   Friction velocity        uk    :  0.12170E-01 0.13807E+01
   Dimensionless distance   yplus :  0.14590E+00 0.30196E+02
   Friction thermal sca.    tstar : -0.62949E+03 0.43138E+02
   Rough dim-less th. sca.  tplus :  0.10886E+00 0.12072E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     172353
   Nb of faces within the viscous sub-layer     :       3511
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19970E+00      24   0.15840E-01   0.25629E+02 0.13141E+03 
c  Velocity[X]                                      0.23399E+02 
c  Velocity[Y]                                      0.58054E+00 
c  Velocity[Z]                                      0.16491E+01 
c  Pressure     0.10446E-03     131   0.59723E-02   0.17319E+00 0.34108E+02 
c  k            0.42531E-02      17   0.82594E-03   0.21200E+01 0.97078E+03 
c  omega        0.13260E+03      33   0.12298E-03   0.28818E+09 0.44351E+03 
c  TempC        0.18790E+04      44   0.38188E-01   0.12538E+06 0.45988E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3599          51.782          3.7035          3.6241
v  Velocity[Y]            -6.5732          9.2381     -0.00054955      0.00033062
v  Velocity[Z]            -23.493          16.725       -0.086727       -0.038094
v  ǁVelocityǁ           0.0094697          51.898          3.8517          3.6676
v  Pressure               -1525.5          192.57           174.1          180.13
v  k                   8.6834e-08          5.8709         0.03876        0.028043
v  omega               3.0224e-12      3.1202e+05          4538.4          1605.6
v  TempC                  -142.98          593.88          15.971           13.62
v  Density                0.40151          2.3904          1.2479          1.2661
v  TurbVisc            4.9574e-13         0.00229      2.9871e-05      4.4586e-05
v  CourantNb                    0          32.238         0.66872         0.47505
v  FourierNb            0.0024576          4.1216         0.03737         0.04061
v  total_pressure           99800      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41483          2.3904          1.1765           1.229


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01514          32.335         0.70609         0.51566


 TIME FOR THE TIME STEP               81:        0.62076E+02

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


 INSTANT    0.613000000E-02   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.107305488E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155864373E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58652E+02 0.47337E+01
   Friction velocity        uet   :  0.71086E-02 0.43359E+01
   Friction velocity        uk    :  0.14926E-01 0.13845E+01
   Dimensionless distance   yplus :  0.23340E+00 0.30943E+02
   Friction thermal sca.    tstar : -0.50389E+03 0.25606E+02
   Rough dim-less th. sca.  tplus :  0.17414E+00 0.12130E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     171689
   Nb of faces within the viscous sub-layer     :       3455
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19974E+00      25   0.15477E-01   0.25600E+02 0.13117E+03 
c  Velocity[X]                                      0.23336E+02 
c  Velocity[Y]                                      0.57474E+00 
c  Velocity[Z]                                      0.16886E+01 
c  Pressure     0.10528E-03     123   0.58101E-02   0.17450E+00 0.20123E+02 
c  k            0.43008E-02      16   0.81606E-03   0.21416E+01 0.96840E+03 
c  omega        0.13222E+03      33   0.12118E-03   0.31368E+09 0.46308E+03 
c  TempC        0.18946E+04      45   0.37726E-01   0.12512E+06 0.45548E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3204          51.488          3.7048          3.6268
v  Velocity[Y]            -6.6496          9.3293     -0.00052727      0.00033277
v  Velocity[Z]            -23.892          16.685        -0.08764       -0.038464
v  ǁVelocityǁ            0.011997          51.809           3.854          3.6706
v  Pressure               -1523.9          192.25          173.77          179.79
v  k                   1.2133e-08          5.8889        0.039289        0.028468
v  omega               8.9751e-12      3.1194e+05          4533.6          1599.8
v  TempC                     -168          584.71          16.174          13.847
v  Density                0.40735          2.7133          1.2474          1.2656
v  TurbVisc            6.3601e-13       0.0022898       3.043e-05      4.5407e-05
v  CourantNb                    0          30.736          0.6691          0.4754
v  FourierNb            0.0024578          4.1408        0.037879        0.041297
v  total_pressure           99801      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42056          2.2956          1.1757          1.2284


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016748           30.83         0.70698          0.5167


 TIME FOR THE TIME STEP               82:        0.61474E+02

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


 INSTANT    0.623000000E-02   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.258719230E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155861431E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56304E+02 0.48986E+01
   Friction velocity        uet   :  0.12307E-02 0.43326E+01
   Friction velocity        uk    :  0.21666E-01 0.13930E+01
   Dimensionless distance   yplus :  0.26200E+00 0.30734E+02
   Friction thermal sca.    tstar : -0.40484E+03 0.24506E+02
   Rough dim-less th. sca.  tplus :  0.19548E+00 0.12114E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     171046
   Nb of faces within the viscous sub-layer     :       3405
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19977E+00      25   0.15236E-01   0.25410E+02 0.13052E+03 
c  Velocity[X]                                      0.23129E+02 
c  Velocity[Y]                                      0.56312E+00 
c  Velocity[Z]                                      0.17179E+01 
c  Pressure     0.10549E-03     120   0.59526E-02   0.17531E+00 0.73292E+01 
c  k            0.43420E-02      17   0.83134E-03   0.21670E+01 0.96690E+03 
c  omega        0.13195E+03      32   0.11344E-03   0.38367E+09 0.51243E+03 
c  TempC        0.19103E+04      45   0.37775E-01   0.12491E+06 0.45127E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2367          52.095           3.706          3.6295
v  Velocity[Y]            -6.6092          9.1516     -0.00053292      0.00033348
v  Velocity[Z]            -23.374          16.698       -0.088554       -0.038834
v  ǁVelocityǁ            0.013534          52.196          3.8563          3.6736
v  Pressure               -1526.6          192.26          173.75          179.78
v  k                   1.6619e-08          5.9297        0.039828        0.028892
v  omega               3.1041e-11       3.113e+05          4529.5          1594.2
v  TempC                  -132.07          595.16          16.375          14.075
v  Density                 0.4117           3.359          1.2468          1.2652
v  TurbVisc            4.9648e-14       0.0022895      3.0992e-05      4.6234e-05
v  CourantNb                    0          32.407         0.66947         0.47574
v  FourierNb             0.002458          4.1553        0.038389        0.041988
v  total_pressure           99798      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4148          2.2776          1.1749          1.2278


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012778          32.504         0.70786         0.51773


 TIME FOR THE TIME STEP               83:        0.61643E+02

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


 INSTANT    0.633000000E-02   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.583722099E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155857616E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56202E+02 0.48749E+01
   Friction velocity        uet   :  0.61837E-02 0.43485E+01
   Friction velocity        uk    :  0.11409E-01 0.13907E+01
   Dimensionless distance   yplus :  0.21591E+00 0.30766E+02
   Friction thermal sca.    tstar : -0.76239E+03 0.30540E+02
   Rough dim-less th. sca.  tplus :  0.16109E+00 0.12116E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     170347
   Nb of faces within the viscous sub-layer     :       3351
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19980E+00      25   0.15969E-01   0.25360E+02 0.13023E+03 
c  Velocity[X]                                      0.23133E+02 
c  Velocity[Y]                                      0.56866E+00 
c  Velocity[Z]                                      0.16583E+01 
c  Pressure     0.10486E-03     125   0.58968E-02   0.17415E+00 0.10776E+02 
c  k            0.43739E-02      16   0.85666E-03   0.21869E+01 0.96405E+03 
c  omega        0.13167E+03      33   0.11481E-03   0.36176E+09 0.49791E+03 
c  TempC        0.19259E+04      44   0.37036E-01   0.12566E+06 0.44889E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2785           51.63          3.7073          3.6322
v  Velocity[Y]            -6.8171          9.1561      -0.0005238      0.00033385
v  Velocity[Z]            -23.785          16.508       -0.089461       -0.039191
v  ǁVelocityǁ            0.014895          51.965          3.8587          3.6765
v  Pressure               -1524.5          192.22          173.63          179.74
v  k                    1.837e-08          6.0252        0.040377        0.029315
v  omega               1.2213e-10      4.5953e+05            4525          1588.7
v  TempC                  -146.23          614.23          16.576          14.303
v  Density                0.40675          2.5034          1.2463          1.2647
v  TurbVisc            8.7689e-14       0.0022895      3.1552e-05       4.706e-05
v  CourantNb                    0          30.893         0.66983         0.47609
v  FourierNb            0.0024582          4.1662          0.0389        0.042676
v  total_pressure           99800      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40987          2.3396          1.1741          1.2272


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012737          30.987         0.70873         0.51877


 TIME FOR THE TIME STEP               84:        0.61955E+02

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


 INSTANT    0.643000000E-02   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.907371345E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155858984E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55008E+02 0.48985E+01
   Friction velocity        uet   :  0.41360E-02 0.43430E+01
   Friction velocity        uk    :  0.21786E-01 0.14070E+01
   Dimensionless distance   yplus :  0.23680E+00 0.31507E+02
   Friction thermal sca.    tstar : -0.46970E+03 0.37920E+02
   Rough dim-less th. sca.  tplus :  0.17668E+00 0.12173E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     169679
   Nb of faces within the viscous sub-layer     :       3334
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19984E+00      25   0.15611E-01   0.25859E+02 0.13134E+03 
c  Velocity[X]                                      0.23618E+02 
c  Velocity[Y]                                      0.58363E+00 
c  Velocity[Z]                                      0.16578E+01 
c  Pressure     0.10487E-03     122   0.60201E-02   0.17442E+00 0.99484E+01 
c  k            0.43969E-02      17   0.87283E-03   0.21955E+01 0.95864E+03 
c  omega        0.13148E+03      33   0.13184E-03   0.33898E+09 0.48226E+03 
c  TempC        0.19410E+04      46   0.37402E-01   0.12642E+06 0.44659E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2497          52.047          3.7086          3.6349
v  Velocity[Y]              -6.55          9.2995     -0.00052118      0.00033547
v  Velocity[Z]            -23.786          16.852       -0.090369       -0.039548
v  ǁVelocityǁ            0.011107          52.217          3.8611          3.6795
v  Pressure               -1527.1          192.03           173.5          179.65
v  k                   1.7913e-08          6.0357        0.040941        0.029739
v  omega               5.6024e-10      3.1235e+05          4521.2          1583.4
v  TempC                  -121.26          596.28          16.778           14.53
v  Density                0.39801          2.7826          1.2458          1.2643
v  TurbVisc            9.6845e-14       0.0022893       3.211e-05      4.7881e-05
v  CourantNb                    0          32.381         0.67022         0.47644
v  FourierNb            0.0024583          4.1745        0.039405        0.043359
v  total_pressure           99798      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41577          1.9883          1.1733          1.2266


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01779          32.478         0.70962          0.5198


 TIME FOR THE TIME STEP               85:        0.61924E+02

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


 INSTANT    0.653000000E-02   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.256621383E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155859053E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56907E+02 0.48652E+01
   Friction velocity        uet   :  0.48080E-02 0.43597E+01
   Friction velocity        uk    :  0.57842E-02 0.14016E+01
   Dimensionless distance   yplus :  0.79995E-01 0.31318E+02
   Friction thermal sca.    tstar : -0.13208E+04 0.47798E+02
   Rough dim-less th. sca.  tplus :  0.59685E-01 0.12159E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     169024
   Nb of faces within the viscous sub-layer     :       3295
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19988E+00      24   0.15387E-01   0.25644E+02 0.13063E+03 
c  Velocity[X]                                      0.23362E+02 
c  Velocity[Y]                                      0.58031E+00 
c  Velocity[Z]                                      0.17015E+01 
c  Pressure     0.10382E-03     119   0.57900E-02   0.17273E+00 0.10093E+02 
c  k            0.44112E-02      16   0.87758E-03   0.22036E+01 0.95338E+03 
c  omega        0.13117E+03      33   0.11434E-03   0.56134E+09 0.62034E+03 
c  TempC        0.19556E+04      46   0.36738E-01   0.12588E+06 0.44203E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4002          51.499            3.71          3.6376
v  Velocity[Y]            -6.6701          9.4568     -0.00050632      0.00033892
v  Velocity[Z]            -24.225          16.215       -0.091267       -0.039909
v  ǁVelocityǁ            0.016256          51.828          3.8635          3.6825
v  Pressure               -1525.9           191.5          173.36          179.52
v  k                   1.4322e-08           6.085        0.041515        0.030159
v  omega                2.922e-09      5.5993e+05          4518.1          1578.3
v  TempC                  -133.14           586.7           16.98          14.758
v  Density                0.40622          2.3252          1.2453          1.2639
v  TurbVisc            9.4369e-14       0.0022893      3.2657e-05      4.8691e-05
v  CourantNb                    0          30.898         0.67061          0.4768
v  FourierNb            0.0024585          4.1806        0.039905        0.044032
v  total_pressure           99799      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41239          2.0648          1.1725           1.226


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.019105          30.992         0.71052         0.52083


 TIME FOR THE TIME STEP               86:        0.61508E+02

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


 INSTANT    0.663000000E-02   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.118788296E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155857720E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55305E+02 0.49515E+01
   Friction velocity        uet   :  0.45502E-02 0.43306E+01
   Friction velocity        uk    :  0.18543E-01 0.14120E+01
   Dimensionless distance   yplus :  0.21102E+00 0.31454E+02
   Friction thermal sca.    tstar : -0.45778E+03 0.23270E+02
   Rough dim-less th. sca.  tplus :  0.15744E+00 0.12169E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     168299
   Nb of faces within the viscous sub-layer     :       3273
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19991E+00      24   0.15441E-01   0.25588E+02 0.13032E+03 
c  Velocity[X]                                      0.23314E+02 
c  Velocity[Y]                                      0.56736E+00 
c  Velocity[Z]                                      0.17065E+01 
c  Pressure     0.10385E-03     121   0.58965E-02   0.17320E+00 0.76598E+01 
c  k            0.44226E-02      17   0.87082E-03   0.22226E+01 0.95077E+03 
c  omega        0.13112E+03      32   0.29137E-03   0.55265E+09 0.61561E+03 
c  TempC        0.19697E+04      44   0.36109E-01   0.12533E+06 0.43757E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3186          52.148          3.7113          3.6403
v  Velocity[Y]            -6.5675          8.9783     -0.00051393      0.00033565
v  Velocity[Z]            -23.755          16.841       -0.092188       -0.040275
v  ǁVelocityǁ            0.016479          52.256           3.866          3.6855
v  Pressure               -1527.7          191.92          173.35           179.5
v  k                   1.1416e-08          6.1739        0.042094        0.030576
v  omega               3.6159e-08      1.0796e+06            4515          1573.2
v  TempC                  -116.77          594.21          17.185          14.986
v  Density                0.41075          2.5226          1.2448          1.2634
v  TurbVisc            7.5404e-14       0.0022893      3.3211e-05      4.9523e-05
v  CourantNb                    0          32.376         0.67101         0.47715
v  FourierNb            0.0024587          4.1853        0.040403        0.044715
v  total_pressure           99797      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41256          2.1522          1.1718          1.2254


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015497          32.474         0.71141         0.52187


 TIME FOR THE TIME STEP               87:        0.61562E+02

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


 INSTANT    0.673000000E-02   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.104636614E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155857602E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55436E+02 0.48912E+01
   Friction velocity        uet   :  0.23202E-02 0.43664E+01
   Friction velocity        uk    :  0.52099E-02 0.14147E+01
   Dimensionless distance   yplus :  0.11485E+00 0.31766E+02
   Friction thermal sca.    tstar : -0.18115E+04 0.26989E+02
   Rough dim-less th. sca.  tplus :  0.85692E-01 0.12192E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     167627
   Nb of faces within the viscous sub-layer     :       3259
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19995E+00      25   0.15931E-01   0.25525E+02 0.13000E+03 
c  Velocity[X]                                      0.23294E+02 
c  Velocity[Y]                                      0.56391E+00 
c  Velocity[Z]                                      0.16673E+01 
c  Pressure     0.10434E-03     125   0.59436E-02   0.17392E+00 0.10766E+02 
c  k            0.44342E-02      17   0.85844E-03   0.22474E+01 0.94965E+03 
c  omega        0.13107E+03      33   0.13419E-03   0.39735E+09 0.52239E+03 
c  TempC        0.19833E+04      46   0.36137E-01   0.12491E+06 0.43345E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4699          51.908          3.7127           3.643
v  Velocity[Y]            -6.5299          8.7514     -0.00051534      0.00033323
v  Velocity[Z]            -24.031          16.891       -0.093108       -0.040637
v  ǁVelocityǁ            0.016616          52.256          3.8685          3.6885
v  Pressure               -1524.9          191.76          173.17          179.35
v  k                   6.8335e-09          6.1534         0.04267         0.03099
v  omega               3.1506e-07      6.9092e+05          4511.8          1568.3
v  TempC                  -123.23          623.32          17.392          15.213
v  Density                0.40719          2.2585          1.2443           1.263
v  TurbVisc            6.0072e-14       0.0022897      3.3761e-05       5.036e-05
v  CourantNb                    0          31.018         0.67141         0.47751
v  FourierNb            0.0024589          4.1888        0.040898        0.045395
v  total_pressure           99800      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40851          2.2585          1.1711          1.2248


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01442          31.112         0.71231         0.52291


 TIME FOR THE TIME STEP               88:        0.62043E+02

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


 INSTANT    0.683000000E-02   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.172546528E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155859143E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53308E+02 0.50299E+01
   Friction velocity        uet   :  0.33215E-02 0.43645E+01
   Friction velocity        uk    :  0.13506E-01 0.14164E+01
   Dimensionless distance   yplus :  0.24624E+00 0.32739E+02
   Friction thermal sca.    tstar : -0.55034E+03 0.32914E+02
   Rough dim-less th. sca.  tplus :  0.18372E+00 0.12264E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     166913
   Nb of faces within the viscous sub-layer     :       3216
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19999E+00      25   0.15568E-01   0.25600E+02 0.13003E+03 
c  Velocity[X]                                      0.23358E+02 
c  Velocity[Y]                                      0.56870E+00 
c  Velocity[Z]                                      0.16737E+01 
c  Pressure     0.10378E-03     118   0.59300E-02   0.17306E+00 0.73390E+01 
c  k            0.44505E-02      17   0.85998E-03   0.22782E+01 0.94995E+03 
c  omega        0.13066E+03      33   0.22674E-03   0.47597E+09 0.57184E+03 
c  TempC        0.19965E+04      44   0.34916E-01   0.12511E+06 0.43050E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3851          52.171          3.7142          3.6457
v  Velocity[Y]            -6.5364          8.8062     -0.00052326       0.0003345
v  Velocity[Z]            -23.875          16.873       -0.094021       -0.041002
v  ǁVelocityǁ            0.016623           52.44          3.8711          3.6915
v  Pressure               -1526.2          191.91          173.17          179.35
v  k                   2.7966e-09          6.2521        0.043241        0.031401
v  omega               2.5929e-06      5.7393e+05          4508.9          1563.6
v  TempC                   -126.8           606.7          17.597           15.44
v  Density                0.39397          2.3558          1.2438          1.2625
v  TurbVisc            3.5945e-14         0.00229      3.4308e-05      5.1197e-05
v  CourantNb                    0          32.552         0.67183         0.47787
v  FourierNb            0.0024591          4.1914        0.041387        0.046073
v  total_pressure           99799      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39397          2.3558          1.1703          1.2242


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014572           32.65         0.71321         0.52395


 TIME FOR THE TIME STEP               89:        0.61594E+02

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


 INSTANT    0.693000000E-02   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.155995863E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856115E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54992E+02 0.49517E+01
   Friction velocity        uet   :  0.12790E-02 0.43850E+01
   Friction velocity        uk    :  0.17432E-01 0.14194E+01
   Dimensionless distance   yplus :  0.20404E+00 0.32395E+02
   Friction thermal sca.    tstar : -0.58372E+03 0.41556E+02
   Rough dim-less th. sca.  tplus :  0.15223E+00 0.12239E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     166284
   Nb of faces within the viscous sub-layer     :       3207
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20002E+00      26   0.15234E-01   0.25610E+02 0.12989E+03 
c  Velocity[X]                                      0.23343E+02 
c  Velocity[Y]                                      0.56786E+00 
c  Velocity[Z]                                      0.16988E+01 
c  Pressure     0.10400E-03     119   0.58036E-02   0.17323E+00 0.76100E+01 
c  k            0.44728E-02      17   0.87697E-03   0.23076E+01 0.94999E+03 
c  omega        0.13046E+03      33   0.17986E-03   0.58415E+09 0.63348E+03 
c  TempC        0.20097E+04      46   0.35167E-01   0.12348E+06 0.42448E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.5279          51.973          3.7156          3.6484
v  Velocity[Y]            -6.6115          8.7553     -0.00050796      0.00033458
v  Velocity[Z]            -24.279           16.54       -0.094926       -0.041357
v  ǁVelocityǁ             0.01712          52.319          3.8736          3.6945
v  Pressure               -1523.2          191.96          173.23          179.41
v  k                    2.658e-09          6.1485        0.043799         0.03181
v  omega               2.3048e-05       7.732e+05          4506.3          1558.9
v  TempC                  -141.04          591.17          17.804          15.667
v  Density                0.40141          2.4133          1.2433          1.2621
v  TurbVisc            1.4706e-14       0.0022901      3.4848e-05      5.2028e-05
v  CourantNb                    0          31.059         0.67224         0.47823
v  FourierNb            0.0024593          4.1933        0.041864         0.04674
v  total_pressure           99802      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40829          2.4133          1.1696          1.2236


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016696          31.153         0.71411         0.52497


 TIME FOR THE TIME STEP               90:        0.61839E+02

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


 INSTANT    0.703000000E-02   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.232919107E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155854655E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54164E+02 0.50200E+01
   Friction velocity        uet   :  0.45747E-02 0.43686E+01
   Friction velocity        uk    :  0.18540E-01 0.14149E+01
   Dimensionless distance   yplus :  0.25728E+00 0.32420E+02
   Friction thermal sca.    tstar : -0.40021E+03 0.19588E+02
   Rough dim-less th. sca.  tplus :  0.19196E+00 0.12241E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     165547
   Nb of faces within the viscous sub-layer     :       3176
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20005E+00      25   0.15819E-01   0.25409E+02 0.12922E+03 
c  Velocity[X]                                      0.23136E+02 
c  Velocity[Y]                                      0.57406E+00 
c  Velocity[Z]                                      0.16992E+01 
c  Pressure     0.10411E-03     122   0.58794E-02   0.17369E+00 0.16366E+02 
c  k            0.45026E-02      17   0.89375E-03   0.23381E+01 0.95015E+03 
c  omega        0.13051E+03      32   0.26217E-03   0.20639E+10 0.11850E+04 
c  TempC        0.20227E+04      46   0.35306E-01   0.12419E+06 0.42256E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4107          52.238          3.7171          3.6511
v  Velocity[Y]            -6.4838          8.9349     -0.00050584      0.00033736
v  Velocity[Z]            -24.003          16.959       -0.095841       -0.041716
v  ǁVelocityǁ            0.014115          52.468          3.8762          3.6975
v  Pressure               -1524.2          192.34          173.49          179.67
v  k                   1.0007e-08          6.2084        0.044346        0.032218
v  omega               0.00024354      1.4296e+06          4504.8          1554.5
v  TempC                  -171.01          596.89          18.009          15.894
v  Density                0.40863          2.6735          1.2428          1.2617
v  TurbVisc            1.3974e-14       0.0022901      3.5382e-05      5.2849e-05
v  CourantNb                    0          32.602         0.67267         0.47859
v  FourierNb            0.0024595          4.1948        0.042331        0.047396
v  total_pressure           99801      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41539          2.0189          1.1689          1.2231


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01549            32.7         0.71501         0.52599


 TIME FOR THE TIME STEP               91:        0.61871E+02

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


 INSTANT    0.713000000E-02   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.336845428E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852902E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54492E+02 0.50478E+01
   Friction velocity        uet   :  0.88232E-03 0.43957E+01
   Friction velocity        uk    :  0.20840E-01 0.14160E+01
   Dimensionless distance   yplus :  0.28424E+00 0.33327E+02
   Friction thermal sca.    tstar : -0.40983E+03 0.23330E+02
   Rough dim-less th. sca.  tplus :  0.21207E+00 0.12307E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     164938
   Nb of faces within the viscous sub-layer     :       3198
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20009E+00      25   0.15472E-01   0.25461E+02 0.12919E+03 
c  Velocity[X]                                      0.23151E+02 
c  Velocity[Y]                                      0.57432E+00 
c  Velocity[Z]                                      0.17357E+01 
c  Pressure     0.10313E-03     118   0.58200E-02   0.17217E+00 0.16770E+02 
c  k            0.45363E-02      17   0.89081E-03   0.23538E+01 0.94711E+03 
c  omega        0.13874E+03      33   0.16240E-03   0.76876E+09 0.72636E+03 
c  TempC        0.20359E+04      45   0.34615E-01   0.12507E+06 0.42101E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3763          52.036          3.7185          3.6538
v  Velocity[Y]            -6.7622          8.7056     -0.00047576      0.00034063
v  Velocity[Z]            -24.092          16.314       -0.096761       -0.042078
v  ǁVelocityǁ            0.012364          52.383          3.8788          3.7005
v  Pressure               -1521.4          192.36          173.71          179.93
v  k                   1.4512e-08          6.2369        0.044883        0.032628
v  omega                0.0029833      7.3679e+05          4501.9          1550.1
v  TempC                  -135.37          604.66          18.212           16.12
v  Density                0.40594          3.4579          1.2423          1.2612
v  TurbVisc            5.2606e-14       0.0022899      3.5907e-05       5.366e-05
v  CourantNb                    0          31.148         0.67308         0.47895
v  FourierNb            0.0024597          4.1959         0.04279        0.048039
v  total_pressure           99804      1.0152e+05       1.015e+05       1.015e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41267          2.1154          1.1682          1.2225


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018401          31.242         0.71587         0.52699


 TIME FOR THE TIME STEP               92:        0.61697E+02

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


 INSTANT    0.723000000E-02   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.147456803E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852460E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53330E+02 0.50784E+01
   Friction velocity        uet   :  0.27922E-02 0.43738E+01
   Friction velocity        uk    :  0.21388E-01 0.14239E+01
   Dimensionless distance   yplus :  0.27895E+00 0.33082E+02
   Friction thermal sca.    tstar : -0.43478E+03 0.29355E+02
   Rough dim-less th. sca.  tplus :  0.20813E+00 0.12289E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     164294
   Nb of faces within the viscous sub-layer     :       3186
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         58 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20012E+00      24   0.15880E-01   0.25680E+02 0.12959E+03 
c  Velocity[X]                                      0.23388E+02 
c  Velocity[Y]                                      0.58354E+00 
c  Velocity[Z]                                      0.17092E+01 
c  Pressure     0.10373E-03     124   0.58084E-02   0.17320E+00 0.22088E+02 
c  k            0.45714E-02      17   0.88767E-03   0.23613E+01 0.94231E+03 
c  omega        0.13056E+03      33   0.16107E-03   0.46774E+09 0.56723E+03 
c  TempC        0.20494E+04      44   0.34321E-01   0.12523E+06 0.41828E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3369          52.021            3.72          3.6565
v  Velocity[Y]            -6.4986          8.9305     -0.00047787      0.00033998
v  Velocity[Z]            -24.053          16.764       -0.097694       -0.042444
v  ǁVelocityǁ            0.011701          52.383          3.8814          3.7035
v  Pressure               -1522.3          192.66          174.06          180.31
v  k                   6.1011e-09          6.2113        0.045414        0.033039
v  omega                 0.017862      3.8922e+05          4499.6          1545.7
v  TempC                   -140.5          599.52          18.414          16.347
v  Density                0.40234          2.5634          1.2418          1.2608
v  TurbVisc            6.1874e-14       0.0022898      3.6428e-05      5.4469e-05
v  CourantNb                    0          32.525          0.6735         0.47931
v  FourierNb            0.0024599          4.1967        0.043241        0.048678
v  total_pressure           99803      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41095          2.1813          1.1675          1.2219


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018046          32.623         0.71674         0.52799


 TIME FOR THE TIME STEP               93:        0.61343E+02

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


 INSTANT    0.733000000E-02   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.418778597E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155850595E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53919E+02 0.49942E+01
   Friction velocity        uet   :  0.10336E-02 0.43924E+01
   Friction velocity        uk    :  0.17813E-01 0.14167E+01
   Dimensionless distance   yplus :  0.22976E+00 0.33121E+02
   Friction thermal sca.    tstar : -0.60556E+03 0.30490E+02
   Rough dim-less th. sca.  tplus :  0.17143E+00 0.12292E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     163529
   Nb of faces within the viscous sub-layer     :       3173
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         58 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20016E+00      25   0.15679E-01   0.25709E+02 0.12950E+03 
c  Velocity[X]                                      0.23411E+02 
c  Velocity[Y]                                      0.58733E+00 
c  Velocity[Z]                                      0.17108E+01 
c  Pressure     0.10355E-03     119   0.60053E-02   0.17288E+00 0.16125E+02 
c  k            0.46043E-02      17   0.88911E-03   0.23740E+01 0.93879E+03 
c  omega        0.12967E+03      33   0.12365E-03   0.41381E+09 0.53380E+03 
c  TempC        0.20630E+04      46   0.33408E-01   0.12515E+06 0.41517E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.365          52.075          3.7215          3.6591
v  Velocity[Y]            -6.5885          8.8358     -0.00045238      0.00034304
v  Velocity[Z]            -24.387          16.872       -0.098627        -0.04281
v  ǁVelocityǁ            0.010823           52.44          3.8841          3.7066
v  Pressure               -1518.9           192.7          174.28          180.56
v  k                   2.1473e-08          6.2677        0.045939        0.033447
v  omega                 0.027483      3.6182e+05          4497.1          1541.5
v  TempC                  -122.43          588.49          18.615          16.574
v  Density                0.40471          2.6624          1.2413          1.2604
v  TurbVisc            2.6015e-14       0.0022897      3.6955e-05      5.5293e-05
v  CourantNb                    0          31.025         0.67393         0.47967
v  FourierNb            0.0024601          4.1973        0.043698        0.049326
v  total_pressure           99806      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40471          2.2802          1.1668          1.2214


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018442           31.12         0.71763         0.52899


 TIME FOR THE TIME STEP               94:        0.61303E+02

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


 INSTANT    0.743000000E-02   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.251829853E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852132E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52321E+02 0.52194E+01
   Friction velocity        uet   :  0.30548E-02 0.43787E+01
   Friction velocity        uk    :  0.12344E-01 0.14251E+01
   Dimensionless distance   yplus :  0.30265E+00 0.33135E+02
   Friction thermal sca.    tstar : -0.60519E+03 0.21281E+02
   Rough dim-less th. sca.  tplus :  0.22581E+00 0.12293E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     162960
   Nb of faces within the viscous sub-layer     :       3181
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         62 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20019E+00      25   0.15656E-01   0.25602E+02 0.12907E+03 
c  Velocity[X]                                      0.23292E+02 
c  Velocity[Y]                                      0.58195E+00 
c  Velocity[Z]                                      0.17278E+01 
c  Pressure     0.10445E-03     141   0.59295E-02   0.17463E+00 0.28416E+02 
c  k            0.46351E-02      17   0.88332E-03   0.24008E+01 0.93833E+03 
c  omega        0.12965E+03      32   0.70205E-03   0.35972E+10 0.15567E+04 
c  TempC        0.20767E+04      44   0.33106E-01   0.12314E+06 0.40892E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3837          52.263          3.7229          3.6618
v  Velocity[Y]             -6.516          8.6823     -0.00046192      0.00033947
v  Velocity[Z]            -24.204          16.909       -0.099558       -0.043181
v  ǁVelocityǁ            0.010465          52.631          3.8867          3.7096
v  Pressure               -1519.4          193.51          174.81          181.06
v  k                    6.572e-09          6.3785         0.04646        0.033851
v  omega                 0.073029      3.0541e+06            4498          1537.6
v  TempC                  -114.42          590.85          18.815          16.802
v  Density                 0.4099          2.3433          1.2408          1.2599
v  TurbVisc            1.3577e-13       0.0022898      3.7489e-05      5.6133e-05
v  CourantNb                    0          32.642         0.67437         0.48003
v  FourierNb            0.0024603          4.1977        0.044155        0.049985
v  total_pressure           99806      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41295          2.3433          1.1662          1.2208


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015441           32.74         0.71852         0.53002


 TIME FOR THE TIME STEP               95:        0.62518E+02

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


 INSTANT    0.753000000E-02   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.403138265E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155848916E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53696E+02 0.51562E+01
   Friction velocity        uet   :  0.46354E-02 0.44086E+01
   Friction velocity        uk    :  0.19365E-01 0.14309E+01
   Dimensionless distance   yplus :  0.21544E+00 0.33304E+02
   Friction thermal sca.    tstar : -0.51674E+03 0.21907E+02
   Rough dim-less th. sca.  tplus :  0.16075E+00 0.12305E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     162361
   Nb of faces within the viscous sub-layer     :       3184
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         62 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20023E+00      25   0.15528E-01   0.25347E+02 0.12827E+03 
c  Velocity[X]                                      0.23046E+02 
c  Velocity[Y]                                      0.58286E+00 
c  Velocity[Z]                                      0.17179E+01 
c  Pressure     0.10443E-03     131   0.58549E-02   0.17455E+00 0.31387E+02 
c  k            0.46627E-02      17   0.87073E-03   0.24344E+01 0.93933E+03 
c  omega        0.17782E+03      32   0.25670E-03   0.13999E+10 0.97802E+03 
c  TempC        0.20903E+04      44   0.33088E-01   0.12271E+06 0.40534E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4132          52.192          3.7243          3.6645
v  Velocity[Y]            -6.5065          8.7883      -0.0004641      0.00033785
v  Velocity[Z]            -24.513          16.713        -0.10047       -0.043544
v  ǁVelocityǁ           0.0085671          52.558          3.8893          3.7126
v  Pressure               -1515.3          194.05          175.35          181.62
v  k                   1.1132e-07          6.3133        0.046979        0.034251
v  omega                 0.087004       1.545e+06          4496.2          1533.6
v  TempC                  -117.53          613.84          19.016           17.03
v  Density                0.40877          2.2251          1.2403          1.2595
v  TurbVisc             5.851e-14       0.0022898      3.8035e-05       5.699e-05
v  CourantNb                    0          31.227         0.67479         0.48039
v  FourierNb            0.0024605          4.1981        0.044622        0.050655
v  total_pressure           99810      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41043          1.9586          1.1655          1.2203


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013343          31.322         0.71941         0.53105


 TIME FOR THE TIME STEP               96:        0.61715E+02

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


 INSTANT    0.763000000E-02   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.124318294E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846963E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51651E+02 0.51062E+01
   Friction velocity        uet   :  0.15078E-02 0.43869E+01
   Friction velocity        uk    :  0.17089E-01 0.14303E+01
   Dimensionless distance   yplus :  0.19983E+00 0.34295E+02
   Friction thermal sca.    tstar : -0.66919E+03 0.27374E+02
   Rough dim-less th. sca.  tplus :  0.14909E+00 0.12375E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     161708
   Nb of faces within the viscous sub-layer     :       3209
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         64 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20026E+00      25   0.15776E-01   0.25416E+02 0.12828E+03 
c  Velocity[X]                                      0.23131E+02 
c  Velocity[Y]                                      0.57505E+00 
c  Velocity[Z]                                      0.17098E+01 
c  Pressure     0.10433E-03     132   0.59122E-02   0.17425E+00 0.36210E+02 
c  k            0.46867E-02      17   0.85820E-03   0.24518E+01 0.93714E+03 
c  omega        0.13341E+03      33   0.19202E-03   0.57681E+09 0.62944E+03 
c  TempC        0.21036E+04      46   0.33841E-01   0.12418E+06 0.40496E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4394          52.223          3.7258          3.6672
v  Velocity[Y]            -6.4796          8.7648     -0.00047131      0.00033687
v  Velocity[Z]            -24.379           16.96        -0.10142       -0.043916
v  ǁVelocityǁ             0.01283          52.624           3.892          3.7156
v  Pressure               -1514.8          194.93          175.98          182.26
v  k                   1.5082e-07          6.4034        0.047499        0.034649
v  omega                 0.020431      7.8908e+05          4494.3          1529.7
v  TempC                  -120.29          601.91          19.215          17.257
v  Density                0.39818          2.2695          1.2398           1.259
v  TurbVisc            4.7471e-13       0.0022902      3.8582e-05      5.7845e-05
v  CourantNb                    0          32.584         0.67523         0.48075
v  FourierNb            0.0024607          4.1983        0.045087        0.051325
v  total_pressure           99810      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40564          2.0398          1.1649          1.2197


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014344          32.682         0.72032         0.53208


 TIME FOR THE TIME STEP               97:        0.61896E+02

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


 INSTANT    0.773000000E-02   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.143274842E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846393E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53825E+02 0.51667E+01
   Friction velocity        uet   :  0.29697E-02 0.44172E+01
   Friction velocity        uk    :  0.15165E-01 0.14346E+01
   Dimensionless distance   yplus :  0.20508E+00 0.33967E+02
   Friction thermal sca.    tstar : -0.73527E+03 0.28769E+02
   Rough dim-less th. sca.  tplus :  0.15301E+00 0.12352E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     161121
   Nb of faces within the viscous sub-layer     :       3212
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         66 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20030E+00      25   0.15524E-01   0.25623E+02 0.12864E+03 
c  Velocity[X]                                      0.23297E+02 
c  Velocity[Y]                                      0.57980E+00 
c  Velocity[Z]                                      0.17460E+01 
c  Pressure     0.10297E-03     131   0.57770E-02   0.17179E+00 0.34986E+02 
c  k            0.47042E-02      16   0.85921E-03   0.24639E+01 0.93397E+03 
c  omega        0.12943E+03      33   0.14431E-03   0.45725E+09 0.56060E+03 
c  TempC        0.21169E+04      46   0.32756E-01   0.12565E+06 0.40460E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4693          52.098          3.7273          3.6699
v  Velocity[Y]            -6.4098          8.7916     -0.00047322      0.00033018
v  Velocity[Z]            -24.526          16.476        -0.10238       -0.044292
v  ǁVelocityǁ             0.01566          52.462          3.8947          3.7186
v  Pressure               -1511.6          195.37          176.57          182.89
v  k                   5.7165e-08          6.4097        0.048021        0.035046
v  omega                0.0074167      4.0902e+05          4492.9          1525.9
v  TempC                  -122.68          596.29          19.415          17.484
v  Density                0.40361          2.3105          1.2393          1.2586
v  TurbVisc            6.4311e-13       0.0022905      3.9127e-05      5.8698e-05
v  CourantNb                    0          31.174         0.67567         0.48112
v  FourierNb            0.0024609          4.1985        0.045548        0.051989
v  total_pressure           99813      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40691          2.1338          1.1642          1.2192


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016705          31.268         0.72121         0.53311


 TIME FOR THE TIME STEP               98:        0.61803E+02

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


 INSTANT    0.783000000E-02   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.230415985E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155847134E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51555E+02 0.53004E+01
   Friction velocity        uet   :  0.23945E-02 0.43810E+01
   Friction velocity        uk    :  0.89328E-02 0.14423E+01
   Dimensionless distance   yplus :  0.12578E+00 0.34220E+02
   Friction thermal sca.    tstar : -0.10546E+04 0.23541E+02
   Rough dim-less th. sca.  tplus :  0.93844E-01 0.12370E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     160488
   Nb of faces within the viscous sub-layer     :       3233
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         68 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20034E+00      25   0.15877E-01   0.25791E+02 0.12890E+03 
c  Velocity[X]                                      0.23469E+02 
c  Velocity[Y]                                      0.58165E+00 
c  Velocity[Z]                                      0.17405E+01 
c  Pressure     0.10417E-03     128   0.58707E-02   0.17405E+00 0.34354E+02 
c  k            0.47158E-02      17   0.86879E-03   0.24927E+01 0.93404E+03 
c  omega        0.12907E+03      33   0.20088E-03   0.67347E+09 0.67961E+03 
c  TempC        0.21298E+04      44   0.32371E-01   0.12392E+06 0.39912E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4994           52.07          3.7289          3.6725
v  Velocity[Y]             -6.496          8.7262     -0.00047714      0.00032979
v  Velocity[Z]            -24.287          16.707        -0.10335       -0.044668
v  ǁVelocityǁ           0.0063491          52.451          3.8974          3.7217
v  Pressure               -1511.2          196.09          177.15          183.51
v  k                   2.5034e-08           6.439        0.048551        0.035441
v  omega                0.0063263      1.0897e+06          4492.8          1522.3
v  TempC                  -122.94          596.39          19.615          17.712
v  Density                0.40622          2.3473          1.2388          1.2582
v  TurbVisc            3.0733e-13       0.0022904      3.9672e-05      5.9553e-05
v  CourantNb                    0          32.601         0.67612         0.48148
v  FourierNb            0.0024611          4.1986        0.046011        0.052653
v  total_pressure           99814      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40622          2.2239          1.1636          1.2187


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016471          32.699         0.72213         0.53414


 TIME FOR THE TIME STEP               99:        0.61695E+02

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


 INSTANT    0.793000000E-02   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.144866908E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155848024E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53916E+02 0.51564E+01
   Friction velocity        uet   :  0.23161E-02 0.44103E+01
   Friction velocity        uk    :  0.17624E-01 0.14364E+01
   Dimensionless distance   yplus :  0.24784E+00 0.35018E+02
   Friction thermal sca.    tstar : -0.58579E+03 0.23929E+02
   Rough dim-less th. sca.  tplus :  0.18491E+00 0.12424E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     159929
   Nb of faces within the viscous sub-layer     :       3233
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         71 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20037E+00      25   0.15851E-01   0.25740E+02 0.12862E+03 
c  Velocity[X]                                      0.23434E+02 
c  Velocity[Y]                                      0.57690E+00 
c  Velocity[Z]                                      0.17287E+01 
c  Pressure     0.10439E-03     127   0.59552E-02   0.17466E+00 0.26669E+02 
c  k            0.47219E-02      17   0.87920E-03   0.25329E+01 0.93626E+03 
c  omega        0.12929E+03      33   0.13526E-03   0.36267E+09 0.49911E+03 
c  TempC        0.21425E+04      46   0.32575E-01   0.12458E+06 0.39754E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.59           52.29          3.7304          3.6752
v  Velocity[Y]             -6.677          8.6024     -0.00047914       0.0003254
v  Velocity[Z]            -24.438          17.101        -0.10427       -0.045033
v  ǁVelocityǁ            0.021003          52.665          3.9001          3.7247
v  Pressure               -1506.8          196.36          177.58          183.98
v  k                    2.225e-07          6.5063        0.049085        0.035833
v  omega                0.0064126       6.966e+05          4490.6          1518.6
v  TempC                  -126.33          596.93          19.817          17.939
v  Density                0.40617          2.3513          1.2383          1.2577
v  TurbVisc            1.5041e-13       0.0022902      4.0221e-05      6.0415e-05
v  CourantNb                    0          31.151         0.67656         0.48185
v  FourierNb            0.0024613          4.1988        0.046478        0.053321
v  total_pressure           99818      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density           0.416          2.3183           1.163          1.2181


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018639          31.246         0.72304         0.53517


 TIME FOR THE TIME STEP              100:        0.61644E+02

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


 INSTANT    0.803000000E-02   TIME STEP NUMBER             101
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.136932794E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155849250E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51494E+02 0.52872E+01
   Friction velocity        uet   :  0.44564E-02 0.43985E+01
   Friction velocity        uk    :  0.22285E-01 0.14481E+01
   Dimensionless distance   yplus :  0.30010E+00 0.34390E+02
   Friction thermal sca.    tstar : -0.49002E+03 0.24706E+02
   Rough dim-less th. sca.  tplus :  0.22391E+00 0.12381E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     159374
   Nb of faces within the viscous sub-layer     :       3233
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         73 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20042E+00      25   0.16118E-01   0.25675E+02 0.12829E+03 
c  Velocity[X]                                      0.23313E+02 
c  Velocity[Y]                                      0.59140E+00 
c  Velocity[Z]                                      0.17704E+01 
c  Pressure     0.10442E-03     142   0.59250E-02   0.17458E+00 0.34323E+02 
c  k            0.47226E-02      17   0.87717E-03   0.25562E+01 0.93524E+03 
c  omega        0.12897E+03      33   0.12028E-03   0.31435E+09 0.46462E+03 
c  TempC        0.21546E+04      44   0.31791E-01   0.12574E+06 0.39680E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6744          52.107           3.732          3.6779
v  Velocity[Y]            -6.7009            8.62     -0.00048709      0.00032235
v  Velocity[Z]            -24.363          16.471        -0.10521       -0.045412
v  ǁVelocityǁ            0.022019          52.514          3.9029          3.7277
v  Pressure               -1506.5          197.07          178.21           184.6
v  k                   1.4407e-07          6.5752         0.04963        0.036224
v  omega                 0.013802      5.7697e+05          4489.5          1515.1
v  TempC                  -129.49          601.64           20.02          18.166
v  Density                0.40592          2.4055          1.2378          1.2573
v  TurbVisc            9.3457e-13       0.0022899      4.0762e-05      6.1266e-05
v  CourantNb                    0          32.614         0.67703         0.48222
v  FourierNb            0.0024615          4.1988        0.046939        0.053983
v  total_pressure           99819      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41403          2.4055          1.1624          1.2176


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021331          32.712         0.72397         0.53621


 TIME FOR THE TIME STEP              101:        0.62448E+02

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


 INSTANT    0.813000000E-02   TIME STEP NUMBER             102
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.131816013E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155847802E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54132E+02 0.52996E+01
   Friction velocity        uet   :  0.33408E-02 0.44162E+01
   Friction velocity        uk    :  0.81847E-02 0.14506E+01
   Dimensionless distance   yplus :  0.18443E+00 0.34029E+02
   Friction thermal sca.    tstar : -0.10344E+04 0.26857E+02
   Rough dim-less th. sca.  tplus :  0.13760E+00 0.12356E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     158806
   Nb of faces within the viscous sub-layer     :       3245
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         76 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20045E+00      24   0.15468E-01   0.25908E+02 0.12872E+03 
c  Velocity[X]                                      0.23549E+02 
c  Velocity[Y]                                      0.58355E+00 
c  Velocity[Z]                                      0.17752E+01 
c  Pressure     0.10393E-03     132   0.58689E-02   0.17361E+00 0.32087E+02 
c  k            0.47187E-02      17   0.88196E-03   0.25773E+01 0.93381E+03 
c  omega        0.12883E+03      33   0.11014E-03   0.36968E+09 0.50360E+03 
c  TempC        0.21666E+04      46   0.31333E-01   0.12549E+06 0.39385E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.764          52.179          3.7335          3.6806
v  Velocity[Y]            -6.7053          8.8125     -0.00050019      0.00031944
v  Velocity[Z]            -24.854          16.744        -0.10616       -0.045787
v  ǁVelocityǁ            0.022964          52.558          3.9057          3.7308
v  Pressure               -1501.9          197.94          178.79          185.18
v  k                   2.1123e-07          6.5194        0.050182        0.036614
v  omega                 0.033927       5.569e+05          4489.2          1511.7
v  TempC                  -125.88          602.89          20.228          18.394
v  Density                0.40373          2.4585          1.2374          1.2569
v  TurbVisc            9.3714e-13       0.0022899      4.1301e-05       6.212e-05
v  CourantNb                    0          31.117         0.67749         0.48259
v  FourierNb            0.0024617          4.1989        0.047406        0.054649
v  total_pressure           99823      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41421          2.4585          1.1618          1.2171


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020081          31.211          0.7249         0.53724


 TIME FOR THE TIME STEP              102:        0.61581E+02

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


 INSTANT    0.823000000E-02   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.141982422E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846832E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51477E+02 0.54402E+01
   Friction velocity        uet   :  0.80675E-02 0.43915E+01
   Friction velocity        uk    :  0.13200E-01 0.14519E+01
   Dimensionless distance   yplus :  0.10641E+00 0.33888E+02
   Friction thermal sca.    tstar : -0.46414E+03 0.25254E+02
   Rough dim-less th. sca.  tplus :  0.79391E-01 0.12346E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     158243
   Nb of faces within the viscous sub-layer     :       3272
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         77 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20049E+00      25   0.15949E-01   0.25781E+02 0.12824E+03 
c  Velocity[X]                                      0.23494E+02 
c  Velocity[Y]                                      0.57910E+00 
c  Velocity[Z]                                      0.17079E+01 
c  Pressure     0.10353E-03     130   0.58989E-02   0.17273E+00 0.32689E+02 
c  k            0.47144E-02      17   0.88743E-03   0.26007E+01 0.93292E+03 
c  omega        0.12881E+03      33   0.16976E-03   0.41713E+09 0.53452E+03 
c  TempC        0.21780E+04      46   0.32159E-01   0.12502E+06 0.39061E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8426           52.08          3.7352          3.6833
v  Velocity[Y]            -6.9738           8.825     -0.00049219      0.00031821
v  Velocity[Z]            -24.525          17.125        -0.10714       -0.046173
v  ǁVelocityǁ            0.012626          52.494          3.9086          3.7338
v  Pressure               -1501.5          198.75          179.38          185.77
v  k                    1.297e-07          6.6506        0.050736        0.037001
v  omega                  0.12066       5.571e+05          4489.6          1508.4
v  TempC                  -108.19          609.43          20.436          18.621
v  Density                0.40316          2.3982          1.2369          1.2564
v  TurbVisc            9.4748e-13       0.0022898      4.1831e-05      6.2967e-05
v  CourantNb                    0          32.651         0.67797         0.48297
v  FourierNb            0.0024619          4.1989        0.047868         0.05531
v  total_pressure           99823      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40316           2.059          1.1612          1.2166


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014862          32.749         0.72584         0.53828


 TIME FOR THE TIME STEP              103:        0.61595E+02

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


 INSTANT    0.833000000E-02   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.140690688E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155847079E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54499E+02 0.53617E+01
   Friction velocity        uet   :  0.21019E-02 0.44196E+01
   Friction velocity        uk    :  0.25949E-01 0.14565E+01
   Dimensionless distance   yplus :  0.30572E+00 0.33770E+02
   Friction thermal sca.    tstar : -0.38045E+03 0.25840E+02
   Rough dim-less th. sca.  tplus :  0.22810E+00 0.12338E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     157725
   Nb of faces within the viscous sub-layer     :       3280
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         80 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20053E+00      25   0.16185E-01   0.25821E+02 0.12818E+03 
c  Velocity[X]                                      0.23479E+02 
c  Velocity[Y]                                      0.58639E+00 
c  Velocity[Z]                                      0.17559E+01 
c  Pressure     0.10358E-03     124   0.59263E-02   0.17290E+00 0.23233E+02 
c  k            0.47125E-02      17   0.89088E-03   0.26282E+01 0.93282E+03 
c  omega        0.12874E+03      33   0.11333E-03   0.36154E+09 0.49748E+03 
c  TempC        0.21888E+04      44   0.31579E-01   0.12633E+06 0.39021E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9221          52.171          3.7368          3.6859
v  Velocity[Y]            -6.6858          8.6323     -0.00047848      0.00031689
v  Velocity[Z]            -24.664          16.577        -0.10811       -0.046544
v  ǁVelocityǁ           0.0083721          52.558          3.9115          3.7369
v  Pressure               -1497.2          198.77          179.74          186.18
v  k                   2.0128e-07          6.5811        0.051282        0.037386
v  omega                  0.14902      5.5121e+05          4489.1          1505.1
v  TempC                  -114.15          601.62          20.647          18.848
v  Density                0.40017          2.1411          1.2364           1.256
v  TurbVisc            9.8746e-13       0.0022901      4.2356e-05      6.3802e-05
v  CourantNb                    0          31.154         0.67844         0.48334
v  FourierNb            0.0024621           4.199        0.048326        0.055963
v  total_pressure           99828      1.0152e+05       1.015e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40017          2.1411          1.1606          1.2161


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012339          31.248         0.72676          0.5393


 TIME FOR THE TIME STEP              104:        0.61354E+02

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


 INSTANT    0.843000000E-02   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.197274268E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155850085E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51660E+02 0.54415E+01
   Friction velocity        uet   :  0.33622E-02 0.43929E+01
   Friction velocity        uk    :  0.21809E-01 0.14577E+01
   Dimensionless distance   yplus :  0.25227E+00 0.34709E+02
   Friction thermal sca.    tstar : -0.41304E+03 0.26148E+02
   Rough dim-less th. sca.  tplus :  0.18822E+00 0.12403E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     157212
   Nb of faces within the viscous sub-layer     :       3306
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         81 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20057E+00      24   0.16198E-01   0.25979E+02 0.12842E+03 
c  Velocity[X]                                      0.23668E+02 
c  Velocity[Y]                                      0.57253E+00 
c  Velocity[Z]                                      0.17376E+01 
c  Pressure     0.10295E-03     130   0.59371E-02   0.17191E+00 0.28851E+02 
c  k            0.47166E-02      17   0.89370E-03   0.26582E+01 0.93317E+03 
c  omega        0.12868E+03      33   0.17169E-03   0.58515E+09 0.63217E+03 
c  TempC        0.21994E+04      45   0.30780E-01   0.12646E+06 0.38803E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8215          51.995          3.7385          3.6886
v  Velocity[Y]            -6.6815          8.7077     -0.00048006       0.0003188
v  Velocity[Z]            -24.514          16.916        -0.10909       -0.046929
v  ǁVelocityǁ            0.015625          52.412          3.9144          3.7399
v  Pressure               -1496.3          199.17          180.28           186.7
v  k                   4.8867e-08          6.6559        0.051815        0.037771
v  omega                 0.019414      7.1561e+05          4489.6            1502
v  TempC                  -120.05          596.15           20.86          19.075
v  Density                0.40374          2.2213          1.2359          1.2556
v  TurbVisc            8.8998e-13       0.0022904      4.2884e-05      6.4643e-05
v  CourantNb                    0          32.539         0.67892         0.48372
v  FourierNb            0.0024623           4.199        0.048785        0.056619
v  total_pressure           99829      1.0152e+05      1.0151e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41886          2.2213            1.16          1.2155


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015927          32.636         0.72771         0.54033


 TIME FOR THE TIME STEP              105:        0.61489E+02

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


 INSTANT    0.853000000E-02   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.788909887E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155847736E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54462E+02 0.54163E+01
   Friction velocity        uet   :  0.45639E-02 0.44145E+01
   Friction velocity        uk    :  0.20425E-01 0.14585E+01
   Dimensionless distance   yplus :  0.34299E+00 0.34313E+02
   Friction thermal sca.    tstar : -0.37233E+03 0.26819E+02
   Rough dim-less th. sca.  tplus :  0.25591E+00 0.12376E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     156741
   Nb of faces within the viscous sub-layer     :       3324
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         82 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20060E+00      25   0.15934E-01   0.26157E+02 0.12870E+03 
c  Velocity[X]                                      0.23835E+02 
c  Velocity[Y]                                      0.58027E+00 
c  Velocity[Z]                                      0.17419E+01 
c  Pressure     0.10390E-03     131   0.59921E-02   0.17336E+00 0.31367E+02 
c  k            0.47275E-02      17   0.90829E-03   0.26951E+01 0.93484E+03 
c  omega        0.12884E+03      33   0.13280E-03   0.51514E+09 0.59285E+03 
c  TempC        0.22099E+04      46   0.30068E-01   0.12573E+06 0.38455E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9726          52.188          3.7402          3.6913
v  Velocity[Y]            -6.7622          8.7741     -0.00050489      0.00031365
v  Velocity[Z]            -24.875          17.306         -0.1101        -0.04732
v  ǁVelocityǁ           0.0091044          52.584          3.9174          3.7429
v  Pressure               -1491.7          199.73          180.85          187.28
v  k                   5.2928e-08          6.7491        0.052324        0.038153
v  omega                  0.13981      3.9675e+05          4489.7            1499
v  TempC                  -123.78          612.41          21.073          19.301
v  Density                0.40628          2.3068          1.2354          1.2551
v  TurbVisc            2.1208e-13       0.0022903      4.3416e-05      6.5495e-05
v  CourantNb                    0          31.072         0.67942         0.48409
v  FourierNb            0.0024625           4.199        0.049246        0.057282
v  total_pressure           99833      1.0152e+05      1.0151e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40871          2.3068          1.1595           1.215


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.019173          31.166         0.72867         0.54137


 TIME FOR THE TIME STEP              106:        0.61803E+02

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


 INSTANT    0.863000000E-02   TIME STEP NUMBER             107
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.362557700E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846815E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52054E+02 0.54678E+01
   Friction velocity        uet   :  0.82661E-03 0.43977E+01
   Friction velocity        uk    :  0.12800E-01 0.14717E+01
   Dimensionless distance   yplus :  0.25384E+00 0.34186E+02
   Friction thermal sca.    tstar : -0.49693E+03 0.27857E+02
   Rough dim-less th. sca.  tplus :  0.18939E+00 0.12367E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     156233
   Nb of faces within the viscous sub-layer     :       3346
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         88 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20063E+00      25   0.15994E-01   0.26132E+02 0.12848E+03 
c  Velocity[X]                                      0.23711E+02 
c  Velocity[Y]                                      0.59381E+00 
c  Velocity[Z]                                      0.18273E+01 
c  Pressure     0.10514E-03     150   0.57952E-02   0.17550E+00 0.45982E+02 
c  k            0.47482E-02      17   0.91404E-03   0.27296E+01 0.93617E+03 
c  omega        0.12866E+03      33   0.15393E-03   0.45093E+09 0.55438E+03 
c  TempC        0.22205E+04      45   0.30176E-01   0.12497E+06 0.38109E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.068          51.985           3.742          3.6939
v  Velocity[Y]            -6.8395          8.5861     -0.00049824      0.00031418
v  Velocity[Z]            -24.533          16.826        -0.11108       -0.047702
v  ǁVelocityǁ           0.0076947          52.405          3.9204          3.7459
v  Pressure               -1491.1          200.79           181.7          188.13
v  k                   1.8637e-07          6.7523        0.052806        0.038531
v  omega                 0.026002      3.5514e+05            4490            1496
v  TempC                  -128.69          613.07          21.284          19.528
v  Density                0.39883          2.3645          1.2349          1.2547
v  TurbVisc             2.294e-13       0.0022902      4.3953e-05      6.6349e-05
v  CourantNb                    0          32.643          0.6799         0.48447
v  FourierNb            0.0024627           4.199        0.049711        0.057948
v  total_pressure           99834      1.0153e+05      1.0151e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41156          2.3645          1.1589          1.2145


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021157           32.74         0.72961         0.54241


 TIME FOR THE TIME STEP              107:        0.62821E+02

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


 INSTANT    0.873000000E-02   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.719150824E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845634E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54806E+02 0.55067E+01
   Friction velocity        uet   :  0.24385E-02 0.44169E+01
   Friction velocity        uk    :  0.15132E-01 0.14688E+01
   Dimensionless distance   yplus :  0.20058E+00 0.34351E+02
   Friction thermal sca.    tstar : -0.62292E+03 0.28880E+02
   Rough dim-less th. sca.  tplus :  0.14965E+00 0.12379E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     155833
   Nb of faces within the viscous sub-layer     :       3369
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         89 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20067E+00      25   0.15673E-01   0.25851E+02 0.12763E+03 
c  Velocity[X]                                      0.23539E+02 
c  Velocity[Y]                                      0.58986E+00 
c  Velocity[Z]                                      0.17226E+01 
c  Pressure     0.10398E-03     133   0.58900E-02   0.17345E+00 0.38951E+02 
c  k            0.47768E-02      17   0.90621E-03   0.27566E+01 0.93620E+03 
c  omega        0.12880E+03      34   0.25224E-03   0.37009E+10 0.15697E+04 
c  TempC        0.22312E+04      45   0.30294E-01   0.12484E+06 0.37865E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1385          52.212          3.7437          3.6966
v  Velocity[Y]            -6.8716          8.7904     -0.00050047      0.00031172
v  Velocity[Z]            -24.845          16.952        -0.11206        -0.04809
v  ǁVelocityǁ           0.0098301           52.61          3.9233           3.749
v  Pressure               -1485.9          201.81          182.39          188.86
v  k                   1.3332e-08          6.7777        0.053265        0.038908
v  omega                0.0088673      1.7102e+06          4491.8          1493.2
v  TempC                  -133.65          616.57          21.494          19.754
v  Density                0.39853          2.4449          1.2344          1.2543
v  TurbVisc              9.69e-13       0.0022899      4.4489e-05      6.7198e-05
v  CourantNb                    0           31.09         0.68039         0.48484
v  FourierNb            0.0024629           4.199        0.050176         0.05861
v  total_pressure           99839      1.0153e+05      1.0151e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41049          2.4449          1.1583           1.214


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020262          31.183         0.73057         0.54345


 TIME FOR THE TIME STEP              108:        0.61754E+02

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


 INSTANT    0.883000000E-02   TIME STEP NUMBER             109
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.115866522E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845424E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52271E+02 0.55882E+01
   Friction velocity        uet   :  0.24816E-02 0.44002E+01
   Friction velocity        uk    :  0.19456E-01 0.14759E+01
   Dimensionless distance   yplus :  0.25264E+00 0.35441E+02
   Friction thermal sca.    tstar : -0.37321E+03 0.28892E+02
   Rough dim-less th. sca.  tplus :  0.18850E+00 0.12453E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     155465
   Nb of faces within the viscous sub-layer     :       3394
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         96 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20071E+00      25   0.15864E-01   0.25892E+02 0.12758E+03 
c  Velocity[X]                                      0.23554E+02 
c  Velocity[Y]                                      0.58906E+00 
c  Velocity[Z]                                      0.17485E+01 
c  Pressure     0.10473E-03     150   0.59797E-02   0.17466E+00 0.46789E+02 
c  k            0.48117E-02      18   0.89573E-03   0.27753E+01 0.93471E+03 
c  omega        0.15191E+03      33   0.18152E-03   0.12560E+10 0.92110E+03 
c  TempC        0.22420E+04      46   0.29900E-01   0.12584E+06 0.37795E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0091          51.958          3.7454          3.6992
v  Velocity[Y]            -6.9035          8.5547     -0.00052269       0.0003088
v  Velocity[Z]            -24.665          17.332        -0.11306       -0.048487
v  ǁVelocityǁ            0.015834          52.385          3.9263           3.752
v  Pressure               -1484.7          202.63          183.25          189.74
v  k                   1.8002e-07          6.8528        0.053705        0.039287
v  omega                0.0040505      8.7487e+05          4491.3          1490.3
v  TempC                  -137.96           610.2          21.699           19.98
v  Density                0.39696          2.5318           1.234          1.2538
v  TurbVisc            7.1701e-14       0.0022899      4.5024e-05      6.8037e-05
v  CourantNb                    0          32.542         0.68089         0.48522
v  FourierNb            0.0024631           4.199         0.05064        0.059266
v  total_pressure           99840      1.0153e+05      1.0151e+05      1.0151e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40814          2.5318          1.1578          1.2135


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018077          32.639         0.73153         0.54448


 TIME FOR THE TIME STEP              109:        0.62902E+02

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


 INSTANT    0.893000000E-02   TIME STEP NUMBER             110
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.298967842E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845563E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54965E+02 0.55867E+01
   Friction velocity        uet   :  0.33327E-02 0.44182E+01
   Friction velocity        uk    :  0.15009E-01 0.14778E+01
   Dimensionless distance   yplus :  0.21975E+00 0.35115E+02
   Friction thermal sca.    tstar : -0.62782E+03 0.29157E+02
   Rough dim-less th. sca.  tplus :  0.16396E+00 0.12431E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     155134
   Nb of faces within the viscous sub-layer     :       3414
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         98 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20074E+00      25   0.15901E-01   0.25812E+02 0.12723E+03 
c  Velocity[X]                                      0.23450E+02 
c  Velocity[Y]                                      0.57894E+00 
c  Velocity[Z]                                      0.17832E+01 
c  Pressure     0.10379E-03     137   0.59019E-02   0.17276E+00 0.40303E+02 
c  k            0.48474E-02      17   0.89305E-03   0.27886E+01 0.93228E+03 
c  omega        0.13061E+03      33   0.13573E-03   0.63205E+09 0.65448E+03 
c  TempC        0.22531E+04      46   0.29254E-01   0.12600E+06 0.37602E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1036          52.028           3.747          3.7019
v  Velocity[Y]            -6.9302          8.6944     -0.00050709      0.00030831
v  Velocity[Z]            -24.755          16.894        -0.11407       -0.048887
v  ǁVelocityǁ            0.016251          52.428          3.9292           3.755
v  Pressure               -1480.2          203.38          183.99           190.5
v  k                   1.7699e-07          6.9888        0.054131        0.039665
v  omega                  0.00126      4.5594e+05            4491          1487.4
v  TempC                  -141.65          597.25          21.901          20.207
v  Density                0.39982          2.6125          1.2335          1.2534
v  TurbVisc            9.3346e-13       0.0022898      4.5563e-05      6.8875e-05
v  CourantNb                    0          31.025         0.68138         0.48559
v  FourierNb            0.0024633           4.199        0.051104        0.059923
v  total_pressure           99845      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41834          2.6125          1.1572           1.213


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018631          31.119         0.73248         0.54551


 TIME FOR THE TIME STEP              110:        0.61986E+02

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


 INSTANT    0.903000000E-02   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.105525136E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155844852E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52315E+02 0.55609E+01
   Friction velocity        uet   :  0.32814E-02 0.43890E+01
   Friction velocity        uk    :  0.23231E-01 0.14935E+01
   Dimensionless distance   yplus :  0.25897E+00 0.34995E+02
   Friction thermal sca.    tstar : -0.47299E+03 0.29740E+02
   Rough dim-less th. sca.  tplus :  0.19322E+00 0.12423E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     154787
   Nb of faces within the viscous sub-layer     :       3456
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        101 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20078E+00      25   0.16156E-01   0.26082E+02 0.12774E+03 
c  Velocity[X]                                      0.23691E+02 
c  Velocity[Y]                                      0.59484E+00 
c  Velocity[Z]                                      0.17966E+01 
c  Pressure     0.10407E-03     156   0.58169E-02   0.17326E+00 0.54812E+02 
c  k            0.48821E-02      18   0.90484E-03   0.28089E+01 0.93120E+03 
c  omega        0.12885E+03      33   0.23484E-03   0.70658E+09 0.69126E+03 
c  TempC        0.22645E+04      45   0.29468E-01   0.12479E+06 0.37206E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1766          51.986          3.7486          3.7045
v  Velocity[Y]            -6.9885          8.6842     -0.00049812      0.00030934
v  Velocity[Z]            -24.568          17.172        -0.11508       -0.049285
v  ǁVelocityǁ            0.015487          52.406          3.9322           3.758
v  Pressure               -1478.7          204.41          185.03          191.54
v  k                   2.5267e-08          6.9528        0.054547        0.040039
v  omega               2.3266e-05      1.1065e+06          4492.2          1484.7
v  TempC                  -143.51          594.54          22.102          20.433
v  Density                0.40577          2.6857           1.233           1.253
v  TurbVisc            9.1651e-13       0.0022899      4.6125e-05      6.9738e-05
v  CourantNb                    0          32.544         0.68187         0.48596
v  FourierNb            0.0024635           4.199        0.051597        0.060607
v  total_pressure           99846      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41927          2.6857          1.1567          1.2126


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016403          32.641         0.73346         0.54657


 TIME FOR THE TIME STEP              111:        0.63225E+02

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


 INSTANT    0.913000000E-02   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.164633614E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155843786E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55702E+02 0.56032E+01
   Friction velocity        uet   :  0.17814E-02 0.44241E+01
   Friction velocity        uk    :  0.14691E-01 0.14857E+01
   Dimensionless distance   yplus :  0.23678E+00 0.35867E+02
   Friction thermal sca.    tstar : -0.67829E+03 0.29850E+02
   Rough dim-less th. sca.  tplus :  0.17667E+00 0.12482E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     154430
   Nb of faces within the viscous sub-layer     :       3473
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        106 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20082E+00      25   0.16352E-01   0.25987E+02 0.12735E+03 
c  Velocity[X]                                      0.23646E+02 
c  Velocity[Y]                                      0.58647E+00 
c  Velocity[Z]                                      0.17547E+01 
c  Pressure     0.10454E-03     134   0.58636E-02   0.17393E+00 0.38053E+02 
c  k            0.49139E-02      17   0.91184E-03   0.28326E+01 0.93081E+03 
c  omega        0.12900E+03      33   0.27334E-03   0.64854E+09 0.66186E+03 
c  TempC        0.22760E+04      46   0.29808E-01   0.12360E+06 0.36818E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2101           52.28          3.7503          3.7072
v  Velocity[Y]            -6.9706           8.558     -0.00048033      0.00031207
v  Velocity[Z]            -25.079          17.394        -0.11611       -0.049684
v  ǁVelocityǁ            0.015314          52.668          3.9351          3.7611
v  Pressure                 -1473          204.62          185.71          192.26
v  k                   1.7079e-07          6.9889        0.054957        0.040411
v  omega               0.00049204      7.5101e+05          4492.6          1482.1
v  TempC                  -110.11          600.14          22.301           20.66
v  Density                0.40704          2.7244          1.2326          1.2525
v  TurbVisc            3.3371e-13       0.0022898      4.6689e-05      7.0599e-05
v  CourantNb                    0          31.119         0.68235         0.48634
v  FourierNb            0.0024637           4.199        0.052087        0.061291
v  total_pressure           99852      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41731          2.7244          1.1562          1.2121


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017076          31.212         0.73444         0.54763


 TIME FOR THE TIME STEP              112:        0.61834E+02

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


 INSTANT    0.923000000E-02   TIME STEP NUMBER             113
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.728493437E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155844988E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53250E+02 0.56553E+01
   Friction velocity        uet   :  0.56140E-03 0.44114E+01
   Friction velocity        uk    :  0.15791E-01 0.14941E+01
   Dimensionless distance   yplus :  0.17579E+00 0.35365E+02
   Friction thermal sca.    tstar : -0.69380E+03 0.30565E+02
   Rough dim-less th. sca.  tplus :  0.13116E+00 0.12448E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     154154
   Nb of faces within the viscous sub-layer     :       3495
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        110 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20085E+00      25   0.16367E-01   0.26034E+02 0.12731E+03 
c  Velocity[X]                                      0.23594E+02 
c  Velocity[Y]                                      0.61052E+00 
c  Velocity[Z]                                      0.18297E+01 
c  Pressure     0.10653E-03     150   0.59435E-02   0.17751E+00 0.43836E+02 
c  k            0.49427E-02      17   0.90969E-03   0.28504E+01 0.92949E+03 
c  omega        0.12899E+03      34   0.26576E-03   0.77907E+09 0.72444E+03 
c  TempC        0.22875E+04      45   0.29418E-01   0.12525E+06 0.36856E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.205          51.882          3.7519          3.7098
v  Velocity[Y]            -6.9496          8.6609     -0.00048004       0.0003142
v  Velocity[Z]            -24.795           16.96        -0.11713       -0.050092
v  ǁVelocityǁ            0.015847          52.292           3.938          3.7641
v  Pressure               -1471.8          205.91          186.53           193.1
v  k                   1.7495e-07          7.1295        0.055367         0.04078
v  omega               0.00051486      7.7259e+05          4493.8          1479.5
v  TempC                  -100.73          615.44          22.498          20.886
v  Density                0.40443          2.1662          1.2321          1.2521
v  TurbVisc            8.8217e-13       0.0022897      4.7263e-05      7.1464e-05
v  CourantNb                    0          32.555         0.68285         0.48671
v  FourierNb            0.0024639           4.199        0.052587        0.061983
v  total_pressure           99853      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4085          2.1662          1.1556          1.2116


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016595          32.651         0.73544          0.5487


 TIME FOR THE TIME STEP              113:        0.62908E+02

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


 INSTANT    0.933000000E-02   TIME STEP NUMBER             114
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.190111362E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846080E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55652E+02 0.57561E+01
   Friction velocity        uet   :  0.58151E-02 0.44192E+01
   Friction velocity        uk    :  0.17280E-01 0.15023E+01
   Dimensionless distance   yplus :  0.19223E+00 0.35392E+02
   Friction thermal sca.    tstar : -0.55519E+03 0.30735E+02
   Rough dim-less th. sca.  tplus :  0.14343E+00 0.12450E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     153874
   Nb of faces within the viscous sub-layer     :       3541
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        111 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20089E+00      25   0.16025E-01   0.26263E+02 0.12771E+03 
c  Velocity[X]                                      0.23842E+02 
c  Velocity[Y]                                      0.60097E+00 
c  Velocity[Z]                                      0.18199E+01 
c  Pressure     0.10446E-03     154   0.59846E-02   0.17394E+00 0.46765E+02 
c  k            0.49652E-02      17   0.90322E-03   0.28561E+01 0.92624E+03 
c  omega        0.12946E+03      34   0.16152E-03   0.54338E+09 0.60489E+03 
c  TempC        0.22989E+04      46   0.29012E-01   0.12563E+06 0.36708E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1845          52.083          3.7534          3.7125
v  Velocity[Y]             -6.933          8.4489     -0.00046425      0.00031362
v  Velocity[Z]            -25.133          17.165        -0.11817       -0.050499
v  ǁVelocityǁ            0.012604          52.468          3.9409          3.7672
v  Pressure               -1466.3          206.91          187.43             194
v  k                   1.8208e-07          7.0816        0.055778        0.041149
v  omega                 0.000559      5.6855e+05          4494.9          1477.1
v  TempC                  -101.24          611.86          22.696          21.113
v  Density                0.39746          2.0484          1.2316          1.2517
v  TurbVisc             9.028e-13       0.0022896      4.7843e-05      7.2331e-05
v  CourantNb                    0          30.946         0.68334         0.48709
v  FourierNb            0.0024642           4.199        0.053092        0.062678
v  total_pressure           99859      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40011          1.9956          1.1551          1.2111


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01857          31.038         0.73643         0.54976


 TIME FOR THE TIME STEP              114:        0.63267E+02

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


 INSTANT    0.943000000E-02   TIME STEP NUMBER             115
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.122245436E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155844528E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53213E+02 0.56778E+01
   Friction velocity        uet   :  0.51580E-02 0.43966E+01
   Friction velocity        uk    :  0.16538E-01 0.15025E+01
   Dimensionless distance   yplus :  0.18762E+00 0.36435E+02
   Friction thermal sca.    tstar : -0.46135E+03 0.29674E+02
   Rough dim-less th. sca.  tplus :  0.13999E+00 0.12519E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     153596
   Nb of faces within the viscous sub-layer     :       3557
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        110 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20093E+00      25   0.15888E-01   0.26192E+02 0.12739E+03 
c  Velocity[X]                                      0.23839E+02 
c  Velocity[Y]                                      0.59882E+00 
c  Velocity[Z]                                      0.17537E+01 
c  Pressure     0.10344E-03     145   0.58197E-02   0.17228E+00 0.45967E+02 
c  k            0.49838E-02      17   0.90913E-03   0.28773E+01 0.92563E+03 
c  omega        0.12885E+03      33   0.12434E-03   0.49169E+09 0.57501E+03 
c  TempC        0.23103E+04      46   0.29031E-01   0.12482E+06 0.36389E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1886          51.817          3.7551          3.7151
v  Velocity[Y]            -6.9073          8.5669     -0.00045305      0.00031525
v  Velocity[Z]             -24.77          17.443         -0.1192       -0.050905
v  ǁVelocityǁ            0.010068          52.229          3.9439          3.7702
v  Pressure               -1464.4          208.01          188.29          194.88
v  k                   1.9175e-07          7.1077        0.056191        0.041514
v  omega               0.00059335      5.6892e+05          4495.8          1474.6
v  TempC                  -101.42          597.41          22.892          21.339
v  Density                0.39907          2.0545          1.2312          1.2512
v  TurbVisc            9.3875e-13       0.0022897      4.8433e-05      7.3205e-05
v  CourantNb                    0          32.506         0.68383         0.48746
v  FourierNb            0.0024644           4.199        0.053605         0.06338
v  total_pressure           99861      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39907          1.9728          1.1546          1.2106


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01893          32.602         0.73743         0.55084


 TIME FOR THE TIME STEP              115:        0.62673E+02

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


 INSTANT    0.953000000E-02   TIME STEP NUMBER             116
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.229903868E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845967E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56399E+02 0.58131E+01
   Friction velocity        uet   :  0.32861E-02 0.44252E+01
   Friction velocity        uk    :  0.16456E-01 0.15020E+01
   Dimensionless distance   yplus :  0.25106E+00 0.35915E+02
   Friction thermal sca.    tstar : -0.54318E+03 0.30606E+02
   Rough dim-less th. sca.  tplus :  0.18732E+00 0.12485E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     153349
   Nb of faces within the viscous sub-layer     :       3582
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        111 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20097E+00      26   0.15888E-01   0.25889E+02 0.12650E+03 
c  Velocity[X]                                      0.23533E+02 
c  Velocity[Y]                                      0.57998E+00 
c  Velocity[Z]                                      0.17763E+01 
c  Pressure     0.10329E-03     147   0.58489E-02   0.17164E+00 0.43703E+02 
c  k            0.49985E-02      17   0.92295E-03   0.29093E+01 0.92682E+03 
c  omega        0.12885E+03      33   0.14508E-03   0.44868E+09 0.54887E+03 
c  TempC        0.23214E+04      45   0.29758E-01   0.12440E+06 0.36131E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1394          52.104          3.7566          3.7178
v  Velocity[Y]            -6.8675          8.4676     -0.00045194      0.00031646
v  Velocity[Z]            -25.117          17.048        -0.12024        -0.05132
v  ǁVelocityǁ            0.012694          52.494          3.9467          3.7732
v  Pressure               -1458.7          208.76          189.12          195.73
v  k                   2.0228e-07          7.2205        0.056605        0.041878
v  omega               0.00076617      5.6977e+05          4496.3          1472.1
v  TempC                  -108.13          615.15          23.089          21.566
v  Density                 0.4057          2.0566          1.2307          1.2508
v  TurbVisc            9.8781e-13       0.0022897      4.9035e-05      7.4089e-05
v  CourantNb                    0          31.001         0.68433         0.48784
v  FourierNb            0.0024646           4.199        0.054136        0.064095
v  total_pressure           99866      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41454          2.0566          1.1541          1.2102


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018824          31.093         0.73846         0.55193


 TIME FOR THE TIME STEP              116:        0.62854E+02

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


 INSTANT    0.963000000E-02   TIME STEP NUMBER             117
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.144816232E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845438E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53684E+02 0.58306E+01
   Friction velocity        uet   :  0.68438E-03 0.44009E+01
   Friction velocity        uk    :  0.17749E-01 0.15164E+01
   Dimensionless distance   yplus :  0.20340E+00 0.35852E+02
   Friction thermal sca.    tstar : -0.48220E+03 0.30439E+02
   Rough dim-less th. sca.  tplus :  0.15176E+00 0.12481E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     153058
   Nb of faces within the viscous sub-layer     :       3634
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        112 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20101E+00      25   0.16455E-01   0.26053E+02 0.12674E+03 
c  Velocity[X]                                      0.23664E+02 
c  Velocity[Y]                                      0.58588E+00 
c  Velocity[Z]                                      0.18025E+01 
c  Pressure     0.10398E-03     146   0.58625E-02   0.17275E+00 0.41160E+02 
c  k            0.50102E-02      17   0.93132E-03   0.29311E+01 0.92626E+03 
c  omega        0.12892E+03      34   0.12946E-03   0.66619E+09 0.66769E+03 
c  TempC        0.23324E+04      46   0.29291E-01   0.12557E+06 0.36106E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0787          51.656          3.7582          3.7204
v  Velocity[Y]            -6.7607          8.4945     -0.00045483      0.00031969
v  Velocity[Z]            -24.906           17.07        -0.12129        -0.05173
v  ǁVelocityǁ           0.0089645          52.065          3.9497          3.7763
v  Pressure               -1456.5          209.34           189.9          196.53
v  k                    2.144e-07          7.2318        0.057027         0.04224
v  omega                0.0013234      6.8025e+05          4498.3          1469.9
v  TempC                  -114.77          602.57          23.286          21.792
v  Density                0.39759          2.1402          1.2303          1.2504
v  TurbVisc            1.0413e-12       0.0022901       4.963e-05      7.4958e-05
v  CourantNb                    0          32.409         0.68482         0.48821
v  FourierNb            0.0024648           4.199        0.054663        0.064803
v  total_pressure           99868      1.0153e+05      1.0151e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39759          2.1402          1.1536          1.2097


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01907          32.505         0.73948         0.55302


 TIME FOR THE TIME STEP              117:        0.62730E+02

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


 INSTANT    0.973000000E-02   TIME STEP NUMBER             118
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.219490870E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846848E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56248E+02 0.58260E+01
   Friction velocity        uet   :  0.15455E-02 0.44138E+01
   Friction velocity        uk    :  0.17760E-01 0.15123E+01
   Dimensionless distance   yplus :  0.17610E+00 0.35854E+02
   Friction thermal sca.    tstar : -0.53189E+03 0.30642E+02
   Rough dim-less th. sca.  tplus :  0.13139E+00 0.12481E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     152794
   Nb of faces within the viscous sub-layer     :       3671
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        114 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20105E+00      25   0.16652E-01   0.26204E+02 0.12696E+03 
c  Velocity[X]                                      0.23798E+02 
c  Velocity[Y]                                      0.60583E+00 
c  Velocity[Z]                                      0.18007E+01 
c  Pressure     0.10509E-03     131   0.60151E-02   0.17442E+00 0.31828E+02 
c  k            0.50175E-02      17   0.93240E-03   0.29303E+01 0.92203E+03 
c  omega        0.12911E+03      34   0.17642E-03   0.96882E+09 0.80346E+03 
c  TempC        0.23431E+04      47   0.28638E-01   0.12628E+06 0.36016E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9758          52.008          3.7598          3.7231
v  Velocity[Y]            -6.9363          8.3904     -0.00044108       0.0003229
v  Velocity[Z]            -25.142          17.465        -0.12237       -0.052151
v  ǁVelocityǁ           0.0084188          52.403          3.9526          3.7793
v  Pressure               -1450.7          209.82          190.49          197.15
v  k                   2.0756e-07          7.3555        0.057454        0.042604
v  omega                0.0025454      7.4581e+05          4500.7          1467.7
v  TempC                  -120.67          607.01          23.485          22.019
v  Density                0.40331            2.23          1.2298          1.2499
v  TurbVisc            1.1029e-12       0.0022903      5.0215e-05      7.5811e-05
v  CourantNb                    0          30.862         0.68531         0.48859
v  FourierNb             0.002465           4.199        0.055182          0.0655
v  total_pressure           99874      1.0153e+05      1.0152e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41373            2.23          1.1531          1.2092


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017874          30.954         0.74049         0.55409


 TIME FOR THE TIME STEP              118:        0.61838E+02

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


 INSTANT    0.983000000E-02   TIME STEP NUMBER             119
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.101441215E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846625E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53951E+02 0.58836E+01
   Friction velocity        uet   :  0.40159E-02 0.43964E+01
   Friction velocity        uk    :  0.62543E-02 0.15259E+01
   Dimensionless distance   yplus :  0.75680E-01 0.36696E+02
   Friction thermal sca.    tstar : -0.15748E+04 0.30918E+02
   Rough dim-less th. sca.  tplus :  0.56466E-01 0.12536E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     152628
   Nb of faces within the viscous sub-layer     :       3691
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        116 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20109E+00      26   0.15925E-01   0.26494E+02 0.12750E+03 
c  Velocity[X]                                      0.24025E+02 
c  Velocity[Y]                                      0.61404E+00 
c  Velocity[Z]                                      0.18553E+01 
c  Pressure     0.10676E-03     147   0.60143E-02   0.17728E+00 0.35577E+02 
c  k            0.50229E-02      17   0.93459E-03   0.29354E+01 0.91888E+03 
c  omega        0.12969E+03      33   0.18232E-03   0.55525E+09 0.60869E+03 
c  TempC        0.23538E+04      45   0.28647E-01   0.12555E+06 0.35723E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9415          51.688          3.7615          3.7257
v  Velocity[Y]            -7.0695          8.5351     -0.00044045      0.00032803
v  Velocity[Z]             -24.84          17.102        -0.12342       -0.052572
v  ǁVelocityǁ            0.021604          52.094          3.9556          3.7824
v  Pressure               -1448.6          210.66          191.19          197.84
v  k                   2.4121e-07          7.3684        0.057883        0.042965
v  omega                0.0054867      3.9466e+05          4501.1          1465.4
v  TempC                  -125.95          605.41          23.683          22.245
v  Density                0.40127          2.3163          1.2294          1.2495
v  TurbVisc             1.167e-12       0.0022903      5.0802e-05      7.6668e-05
v  CourantNb                    0          32.455         0.68581         0.48897
v  FourierNb            0.0024653           4.199        0.055709        0.066204
v  total_pressure           99876      1.0154e+05      1.0152e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41322          2.3163          1.1526          1.2088


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018858           32.55         0.74152         0.55517


 TIME FOR THE TIME STEP              119:        0.62944E+02

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


 INSTANT    0.993000000E-02   TIME STEP NUMBER             120
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.257530706E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155847386E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56958E+02 0.59999E+01
   Friction velocity        uet   :  0.50704E-02 0.44205E+01
   Friction velocity        uk    :  0.14145E-01 0.15238E+01
   Dimensionless distance   yplus :  0.22502E+00 0.35988E+02
   Friction thermal sca.    tstar : -0.34064E+03 0.30563E+02
   Rough dim-less th. sca.  tplus :  0.16789E+00 0.12490E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     152364
   Nb of faces within the viscous sub-layer     :       3723
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        118 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20113E+00      25   0.16546E-01   0.26236E+02 0.12673E+03 
c  Velocity[X]                                      0.23792E+02 
c  Velocity[Y]                                      0.61374E+00 
c  Velocity[Z]                                      0.18298E+01 
c  Pressure     0.10657E-03     136   0.59400E-02   0.17666E+00 0.34686E+02 
c  k            0.50288E-02      17   0.93189E-03   0.29606E+01 0.91908E+03 
c  omega        0.12900E+03      34   0.17862E-03   0.94098E+09 0.79078E+03 
c  TempC        0.23642E+04      46   0.28320E-01   0.12448E+06 0.35385E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9173          52.093          3.7631          3.7283
v  Velocity[Y]            -6.8784          8.4078     -0.00043324      0.00032925
v  Velocity[Z]            -25.114           17.04        -0.12451       -0.052995
v  ǁVelocityǁ            0.016069          52.494          3.9586          3.7854
v  Pressure               -1441.9          211.12          191.88          198.52
v  k                   1.1021e-07          7.3361        0.058311        0.043322
v  omega                 0.013119      8.3743e+05            4503          1463.3
v  TempC                  -131.01          592.48          23.885          22.472
v  Density                  0.402          2.3993          1.2289          1.2491
v  TurbVisc            1.2392e-12       0.0022902      5.1394e-05       7.753e-05
v  CourantNb                    0          30.919         0.68632         0.48934
v  FourierNb            0.0024655           4.199        0.056236        0.066912
v  total_pressure           99883      1.0154e+05      1.0152e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40587          2.3993          1.1522          1.2083


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016883          31.011         0.74255         0.55626


 TIME FOR THE TIME STEP              120:        0.62060E+02

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


 INSTANT    0.100300000E-01   TIME STEP NUMBER             121
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.101385981E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155844755E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54483E+02 0.58972E+01
   Friction velocity        uet   :  0.31132E-02 0.44051E+01
   Friction velocity        uk    :  0.23830E-01 0.15255E+01
   Dimensionless distance   yplus :  0.29403E+00 0.35970E+02
   Friction thermal sca.    tstar : -0.35944E+03 0.30922E+02
   Rough dim-less th. sca.  tplus :  0.21938E+00 0.12488E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     152104
   Nb of faces within the viscous sub-layer     :       3728
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        120 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20116E+00      25   0.16667E-01   0.26186E+02 0.12645E+03 
c  Velocity[X]                                      0.23742E+02 
c  Velocity[Y]                                      0.60667E+00 
c  Velocity[Z]                                      0.18375E+01 
c  Pressure     0.10570E-03     155   0.58615E-02   0.17531E+00 0.52181E+02 
c  k            0.50388E-02      17   0.92610E-03   0.29931E+01 0.92051E+03 
c  omega        0.12984E+03      34   0.18111E-03   0.74185E+09 0.70212E+03 
c  TempC        0.23743E+04      46   0.28488E-01   0.12464E+06 0.35226E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8669          51.585          3.7647          3.7309
v  Velocity[Y]            -6.7547          8.3817     -0.00042048      0.00033617
v  Velocity[Z]             -24.87          17.406        -0.12557        -0.05341
v  ǁVelocityǁ            0.012378          51.999          3.9616          3.7884
v  Pressure               -1439.3          212.28          192.91          199.55
v  k                   1.2303e-07          7.4046        0.058734        0.043677
v  omega                 0.074959       5.035e+05          4503.9          1461.1
v  TempC                  -134.11          594.68          24.087          22.698
v  Density                0.40801          2.4847          1.2285          1.2487
v  TurbVisc            3.9912e-12         0.00229      5.1983e-05      7.8392e-05
v  CourantNb                    0          32.371         0.68682         0.48972
v  FourierNb            0.0024657           4.199        0.056763        0.067618
v  total_pressure           99886      1.0154e+05      1.0152e+05      1.0152e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41582          2.4847          1.1517          1.2078


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018488          32.466         0.74359         0.55734


 TIME FOR THE TIME STEP              121:        0.63302E+02

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


 INSTANT    0.101300000E-01   TIME STEP NUMBER             122
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.149530976E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155843415E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57011E+02 0.60569E+01
   Friction velocity        uet   :  0.19946E-02 0.44183E+01
   Friction velocity        uk    :  0.16601E-01 0.15282E+01
   Dimensionless distance   yplus :  0.31933E+00 0.36168E+02
   Friction thermal sca.    tstar : -0.37208E+03 0.31330E+02
   Rough dim-less th. sca.  tplus :  0.23825E+00 0.12501E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     151926
   Nb of faces within the viscous sub-layer     :       3773
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        121 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20120E+00      25   0.16560E-01   0.26227E+02 0.12640E+03 
c  Velocity[X]                                      0.23738E+02 
c  Velocity[Y]                                      0.61138E+00 
c  Velocity[Z]                                      0.18777E+01 
c  Pressure     0.10572E-03     138   0.59501E-02   0.17505E+00 0.43336E+02 
c  k            0.50527E-02      17   0.92116E-03   0.30142E+01 0.92013E+03 
c  omega        0.12914E+03      34   0.23099E-03   0.93003E+09 0.78474E+03 
c  TempC        0.23843E+04      46   0.27829E-01   0.12548E+06 0.35166E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8451          51.857          3.7664          3.7336
v  Velocity[Y]            -6.7241          8.4266     -0.00040364      0.00033979
v  Velocity[Z]            -25.261          17.116        -0.12666       -0.053835
v  ǁVelocityǁ            0.014869          52.258          3.9646          3.7915
v  Pressure               -1433.4          213.11          193.73          200.41
v  k                   6.8983e-08          7.5461        0.059148        0.044031
v  omega                  0.38702      8.2352e+05          4505.5          1459.1
v  TempC                  -138.08          600.37          24.289          22.924
v  Density                0.40697          2.5402           1.228          1.2482
v  TurbVisc            6.5042e-13       0.0022899      5.2566e-05      7.9251e-05
v  CourantNb                    0          30.806         0.68733          0.4901
v  FourierNb            0.0024659           4.199        0.057279        0.068319
v  total_pressure           99892      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40697          2.5402          1.1512          1.2074


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018535          30.898         0.74461         0.55842


 TIME FOR THE TIME STEP              122:        0.62206E+02

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


 INSTANT    0.102300000E-01   TIME STEP NUMBER             123
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.505435139E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155843868E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54437E+02 0.60385E+01
   Friction velocity        uet   :  0.34614E-02 0.43897E+01
   Friction velocity        uk    :  0.12516E-01 0.15445E+01
   Dimensionless distance   yplus :  0.20510E+00 0.37208E+02
   Friction thermal sca.    tstar : -0.66739E+03 0.32047E+02
   Rough dim-less th. sca.  tplus :  0.15303E+00 0.12569E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     151724
   Nb of faces within the viscous sub-layer     :       3774
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        123 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20124E+00      25   0.16237E-01   0.26426E+02 0.12673E+03 
c  Velocity[X]                                      0.23979E+02 
c  Velocity[Y]                                      0.61350E+00 
c  Velocity[Z]                                      0.18332E+01 
c  Pressure     0.10555E-03     153   0.59763E-02   0.17495E+00 0.53164E+02 
c  k            0.50724E-02      17   0.92824E-03   0.30304E+01 0.91900E+03 
c  omega        0.12987E+03      34   0.12145E-03   0.52134E+09 0.58800E+03 
c  TempC        0.23945E+04      46   0.27970E-01   0.12470E+06 0.34880E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8184          51.628          3.7681          3.7362
v  Velocity[Y]            -6.7677          8.4942     -0.00040476      0.00034578
v  Velocity[Z]             -24.92          17.506        -0.12775       -0.054263
v  ǁVelocityǁ            0.019282          52.065          3.9677          3.7945
v  Pressure               -1430.3          214.26          194.77          201.47
v  k                   2.7338e-07          7.5705        0.059547        0.044384
v  omega                  0.79066      4.2844e+05          4505.1            1457
v  TempC                  -141.93          591.82           24.49           23.15
v  Density                0.40432          2.6147          1.2275          1.2478
v  TurbVisc            1.5778e-12       0.0022898      5.3153e-05      8.0116e-05
v  CourantNb                    0          32.361         0.68786         0.49048
v  FourierNb            0.0024662           4.199        0.057801        0.069025
v  total_pressure           99895      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4163          2.6147          1.1507          1.2069


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.0186          32.457         0.74566          0.5595


 TIME FOR THE TIME STEP              123:        0.63206E+02

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


 INSTANT    0.103300000E-01   TIME STEP NUMBER             124
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.241702024E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155844452E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57884E+02 0.60575E+01
   Friction velocity        uet   :  0.17096E-02 0.44204E+01
   Friction velocity        uk    :  0.18927E-01 0.15429E+01
   Dimensionless distance   yplus :  0.28778E+00 0.36831E+02
   Friction thermal sca.    tstar : -0.41905E+03 0.32161E+02
   Rough dim-less th. sca.  tplus :  0.21472E+00 0.12545E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     151486
   Nb of faces within the viscous sub-layer     :       3791
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        124 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20128E+00      25   0.16740E-01   0.26216E+02 0.12608E+03 
c  Velocity[X]                                      0.23764E+02 
c  Velocity[Y]                                      0.61824E+00 
c  Velocity[Z]                                      0.18336E+01 
c  Pressure     0.10516E-03     130   0.59660E-02   0.17388E+00 0.34721E+02 
c  k            0.50967E-02      17   0.93931E-03   0.30487E+01 0.91822E+03 
c  omega        0.12913E+03      35   0.18132E-03   0.21591E+10 0.11895E+04 
c  TempC        0.24047E+04      47   0.28403E-01   0.12421E+06 0.34638E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7922          51.962          3.7697          3.7388
v  Velocity[Y]            -6.9459          8.5699     -0.00038748      0.00034882
v  Velocity[Z]             -25.19          17.438        -0.12886       -0.054694
v  ǁVelocityǁ            0.019908          52.368          3.9707          3.7976
v  Pressure               -1423.4          214.59           195.4          202.16
v  k                   1.0159e-08          7.5599        0.059931        0.044735
v  omega                  0.05972      2.5618e+06          4507.1            1455
v  TempC                  -143.65          593.45          24.691          23.377
v  Density                0.40832          2.6916          1.2271          1.2474
v  TurbVisc            1.8065e-12       0.0022902      5.3733e-05      8.0971e-05
v  CourantNb                    0           30.87         0.68836         0.49086
v  FourierNb            0.0024664           4.199        0.058311        0.069721
v  total_pressure           99902      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40832          2.6916          1.1503          1.2065


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018895          30.961         0.74667         0.56058


 TIME FOR THE TIME STEP              124:        0.62101E+02

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


 INSTANT    0.104300000E-01   TIME STEP NUMBER             125
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.438614336E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845866E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55022E+02 0.60732E+01
   Friction velocity        uet   :  0.97453E-03 0.43995E+01
   Friction velocity        uk    :  0.18473E-01 0.15458E+01
   Dimensionless distance   yplus :  0.30420E+00 0.37486E+02
   Friction thermal sca.    tstar : -0.41292E+03 0.33228E+02
   Rough dim-less th. sca.  tplus :  0.22697E+00 0.12587E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     151309
   Nb of faces within the viscous sub-layer     :       3809
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        126 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20132E+00      26   0.16268E-01   0.26413E+02 0.12640E+03 
c  Velocity[X]                                      0.23898E+02 
c  Velocity[Y]                                      0.62439E+00 
c  Velocity[Z]                                      0.18909E+01 
c  Pressure     0.10654E-03     131   0.58615E-02   0.17620E+00 0.29898E+02 
c  k            0.51255E-02      18   0.94020E-03   0.30642E+01 0.91697E+03 
c  omega        0.13909E+03      34   0.14410E-03   0.88994E+09 0.76624E+03 
c  TempC        0.24149E+04      46   0.28140E-01   0.12490E+06 0.34564E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8623          51.278          3.7714          3.7415
v  Velocity[Y]            -6.8708          8.4057     -0.00037699      0.00035794
v  Velocity[Z]            -24.835           17.14        -0.12997       -0.055125
v  ǁVelocityǁ            0.027173          51.702          3.9738          3.8006
v  Pressure               -1420.9          214.95          195.98          202.75
v  k                   7.5639e-08          7.6357        0.060302        0.045087
v  omega                  0.49148      1.2999e+06          4506.5            1453
v  TempC                  -115.53           591.4          24.889          23.602
v  Density                0.40755          2.7273          1.2267          1.2469
v  TurbVisc            1.3098e-13       0.0022904      5.4307e-05       8.182e-05
v  CourantNb                    0          32.242         0.68888         0.49124
v  FourierNb            0.0024667           4.199        0.058814         0.07041
v  total_pressure           99904      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40975          2.7273          1.1498           1.206


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018839          32.336         0.74769         0.56165


 TIME FOR THE TIME STEP              125:        0.62081E+02

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


 INSTANT    0.105300000E-01   TIME STEP NUMBER             126
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.103927455E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155847565E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57429E+02 0.62076E+01
   Friction velocity        uet   :  0.36764E-02 0.44250E+01
   Friction velocity        uk    :  0.98237E-02 0.15508E+01
   Dimensionless distance   yplus :  0.12030E+00 0.37138E+02
   Friction thermal sca.    tstar : -0.50808E+03 0.32655E+02
   Rough dim-less th. sca.  tplus :  0.89754E-01 0.12564E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     151175
   Nb of faces within the viscous sub-layer     :       3860
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        128 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20136E+00      26   0.16853E-01   0.26163E+02 0.12565E+03 
c  Velocity[X]                                      0.23674E+02 
c  Velocity[Y]                                      0.62346E+00 
c  Velocity[Z]                                      0.18650E+01 
c  Pressure     0.10591E-03     146   0.59794E-02   0.17474E+00 0.35907E+02 
c  k            0.51544E-02      17   0.92894E-03   0.30703E+01 0.91430E+03 
c  omega        0.12992E+03      34   0.21598E-03   0.97466E+09 0.80090E+03 
c  TempC        0.24252E+04      46   0.27375E-01   0.12512E+06 0.34426E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9112          51.689           3.773          3.7441
v  Velocity[Y]              -6.92          8.4366     -0.00035272       0.0003607
v  Velocity[Z]            -25.326           17.43         -0.1311       -0.055563
v  ǁVelocityǁ            0.016607           52.09          3.9767          3.8036
v  Pressure               -1414.2          215.98          196.72          203.47
v  k                    8.776e-08          7.6582        0.060662        0.045439
v  omega                  0.15757      1.1382e+06          4508.8          1451.1
v  TempC                  -120.33           601.5          25.086          23.828
v  Density                0.40852          2.2407          1.2262          1.2465
v  TurbVisc            9.7306e-13       0.0022902      5.4877e-05      8.2662e-05
v  CourantNb                    0          30.611         0.68939         0.49162
v  FourierNb            0.0024669           4.199        0.059315        0.071093
v  total_pressure           99911      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41332          2.2407          1.1493          1.2056


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.0187          30.702          0.7487         0.56271


 TIME FOR THE TIME STEP              126:        0.63155E+02

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


 INSTANT    0.106300000E-01   TIME STEP NUMBER             127
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.184377878E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846494E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55188E+02 0.60527E+01
   Friction velocity        uet   :  0.47058E-02 0.43823E+01
   Friction velocity        uk    :  0.13945E-01 0.15566E+01
   Dimensionless distance   yplus :  0.24803E+00 0.37203E+02
   Friction thermal sca.    tstar : -0.39817E+03 0.34321E+02
   Rough dim-less th. sca.  tplus :  0.18506E+00 0.12569E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     150988
   Nb of faces within the viscous sub-layer     :       3899
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        129 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20140E+00      25   0.17005E-01   0.26439E+02 0.12616E+03 
c  Velocity[X]                                      0.23947E+02 
c  Velocity[Y]                                      0.62158E+00 
c  Velocity[Z]                                      0.18704E+01 
c  Pressure     0.10588E-03     155   0.60392E-02   0.17481E+00 0.47630E+02 
c  k            0.51826E-02      18   0.92235E-03   0.30860E+01 0.91316E+03 
c  omega        0.12975E+03      35   0.16046E-03   0.87244E+09 0.75711E+03 
c  TempC        0.24358E+04      46   0.26734E-01   0.12432E+06 0.34151E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9587          51.267          3.7746          3.7467
v  Velocity[Y]            -6.9021          8.5255     -0.00033838      0.00036934
v  Velocity[Z]            -24.884          17.331        -0.13222       -0.056002
v  ǁVelocityǁ           0.0098613          51.734          3.9798          3.8067
v  Pressure                 -1411          216.97          197.69          204.43
v  k                   1.5684e-07          7.7525        0.061015        0.045789
v  omega                  0.15513      7.2009e+05          4510.5          1449.4
v  TempC                  -124.73          590.45           25.28          24.054
v  Density                 0.4038          2.3111          1.2258          1.2461
v  TurbVisc            3.7563e-13       0.0022901      5.5456e-05      8.3514e-05
v  CourantNb                    0          32.207          0.6899           0.492
v  FourierNb            0.0024671           4.199        0.059824        0.071787
v  total_pressure           99914      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4038          2.3111          1.1489          1.2051


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018256          32.301         0.74973         0.56379


 TIME FOR THE TIME STEP              127:        0.63464E+02

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


 INSTANT    0.107300000E-01   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.300296793E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155844292E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58301E+02 0.62463E+01
   Friction velocity        uet   :  0.18100E-02 0.44228E+01
   Friction velocity        uk    :  0.10782E-01 0.15584E+01
   Dimensionless distance   yplus :  0.11706E+00 0.37472E+02
   Friction thermal sca.    tstar : -0.29196E+03 0.35513E+02
   Rough dim-less th. sca.  tplus :  0.87341E-01 0.12586E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     150798
   Nb of faces within the viscous sub-layer     :       3950
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        135 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20143E+00      25   0.16453E-01   0.26417E+02 0.12596E+03 
c  Velocity[X]                                      0.23885E+02 
c  Velocity[Y]                                      0.61558E+00 
c  Velocity[Z]                                      0.19163E+01 
c  Pressure     0.10570E-03     129   0.58311E-02   0.17451E+00 0.32399E+02 
c  k            0.52087E-02      18   0.91045E-03   0.31096E+01 0.91333E+03 
c  omega        0.12960E+03      34   0.14661E-03   0.72651E+09 0.69021E+03 
c  TempC        0.24465E+04      46   0.27286E-01   0.12289E+06 0.33790E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9773          51.697          3.7762          3.7493
v  Velocity[Y]            -6.9011          8.3968     -0.00031101      0.00037977
v  Velocity[Z]             -25.25           17.43        -0.13336       -0.056449
v  ǁVelocityǁ            0.015886          52.104          3.9827          3.8097
v  Pressure               -1404.3          217.66          198.29          205.08
v  k                   3.1574e-07          7.8516        0.061364        0.046135
v  omega                  0.20171       5.922e+05          4512.7          1447.7
v  TempC                  -128.71          601.09          25.474          24.281
v  Density                0.40896          2.3797          1.2253          1.2456
v  TurbVisc            6.6825e-13       0.0022899      5.6038e-05      8.4369e-05
v  CourantNb                    0           30.65          0.6904         0.49238
v  FourierNb            0.0024674           4.199        0.060328        0.072482
v  total_pressure           99921      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40896          2.3797          1.1485          1.2047


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016406          30.741         0.75073         0.56486


 TIME FOR THE TIME STEP              128:        0.61751E+02

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


 INSTANT    0.108300000E-01   TIME STEP NUMBER             129
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.260776246E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846623E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55607E+02 0.62412E+01
   Friction velocity        uet   :  0.47706E-02 0.44180E+01
   Friction velocity        uk    :  0.20796E-01 0.15717E+01
   Dimensionless distance   yplus :  0.31222E+00 0.37624E+02
   Friction thermal sca.    tstar : -0.43041E+03 0.36483E+02
   Rough dim-less th. sca.  tplus :  0.23295E+00 0.12595E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     150631
   Nb of faces within the viscous sub-layer     :       3988
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        138 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20148E+00      25   0.16895E-01   0.26161E+02 0.12520E+03 
c  Velocity[X]                                      0.23648E+02 
c  Velocity[Y]                                      0.62053E+00 
c  Velocity[Z]                                      0.18922E+01 
c  Pressure     0.10503E-03     150   0.58539E-02   0.17294E+00 0.41590E+02 
c  k            0.52337E-02      18   0.89966E-03   0.31271E+01 0.91265E+03 
c  omega        0.12963E+03      35   0.17039E-03   0.55943E+09 0.60524E+03 
c  TempC        0.24571E+04      46   0.28357E-01   0.12384E+06 0.33760E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9381          51.081          3.7778           3.752
v  Velocity[Y]             -6.752          8.4034      -0.0003005      0.00038888
v  Velocity[Z]            -24.955          17.286         -0.1345       -0.056891
v  ǁVelocityǁ            0.018368          51.533          3.9857          3.8128
v  Pressure               -1401.3          218.61          199.12          205.93
v  k                   1.5021e-07          7.7942        0.061714         0.04648
v  omega                 0.052935      5.7094e+05          4514.2          1445.9
v  TempC                  -131.36          596.87          25.667          24.507
v  Density                0.40399          2.4452          1.2249          1.2452
v  TurbVisc            1.3392e-12       0.0022897      5.6623e-05      8.5229e-05
v  CourantNb                    0          32.079         0.69091         0.49276
v  FourierNb            0.0024676           4.199        0.060836         0.07318
v  total_pressure           99924      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40743          2.4452           1.148          1.2043


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017861          32.173         0.75175         0.56594


 TIME FOR THE TIME STEP              129:        0.63289E+02

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


 INSTANT    0.109300000E-01   TIME STEP NUMBER             130
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.250836688E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845934E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58270E+02 0.62651E+01
   Friction velocity        uet   :  0.46381E-02 0.43918E+01
   Friction velocity        uk    :  0.26023E-01 0.15642E+01
   Dimensionless distance   yplus :  0.36603E+00 0.38646E+02
   Friction thermal sca.    tstar : -0.32582E+03 0.36637E+02
   Rough dim-less th. sca.  tplus :  0.27310E+00 0.12659E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     150483
   Nb of faces within the viscous sub-layer     :       4020
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        137 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20152E+00      25   0.16929E-01   0.26223E+02 0.12520E+03 
c  Velocity[X]                                      0.23737E+02 
c  Velocity[Y]                                      0.61470E+00 
c  Velocity[Z]                                      0.18714E+01 
c  Pressure     0.10544E-03     136   0.59320E-02   0.17329E+00 0.34649E+02 
c  k            0.52541E-02      18   0.88944E-03   0.31254E+01 0.90914E+03 
c  omega        0.12978E+03      34   0.47414E-03   0.22102E+10 0.11952E+04 
c  TempC        0.24676E+04      47   0.27307E-01   0.12528E+06 0.33796E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9302          51.548          3.7793          3.7546
v  Velocity[Y]            -6.7661          8.5207     -0.00026676      0.00039403
v  Velocity[Z]             -25.34          17.497        -0.13565       -0.057336
v  ǁVelocityǁ            0.017898          51.953          3.9887          3.8158
v  Pressure               -1394.4          219.05          199.82          206.63
v  k                   5.8156e-08           7.809        0.062062        0.046825
v  omega                 0.096166       1.982e+06          4517.7          1444.4
v  TempC                  -107.16           601.6          25.861          24.733
v  Density                0.40595           2.491          1.2245          1.2448
v  TurbVisc            9.4395e-13       0.0022896      5.7204e-05      8.6078e-05
v  CourantNb                    0          30.482         0.69141         0.49313
v  FourierNb            0.0024679           4.199        0.061339        0.073871
v  total_pressure           99931      1.0154e+05      1.0152e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41421           2.491          1.1476          1.2038


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014503          30.572         0.75275           0.567


 TIME FOR THE TIME STEP              130:        0.62285E+02

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


 INSTANT    0.110300000E-01   TIME STEP NUMBER             131
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.349955418E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155844879E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55940E+02 0.63148E+01
   Friction velocity        uet   :  0.34804E-02 0.44284E+01
   Friction velocity        uk    :  0.23904E-01 0.15687E+01
   Dimensionless distance   yplus :  0.26137E+00 0.38252E+02
   Friction thermal sca.    tstar : -0.30709E+03 0.40091E+02
   Rough dim-less th. sca.  tplus :  0.19501E+00 0.12635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     150299
   Nb of faces within the viscous sub-layer     :       4030
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        140 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20156E+00      26   0.16537E-01   0.26515E+02 0.12574E+03 
c  Velocity[X]                                      0.23948E+02 
c  Velocity[Y]                                      0.63399E+00 
c  Velocity[Z]                                      0.19327E+01 
c  Pressure     0.10658E-03     133   0.60008E-02   0.17521E+00 0.35149E+02 
c  k            0.52699E-02      18   0.89004E-03   0.31339E+01 0.90717E+03 
c  omega        0.14026E+03      34   0.25767E-03   0.12942E+10 0.91643E+03 
c  TempC        0.24782E+04      46   0.26788E-01   0.12420E+06 0.33493E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9066          51.008          3.7809          3.7572
v  Velocity[Y]            -6.7707          8.4837     -0.00024245      0.00040778
v  Velocity[Z]            -24.882           17.23        -0.13682       -0.057788
v  ǁVelocityǁ            0.015415          51.464          3.9917          3.8189
v  Pressure               -1391.1          220.01          200.51          207.35
v  k                   5.6145e-08          7.9487        0.062411        0.047168
v  omega                  0.16016      1.0074e+06          4517.8          1442.6
v  TempC                  -111.83          619.75          26.052          24.959
v  Density                0.40375          2.1277           1.224          1.2444
v  TurbVisc            3.6524e-13       0.0022897      5.7792e-05      8.6935e-05
v  CourantNb                    0           32.11         0.69191         0.49351
v  FourierNb            0.0024681           4.199        0.061849        0.074568
v  total_pressure           99934      1.0155e+05      1.0153e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41711          2.1277          1.1472          1.2034


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017095          32.204         0.75376         0.56808


 TIME FOR THE TIME STEP              131:        0.62193E+02

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


 INSTANT    0.111300000E-01   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.933094237E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846641E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58893E+02 0.64051E+01
   Friction velocity        uet   :  0.70542E-03 0.44403E+01
   Friction velocity        uk    :  0.13169E-01 0.15780E+01
   Dimensionless distance   yplus :  0.14406E+00 0.38204E+02
   Friction thermal sca.    tstar : -0.49243E+03 0.38649E+02
   Rough dim-less th. sca.  tplus :  0.10749E+00 0.12632E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     150131
   Nb of faces within the viscous sub-layer     :       4046
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        142 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20160E+00      26   0.17116E-01   0.26499E+02 0.12556E+03 
c  Velocity[X]                                      0.23964E+02 
c  Velocity[Y]                                      0.62862E+00 
c  Velocity[Z]                                      0.19065E+01 
c  Pressure     0.10662E-03     132   0.59531E-02   0.17498E+00 0.29692E+02 
c  k            0.52809E-02      18   0.90412E-03   0.31631E+01 0.90835E+03 
c  omega        0.13148E+03      35   0.33850E-03   0.45272E+10 0.16950E+04 
c  TempC        0.24888E+04      47   0.27133E-01   0.12292E+06 0.33165E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8647          51.494          3.7824          3.7598
v  Velocity[Y]             -6.884           8.141      -0.0001949      0.00042171
v  Velocity[Z]             -25.18          17.691          -0.138       -0.058243
v  ǁVelocityǁ            0.015821          51.892          3.9946          3.8219
v  Pressure               -1383.8          220.46           201.1          207.95
v  k                   1.1332e-07          7.9412        0.062763        0.047508
v  omega                  0.51511        3.26e+06          4520.3          1441.1
v  TempC                  -116.52          622.49          26.245          25.185
v  Density                0.39555          2.1893          1.2236          1.2439
v  TurbVisc            2.4471e-13       0.0022897      5.8396e-05       8.781e-05
v  CourantNb                    0          30.492         0.69241         0.49389
v  FourierNb            0.0024684           4.199        0.062371        0.075282
v  total_pressure           99941      1.0155e+05      1.0153e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41043          2.1893          1.1467           1.203


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.019265          30.582         0.75478         0.56917


 TIME FOR THE TIME STEP              132:        0.62269E+02

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


 INSTANT    0.112300000E-01   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.709247065E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846268E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56474E+02 0.62859E+01
   Friction velocity        uet   :  0.16589E-02 0.43756E+01
   Friction velocity        uk    :  0.22442E-01 0.15817E+01
   Dimensionless distance   yplus :  0.30853E+00 0.39249E+02
   Friction thermal sca.    tstar : -0.41130E+03 0.37947E+02
   Rough dim-less th. sca.  tplus :  0.23020E+00 0.12696E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     150009
   Nb of faces within the viscous sub-layer     :       4092
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        144 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20164E+00      26   0.17395E-01   0.26454E+02 0.12530E+03 
c  Velocity[X]                                      0.23933E+02 
c  Velocity[Y]                                      0.62834E+00 
c  Velocity[Z]                                      0.18927E+01 
c  Pressure     0.10696E-03     127   0.58704E-02   0.17562E+00 0.29984E+02 
c  k            0.52886E-02      18   0.92640E-03   0.31850E+01 0.90845E+03 
c  omega        0.18189E+03      34   0.19526E-03   0.21249E+10 0.11687E+04 
c  TempC        0.24991E+04      47   0.27648E-01   0.12359E+06 0.33104E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8257          50.968           3.784          3.7625
v  Velocity[Y]            -6.9343          8.2179     -0.00018721      0.00042986
v  Velocity[Z]            -24.789          17.336        -0.13916       -0.058702
v  ǁVelocityǁ            0.024554          51.435          3.9976           3.825
v  Pressure               -1380.1          221.21          201.67          208.56
v  k                   2.3777e-08          7.9829        0.063123        0.047847
v  omega                   1.2673      1.6561e+06          4522.4          1439.5
v  TempC                  -120.74          592.64          26.437          25.411
v  Density                0.39433          2.2549          1.2232          1.2435
v  TurbVisc            7.1085e-13       0.0022897      5.8996e-05      8.8686e-05
v  CourantNb                    0          31.931         0.69291         0.49427
v  FourierNb            0.0024687           4.199        0.062891        0.075993
v  total_pressure           99945      1.0155e+05      1.0153e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41481          2.2549          1.1463          1.2025


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020698          32.025          0.7558         0.57026


 TIME FOR THE TIME STEP              133:        0.62466E+02

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


 INSTANT    0.113300000E-01   TIME STEP NUMBER             134
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.745192465E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155848219E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59323E+02 0.64592E+01
   Friction velocity        uet   :  0.19478E-02 0.44640E+01
   Friction velocity        uk    :  0.20502E-01 0.15808E+01
   Dimensionless distance   yplus :  0.21137E+00 0.38702E+02
   Friction thermal sca.    tstar : -0.29883E+03 0.39354E+02
   Rough dim-less th. sca.  tplus :  0.15771E+00 0.12663E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     149830
   Nb of faces within the viscous sub-layer     :       4130
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        146 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20168E+00      25   0.16910E-01   0.26391E+02 0.12501E+03 
c  Velocity[X]                                      0.23808E+02 
c  Velocity[Y]                                      0.63258E+00 
c  Velocity[Z]                                      0.19503E+01 
c  Pressure     0.10661E-03     124   0.58817E-02   0.17485E+00 0.17415E+02 
c  k            0.52910E-02      18   0.94162E-03   0.31897E+01 0.90597E+03 
c  omega        0.13550E+03      35   0.22240E-03   0.93268E+09 0.77650E+03 
c  TempC        0.25091E+04      46   0.26692E-01   0.12495E+06 0.33136E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7678          51.378          3.7855          3.7651
v  Velocity[Y]            -6.9307          8.2097     -0.00015234      0.00044179
v  Velocity[Z]            -25.129          17.779        -0.14034       -0.059162
v  ǁVelocityǁ            0.023865           51.78          4.0006           3.828
v  Pressure               -1372.9          221.56          201.96          208.89
v  k                   1.1466e-07          8.0865        0.063489        0.048187
v  omega                  0.92871      8.5611e+05          4523.4          1437.9
v  TempC                  -124.68          584.81          26.629          25.637
v  Density                0.40793          2.3173          1.2227          1.2431
v  TurbVisc            1.5216e-13       0.0022898      5.9584e-05      8.9547e-05
v  CourantNb                    0          30.382          0.6934         0.49464
v  FourierNb            0.0024689           4.199        0.063402        0.076693
v  total_pressure           99952      1.0155e+05      1.0153e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41283          2.3173          1.1459          1.2021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021215          30.471          0.7568         0.57134


 TIME FOR THE TIME STEP              134:        0.62190E+02

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


 INSTANT    0.114300000E-01   TIME STEP NUMBER             135
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.152150521E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155850912E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57014E+02 0.64762E+01
   Friction velocity        uet   :  0.68429E-03 0.44642E+01
   Friction velocity        uk    :  0.16655E-01 0.15935E+01
   Dimensionless distance   yplus :  0.18562E+00 0.39157E+02
   Friction thermal sca.    tstar : -0.35573E+03 0.39077E+02
   Rough dim-less th. sca.  tplus :  0.13849E+00 0.12690E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     149716
   Nb of faces within the viscous sub-layer     :       4152
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        149 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20173E+00      25   0.16822E-01   0.26537E+02 0.12520E+03 
c  Velocity[X]                                      0.23975E+02 
c  Velocity[Y]                                      0.62867E+00 
c  Velocity[Z]                                      0.19330E+01 
c  Pressure     0.10606E-03     128   0.58890E-02   0.17407E+00 0.20102E+02 
c  k            0.52893E-02      18   0.94323E-03   0.31863E+01 0.90228E+03 
c  omega        0.13049E+03      34   0.16044E-03   0.92788E+09 0.77368E+03 
c  TempC        0.25192E+04      47   0.26366E-01   0.12494E+06 0.32985E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9253          50.949          3.7871          3.7677
v  Velocity[Y]            -6.7939          8.0064     -0.00012467      0.00045363
v  Velocity[Z]            -24.878          17.328         -0.1415       -0.059617
v  ǁVelocityǁ            0.024447          51.368          4.0036          3.8311
v  Pressure               -1368.7          221.87          202.39          209.29
v  k                   1.6082e-07          8.0592        0.063862        0.048527
v  omega                  0.53541      9.7012e+05          4524.6          1436.4
v  TempC                  -127.14          586.31          26.823          25.863
v  Density                0.41166          2.3789          1.2223          1.2426
v  TurbVisc            1.4989e-12       0.0022898      6.0169e-05      9.0405e-05
v  CourantNb                    0          31.998         0.69392         0.49503
v  FourierNb            0.0024692           4.199        0.063917        0.077392
v  total_pressure           99956      1.0155e+05      1.0153e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41381          2.3789          1.1455          1.2017


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.02097          32.091         0.75783         0.57242


 TIME FOR THE TIME STEP              135:        0.62384E+02

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


 INSTANT    0.115300000E-01   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.857172271E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155849193E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60337E+02 0.64522E+01
   Friction velocity        uet   :  0.22567E-02 0.44044E+01
   Friction velocity        uk    :  0.16709E-01 0.15873E+01
   Dimensionless distance   yplus :  0.18539E+00 0.38416E+02
   Friction thermal sca.    tstar : -0.39000E+03 0.39537E+02
   Rough dim-less th. sca.  tplus :  0.13832E+00 0.12645E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     149622
   Nb of faces within the viscous sub-layer     :       4199
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        149 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20177E+00      25   0.17263E-01   0.26589E+02 0.12518E+03 
c  Velocity[X]                                      0.24054E+02 
c  Velocity[Y]                                      0.62199E+00 
c  Velocity[Z]                                      0.19130E+01 
c  Pressure     0.10575E-03     122   0.57786E-02   0.17319E+00 0.13998E+02 
c  k            0.52848E-02      18   0.94290E-03   0.31932E+01 0.90019E+03 
c  omega        0.13101E+03      35   0.19405E-03   0.16650E+10 0.10326E+04 
c  TempC        0.25290E+04      47   0.26531E-01   0.12389E+06 0.32698E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6639          51.383          3.7886          3.7703
v  Velocity[Y]            -6.7165          8.2842     -8.9122e-05      0.00046706
v  Velocity[Z]            -25.345          17.915        -0.14268       -0.060082
v  ǁVelocityǁ            0.014618          51.806          4.0065          3.8341
v  Pressure               -1360.7          222.34          202.63          209.55
v  k                   1.3725e-07          8.0932        0.064241        0.048864
v  omega                  0.31143      1.1077e+06          4528.2          1435.1
v  TempC                   -130.7          592.32           27.02           26.09
v  Density                0.41094           2.419          1.2219          1.2422
v  TurbVisc            9.5986e-13       0.0022898      6.0751e-05      9.1269e-05
v  CourantNb                    0          30.422         0.69441          0.4954
v  FourierNb            0.0024694           4.199        0.064434        0.078097
v  total_pressure           99964      1.0155e+05      1.0153e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41094           2.419          1.1451          1.2013


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.019532          30.511         0.75884          0.5735


 TIME FOR THE TIME STEP              136:        0.62192E+02

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


 INSTANT    0.116300000E-01   TIME STEP NUMBER             137
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.185239481E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155851817E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57530E+02 0.64843E+01
   Friction velocity        uet   :  0.35679E-02 0.44651E+01
   Friction velocity        uk    :  0.15662E-01 0.15939E+01
   Dimensionless distance   yplus :  0.24430E+00 0.38486E+02
   Friction thermal sca.    tstar : -0.55657E+03 0.42779E+02
   Rough dim-less th. sca.  tplus :  0.18228E+00 0.12649E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     149431
   Nb of faces within the viscous sub-layer     :       4231
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        154 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20181E+00      26   0.17311E-01   0.26603E+02 0.12507E+03 
c  Velocity[X]                                      0.23993E+02 
c  Velocity[Y]                                      0.63053E+00 
c  Velocity[Z]                                      0.19797E+01 
c  Pressure     0.10754E-03     122   0.59161E-02   0.17589E+00 0.12048E+02 
c  k            0.52821E-02      18   0.93385E-03   0.32055E+01 0.89899E+03 
c  omega        0.13354E+03      36   0.29826E-03   0.38527E+10 0.15577E+04 
c  TempC        0.25384E+04      47   0.26984E-01   0.12379E+06 0.32540E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8049          50.617          3.7902          3.7729
v  Velocity[Y]            -6.7374          8.2333     -9.1843e-05      0.00047496
v  Velocity[Z]            -24.972          17.501        -0.14389       -0.060548
v  ǁVelocityǁ            0.017338           51.09          4.0096          3.8372
v  Pressure               -1357.2          222.59          202.84          209.76
v  k                   8.1465e-08          8.2337        0.064619        0.049199
v  omega                 0.092297      3.1008e+06          4530.7          1433.7
v  TempC                  -133.83          598.63          27.217          26.316
v  Density                0.40808          2.4793          1.2214          1.2418
v  TurbVisc            5.2421e-13       0.0022902      6.1324e-05       9.212e-05
v  CourantNb                    0          31.816         0.69491         0.49578
v  FourierNb            0.0024697           4.199        0.064941        0.078791
v  total_pressure           99968      1.0155e+05      1.0153e+05      1.0153e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41708          2.4793          1.1447          1.2008


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020153          31.909         0.75985         0.57457


 TIME FOR THE TIME STEP              137:        0.61882E+02

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


 INSTANT    0.117300000E-01   TIME STEP NUMBER             138
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.322532539E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155853501E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59738E+02 0.65981E+01
   Friction velocity        uet   :  0.14813E-02 0.44729E+01
   Friction velocity        uk    :  0.21388E-01 0.16027E+01
   Dimensionless distance   yplus :  0.24917E+00 0.39738E+02
   Friction thermal sca.    tstar : -0.37957E+03 0.47731E+02
   Rough dim-less th. sca.  tplus :  0.18591E+00 0.12726E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     149328
   Nb of faces within the viscous sub-layer     :       4258
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        153 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20186E+00      26   0.17224E-01   0.26665E+02 0.12507E+03 
c  Velocity[X]                                      0.24043E+02 
c  Velocity[Y]                                      0.64611E+00 
c  Velocity[Z]                                      0.19753E+01 
c  Pressure     0.10840E-03     126   0.61612E-02   0.17718E+00 0.18618E+02 
c  k            0.52820E-02      18   0.92628E-03   0.32197E+01 0.89811E+03 
c  omega        0.17329E+03      34   0.16262E-03   0.13362E+10 0.92366E+03 
c  TempC        0.25476E+04      46   0.26417E-01   0.12462E+06 0.32505E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9387          50.996          3.7917          3.7755
v  Velocity[Y]            -6.8886          8.1694     -7.3873e-05      0.00048326
v  Velocity[Z]             -25.28          17.966         -0.1451       -0.061028
v  ǁVelocityǁ            0.011084          51.408          4.0126          3.8402
v  Pressure               -1349.8          223.07          203.21          210.13
v  k                   3.4136e-08          8.1659        0.064993        0.049533
v  omega                 0.010858      1.5765e+06          4531.4          1432.2
v  TempC                  -136.62          605.77          27.416          26.542
v  Density                0.40513           2.535           1.221          1.2414
v  TurbVisc            3.1107e-13       0.0022904      6.1892e-05      9.2965e-05
v  CourantNb                    0          30.119         0.69542         0.49617
v  FourierNb            0.0024699           4.199        0.065443         0.07948
v  total_pressure           99975      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41341           2.535          1.1443          1.2004


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.019911          30.208         0.76086         0.57565


 TIME FOR THE TIME STEP              138:        0.61959E+02

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


 INSTANT    0.118300000E-01   TIME STEP NUMBER             139
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.118663503E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155849160E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57595E+02 0.64553E+01
   Friction velocity        uet   :  0.10435E-02 0.44041E+01
   Friction velocity        uk    :  0.20272E-01 0.16006E+01
   Dimensionless distance   yplus :  0.25516E+00 0.39360E+02
   Friction thermal sca.    tstar : -0.42699E+03 0.53288E+02
   Rough dim-less th. sca.  tplus :  0.19038E+00 0.12703E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     149147
   Nb of faces within the viscous sub-layer     :       4277
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        158 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20190E+00      26   0.16940E-01   0.26789E+02 0.12521E+03 
c  Velocity[X]                                      0.24188E+02 
c  Velocity[Y]                                      0.65037E+00 
c  Velocity[Z]                                      0.19501E+01 
c  Pressure     0.10740E-03     124   0.59888E-02   0.17560E+00 0.18573E+02 
c  k            0.52875E-02      19   0.93077E-03   0.32338E+01 0.89727E+03 
c  omega        0.13824E+03      34   0.25578E-03   0.96117E+09 0.78384E+03 
c  TempC        0.25565E+04      47   0.25916E-01   0.12458E+06 0.32360E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7413          50.628          3.7934          3.7782
v  Velocity[Y]            -6.8089          8.3726      -7.255e-05      0.00049305
v  Velocity[Z]            -24.649          17.746        -0.14632       -0.061503
v  ǁVelocityǁ           0.0091881          51.065          4.0156          3.8433
v  Pressure               -1345.4          223.33          203.59           210.5
v  k                   1.5794e-07          8.2585        0.065352        0.049866
v  omega                0.0087084      8.1339e+05          4532.6          1430.8
v  TempC                  -138.03          584.38          27.617          26.768
v  Density                0.40184          2.5868          1.2206          1.2409
v  TurbVisc            5.5425e-13       0.0022903       6.246e-05      9.3818e-05
v  CourantNb                    0          31.739         0.69592         0.49655
v  FourierNb            0.0024702           4.199        0.065944        0.080171
v  total_pressure           99980      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41299          2.5868          1.1439             1.2


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018886          31.831         0.76187         0.57672


 TIME FOR THE TIME STEP              139:        0.61891E+02

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


 INSTANT    0.119300000E-01   TIME STEP NUMBER             140
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.325991495E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155850304E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61124E+02 0.66613E+01
   Friction velocity        uet   :  0.22689E-02 0.44825E+01
   Friction velocity        uk    :  0.18921E-01 0.16034E+01
   Dimensionless distance   yplus :  0.29669E+00 0.40057E+02
   Friction thermal sca.    tstar : -0.50425E+03 0.62608E+02
   Rough dim-less th. sca.  tplus :  0.22137E+00 0.12745E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     149090
   Nb of faces within the viscous sub-layer     :       4286
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        162 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20194E+00      25   0.16756E-01   0.26600E+02 0.12462E+03 
c  Velocity[X]                                      0.24013E+02 
c  Velocity[Y]                                      0.63368E+00 
c  Velocity[Z]                                      0.19538E+01 
c  Pressure     0.10649E-03     119   0.59597E-02   0.17375E+00 0.15669E+02 
c  k            0.52994E-02      18   0.95167E-03   0.32623E+01 0.89851E+03 
c  omega        0.13110E+03      34   0.18669E-03   0.65415E+09 0.64677E+03 
c  TempC        0.25656E+04      48   0.25450E-01   0.12388E+06 0.32130E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7683          50.907           3.795          3.7808
v  Velocity[Y]             -6.899          8.1249     -4.8446e-05      0.00050625
v  Velocity[Z]            -25.035           17.72        -0.14755       -0.061979
v  ǁVelocityǁ           0.0071904          51.312          4.0187          3.8463
v  Pressure               -1338.1           223.6          203.83          210.79
v  k                   1.2653e-07          8.3338         0.06569        0.050196
v  omega                 0.004518       4.822e+05          4533.2          1429.4
v  TempC                  -111.15          604.08          27.816          26.993
v  Density                0.41186          2.6138          1.2202          1.2405
v  TurbVisc            6.3904e-13       0.0022901      6.3033e-05      9.4683e-05
v  CourantNb                    0          30.194         0.69643         0.49693
v  FourierNb            0.0024705           4.199        0.066451         0.08087
v  total_pressure           99987      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41831          2.6138          1.1435          1.1996


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018925          30.283         0.76288          0.5778


 TIME FOR THE TIME STEP              140:        0.61527E+02

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


 INSTANT    0.120300000E-01   TIME STEP NUMBER             141
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.745220270E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155851911E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58110E+02 0.66314E+01
   Friction velocity        uet   :  0.33841E-02 0.44998E+01
   Friction velocity        uk    :  0.17291E-01 0.16141E+01
   Dimensionless distance   yplus :  0.26092E+00 0.39597E+02
   Friction thermal sca.    tstar : -0.50189E+03 0.72663E+02
   Rough dim-less th. sca.  tplus :  0.19468E+00 0.12717E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148939
   Nb of faces within the viscous sub-layer     :       4309
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        163 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20198E+00      25   0.17549E-01   0.26408E+02 0.12403E+03 
c  Velocity[X]                                      0.23834E+02 
c  Velocity[Y]                                      0.62799E+00 
c  Velocity[Z]                                      0.19463E+01 
c  Pressure     0.10595E-03     120   0.58501E-02   0.17250E+00 0.13736E+02 
c  k            0.53197E-02      18   0.96472E-03   0.32932E+01 0.90006E+03 
c  omega        0.13078E+03      36   0.15095E-03   0.47889E+09 0.55328E+03 
c  TempC        0.25748E+04      47   0.26290E-01   0.12298E+06 0.31877E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8022          50.372          3.7966          3.7834
v  Velocity[Y]            -6.8126          8.0906     -3.1039e-05      0.00052062
v  Velocity[Z]            -24.759          17.627        -0.14876        -0.06245
v  ǁVelocityǁ            0.013394          50.823          4.0218          3.8494
v  Pressure               -1334.2          223.96          204.06          211.05
v  k                   8.0744e-08          8.2838        0.066007        0.050526
v  omega                0.0026954      3.8375e+05          4533.7          1428.1
v  TempC                  -102.16          618.84          28.014          27.219
v  Density                0.40261          2.1801          1.2197          1.2401
v  TurbVisc            5.1045e-13       0.0022898      6.3601e-05      9.5539e-05
v  CourantNb                    0           31.53         0.69693         0.49731
v  FourierNb            0.0024707           4.199        0.066953        0.081562
v  total_pressure           99991      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41829          2.1801          1.1431          1.1992


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020813          31.622         0.76389         0.57887


 TIME FOR THE TIME STEP              141:        0.61576E+02

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


 INSTANT    0.121300000E-01   TIME STEP NUMBER             142
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.201658727E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155853555E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60988E+02 0.65997E+01
   Friction velocity        uet   :  0.63762E-02 0.44365E+01
   Friction velocity        uk    :  0.18159E-01 0.16068E+01
   Dimensionless distance   yplus :  0.19708E+00 0.39722E+02
   Friction thermal sca.    tstar : -0.39956E+03 0.67720E+02
   Rough dim-less th. sca.  tplus :  0.14705E+00 0.12725E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148816
   Nb of faces within the viscous sub-layer     :       4370
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        164 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20202E+00      25   0.17385E-01   0.26563E+02 0.12425E+03 
c  Velocity[X]                                      0.23927E+02 
c  Velocity[Y]                                      0.61990E+00 
c  Velocity[Z]                                      0.20153E+01 
c  Pressure     0.10707E-03     122   0.59985E-02   0.17438E+00 0.81226E+01 
c  k            0.53456E-02      18   0.96753E-03   0.33054E+01 0.89889E+03 
c  omega        0.13106E+03      34   0.32299E-03   0.66949E+10 0.20265E+04 
c  TempC        0.25839E+04      47   0.26405E-01   0.12403E+06 0.31878E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8215          50.833          3.7982           3.786
v  Velocity[Y]            -6.8161          8.3489      1.1597e-05      0.00052971
v  Velocity[Z]            -25.026          17.712        -0.14998       -0.062928
v  ǁVelocityǁ            0.011489          51.242          4.0248          3.8525
v  Pressure               -1326.4          224.23           204.1          211.12
v  k                   1.2836e-07          8.3102        0.066307        0.050857
v  omega                0.0020595      3.7642e+06          4538.7          1427.1
v  TempC                  -102.32          633.01           28.21          27.445
v  Density                0.39595          2.0655          1.2193          1.2396
v  TurbVisc            4.2348e-13       0.0022898      6.4163e-05      9.6384e-05
v  CourantNb                    0          29.975         0.69743         0.49769
v  FourierNb             0.002471           4.199        0.067448        0.082246
v  total_pressure           99999      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41785           1.933          1.1427          1.1988


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.022188          30.063         0.76488         0.57994


 TIME FOR THE TIME STEP              142:        0.61638E+02

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


 INSTANT    0.122300000E-01   TIME STEP NUMBER             143
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.105502060E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855521E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59006E+02 0.66840E+01
   Friction velocity        uet   :  0.24765E-02 0.45001E+01
   Friction velocity        uk    :  0.12941E-01 0.16116E+01
   Dimensionless distance   yplus :  0.15732E+00 0.40793E+02
   Friction thermal sca.    tstar : -0.52514E+03 0.58093E+02
   Rough dim-less th. sca.  tplus :  0.11738E+00 0.12788E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148749
   Nb of faces within the viscous sub-layer     :       4404
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        167 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20206E+00      26   0.17491E-01   0.26792E+02 0.12464E+03 
c  Velocity[X]                                      0.24089E+02 
c  Velocity[Y]                                      0.65272E+00 
c  Velocity[Z]                                      0.20506E+01 
c  Pressure     0.10882E-03     118   0.59963E-02   0.17725E+00 0.59659E+01 
c  k            0.53759E-02      18   0.96505E-03   0.32849E+01 0.89315E+03 
c  omega        0.24008E+03      34   0.23515E-03   0.23784E+10 0.12220E+04 
c  TempC        0.25933E+04      47   0.25292E-01   0.12555E+06 0.31939E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8695          50.259          3.7998          3.7886
v  Velocity[Y]            -6.7273          7.9147       4.321e-05       0.0005425
v  Velocity[Z]            -24.459          17.791        -0.15123       -0.063415
v  ǁVelocityǁ           0.0074001          50.681          4.0278          3.8555
v  Pressure               -1322.5          224.39          204.12          211.14
v  k                    6.577e-08          8.4231         0.06659        0.051189
v  omega                0.0021518      1.9063e+06          4540.7          1425.9
v  TempC                  -108.39           596.1          28.402           27.67
v  Density                0.38976          2.0674          1.2189          1.2392
v  TurbVisc            5.1501e-13       0.0022897      6.4723e-05      9.7224e-05
v  CourantNb                    0          31.586         0.69793         0.49807
v  FourierNb            0.0024712           4.199        0.067944        0.082928
v  total_pressure           1e+05      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41906           2.003          1.1423          1.1984


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018841          31.677         0.76587           0.581


 TIME FOR THE TIME STEP              143:        0.61545E+02

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


 INSTANT    0.123300000E-01   TIME STEP NUMBER             144
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.601391842E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856785E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61923E+02 0.68439E+01
   Friction velocity        uet   :  0.30628E-02 0.45327E+01
   Friction velocity        uk    :  0.18498E-01 0.16180E+01
   Dimensionless distance   yplus :  0.20074E+00 0.40587E+02
   Friction thermal sca.    tstar : -0.32035E+03 0.51290E+02
   Rough dim-less th. sca.  tplus :  0.14977E+00 0.12776E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148599
   Nb of faces within the viscous sub-layer     :       4455
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        166 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20211E+00      26   0.17486E-01   0.27079E+02 0.12516E+03 
c  Velocity[X]                                      0.24430E+02 
c  Velocity[Y]                                      0.66058E+00 
c  Velocity[Z]                                      0.19883E+01 
c  Pressure     0.10851E-03     122   0.59402E-02   0.17651E+00 0.77560E+01 
c  k            0.54080E-02      18   0.96105E-03   0.32709E+01 0.88841E+03 
c  omega        0.14206E+03      35   0.22294E-03   0.14457E+10 0.95411E+03 
c  TempC        0.26029E+04      48   0.25229E-01   0.12378E+06 0.31581E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9147          50.666          3.8013          3.7912
v  Velocity[Y]            -6.5916          8.4085      7.4492e-05      0.00055681
v  Velocity[Z]             -24.84          17.799        -0.15244       -0.063893
v  ǁVelocityǁ           0.0035328          51.055          4.0307          3.8586
v  Pressure               -1314.5          224.33             204          211.05
v  k                   1.4454e-07          8.3659        0.066863        0.051521
v  omega                0.0030987      9.7687e+05          4543.2          1424.8
v  TempC                  -124.71          598.88          28.593          27.896
v  Density                0.40631          2.1437          1.2185          1.2388
v  TurbVisc            2.6327e-13       0.0022901      6.5287e-05       9.806e-05
v  CourantNb                    0           29.91         0.69841         0.49845
v  FourierNb            0.0024715           4.199         0.06844        0.083609
v  total_pressure      1.0001e+05      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41403           2.044           1.142           1.198


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020655          29.998         0.76685         0.58206


 TIME FOR THE TIME STEP              144:        0.62170E+02

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


 INSTANT    0.124300000E-01   TIME STEP NUMBER             145
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.692732149E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155859019E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59329E+02 0.67160E+01
   Friction velocity        uet   :  0.35530E-02 0.44372E+01
   Friction velocity        uk    :  0.10941E-01 0.16186E+01
   Dimensionless distance   yplus :  0.18812E+00 0.40539E+02
   Friction thermal sca.    tstar : -0.27964E+03 0.44115E+02
   Rough dim-less th. sca.  tplus :  0.14036E+00 0.12773E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148554
   Nb of faces within the viscous sub-layer     :       4467
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        163 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20215E+00      26   0.17698E-01   0.26690E+02 0.12411E+03 
c  Velocity[X]                                      0.24058E+02 
c  Velocity[Y]                                      0.64792E+00 
c  Velocity[Z]                                      0.19841E+01 
c  Pressure     0.10899E-03     133   0.59883E-02   0.17707E+00 0.18573E+02 
c  k            0.54430E-02      19   0.96099E-03   0.32943E+01 0.88902E+03 
c  omega        0.13269E+03      36   0.16992E-03   0.61652E+09 0.62404E+03 
c  TempC        0.26126E+04      48   0.25451E-01   0.12219E+06 0.31249E+03 
-----------------------------------------------------------------------------
  
  

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

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9432           50.08          3.8028          3.7939
v  Velocity[Y]            -6.5577          8.1825      7.2499e-05      0.00056479
v  Velocity[Z]            -24.614          17.849        -0.15365       -0.064366
v  ǁVelocityǁ           0.0033794          50.542          4.0336          3.8617
v  Pressure               -1310.3          223.94          203.59           210.7
v  k                   2.6408e-08          8.4603        0.067123        0.051849
v  omega                0.0054338      5.9612e+05          4542.9          1423.5
v  TempC                  -109.37          601.82          28.781          28.122
v  Density                0.40501          2.3792          1.2181          1.2384
v  TurbVisc            7.5405e-13       0.0022904       6.587e-05      9.8918e-05
v  CourantNb                    0          31.343         0.69887         0.49883
v  FourierNb            0.0024718           4.199        0.068948        0.084306
v  total_pressure      1.0001e+05      1.0155e+05      1.0153e+05      1.0154e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40811          2.1006          1.1416          1.1975


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018983          31.434         0.76782         0.58313


 TIME FOR THE TIME STEP              145:        0.62479E+02

===============================================================


 INSTANT    0.125300000E-01   TIME STEP NUMBER             146
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.355140429E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155863439E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62105E+02 0.68414E+01
   Friction velocity        uet   :  0.14943E-02 0.45216E+01
   Friction velocity        uk    :  0.14895E-01 0.16220E+01
   Dimensionless distance   yplus :  0.18580E+00 0.41442E+02
   Friction thermal sca.    tstar : -0.29704E+03 0.40444E+02
   Rough dim-less th. sca.  tplus :  0.13862E+00 0.12825E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148443
   Nb of faces within the viscous sub-layer     :       4504
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        160 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20219E+00      27   0.17168E-01   0.26495E+02 0.12352E+03 
c  Velocity[X]                                      0.23796E+02 
c  Velocity[Y]                                      0.65877E+00 
c  Velocity[Z]                                      0.20404E+01 
c  Pressure     0.10911E-03     153   0.60511E-02   0.17717E+00 0.38904E+02 
c  k            0.54791E-02      18   0.95724E-03   0.33298E+01 0.89134E+03 
c  omega        0.28002E+04      28   0.19675E-02   0.10244E+16 0.99992E+04 
c  TempC        0.26225E+04      47   0.25383E-01   0.12213E+06 0.31113E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9692          50.471          3.8042          3.7965
v  Velocity[Y]            -6.8539          8.0837      0.00010283      0.00057945
v  Velocity[Z]            -24.951          17.808        -0.15486       -0.064844
v  ǁVelocityǁ           0.0089302          50.874          4.0365          3.8647
v  Pressure               -1302.6          223.26          202.75          209.89
v  k                   4.7848e-08          8.6059        0.067376        0.052174
v  omega                 0.013166      1.7159e+09          5644.1          1494.5
v  TempC                  -113.77          611.34          28.968          28.348
v  Density                0.40365          2.1564          1.2177          1.2379
v  TurbVisc            6.6444e-13       0.0022903      6.6462e-05      9.9778e-05
v  CourantNb                    0          29.755         0.69934         0.49921
v  FourierNb             0.002472           4.199        0.069463        0.085009
v  total_pressure      1.0002e+05      1.0155e+05      1.0153e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41719          2.1564          1.1412          1.1971


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014375          29.842          0.7688         0.58422


 TIME FOR THE TIME STEP              146:        0.63436E+02

===============================================================


 INSTANT    0.126300000E-01   TIME STEP NUMBER             147
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.190141031E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866770E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59911E+02 0.68878E+01
   Friction velocity        uet   :  0.47399E-02 0.45091E+01
   Friction velocity        uk    :  0.16704E-01 0.16377E+01
   Dimensionless distance   yplus :  0.26532E+00 0.40950E+02
   Friction thermal sca.    tstar : -0.28715E+03 0.37711E+02
   Rough dim-less th. sca.  tplus :  0.19796E+00 0.12797E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148432
   Nb of faces within the viscous sub-layer     :       4529
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        165 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20224E+00      27   0.17235E-01   0.26424E+02 0.12321E+03 
c  Velocity[X]                                      0.23729E+02 
c  Velocity[Y]                                      0.66114E+00 
c  Velocity[Z]                                      0.20338E+01 
c  Pressure     0.10852E-03     149   0.59671E-02   0.17597E+00 0.45566E+02 
c  k            0.55158E-02      18   0.94194E-03   0.33433E+01 0.89061E+03 
c  omega        0.30486E+08       5   0.83530E-07   0.25609E+15 0.99961E+04 
c  TempC        0.26325E+04      47   0.25410E-01   0.12271E+06 0.31061E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0036           49.97          3.8057          3.7991
v  Velocity[Y]             -6.746          7.5558       0.0001024      0.00058882
v  Velocity[Z]            -24.583          18.015        -0.15606       -0.065323
v  ǁVelocityǁ            0.016941          50.431          4.0393          3.8678
v  Pressure                 -1298          222.01          201.84          208.95
v  k                    4.863e-08          8.5755        0.067623          0.0525
v  omega                   0.0256      8.5795e+08          5097.3          1457.4
v  TempC                  -117.73          608.59          29.151          28.573
v  Density                 0.3993          2.2159          1.2173          1.2375
v  TurbVisc            2.4878e-13       0.0022902      6.7055e-05      0.00010064
v  CourantNb                    0          31.347          0.6998         0.49959
v  FourierNb            0.0024723           4.199        0.069976        0.085711
v  total_pressure      1.0003e+05      1.0155e+05      1.0153e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41217          2.2159          1.1409          1.1968


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011397          31.437         0.76977          0.5853


 TIME FOR THE TIME STEP              147:        0.61437E+02

===============================================================


 INSTANT    0.127300000E-01   TIME STEP NUMBER             148
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.126689595E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867772E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62855E+02 0.68500E+01
   Friction velocity        uet   :  0.35013E-02 0.44526E+01
   Friction velocity        uk    :  0.24009E-01 0.16298E+01
   Dimensionless distance   yplus :  0.27456E+00 0.41718E+02
   Friction thermal sca.    tstar : -0.30763E+03 0.37050E+02
   Rough dim-less th. sca.  tplus :  0.20485E+00 0.12841E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148305
   Nb of faces within the viscous sub-layer     :       4567
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        163 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20229E+00      26   0.17774E-01   0.26435E+02 0.12310E+03 
c  Velocity[X]                                      0.23803E+02 
c  Velocity[Y]                                      0.64153E+00 
c  Velocity[Z]                                      0.19904E+01 
c  Pressure     0.10744E-03     155   0.59686E-02   0.17381E+00 0.51372E+02 
c  k            0.55490E-02      18   0.92962E-03   0.33415E+01 0.88783E+03 
c  omega        0.76417E+07       8   0.16627E-06   0.64023E+14 0.99859E+04 
c  TempC        0.26427E+04      47   0.25494E-01   0.12279E+06 0.30947E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0268          50.374           3.807          3.8017
v  Velocity[Y]            -6.7188          7.5766      0.00012006      0.00059121
v  Velocity[Z]             -24.83          17.816        -0.15728       -0.065804
v  ǁVelocityǁ            0.016307          50.787           4.042          3.8708
v  Pressure                 -1290          220.93          200.78          207.89
v  k                   2.6035e-08          8.6492        0.067869        0.052824
v  omega                 0.062139        4.29e+08          4823.9          1438.3
v  TempC                  -121.33          612.61          29.334          28.799
v  Density                0.40055          2.2724          1.2169          1.2371
v  TurbVisc            2.9452e-15       0.0022899      6.7636e-05      0.00010147
v  CourantNb                    0          29.716         0.70023         0.49996
v  FourierNb            0.0024725           4.199         0.07048        0.086394
v  total_pressure      1.0003e+05      1.0155e+05      1.0153e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40708          2.2724          1.1405          1.1964


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015622          29.803         0.77071         0.58636


 TIME FOR THE TIME STEP              148:        0.62036E+02

===============================================================


 INSTANT    0.128300000E-01   TIME STEP NUMBER             149
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.136364840E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869090E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60316E+02 0.68754E+01
   Friction velocity        uet   :  0.44071E-02 0.45367E+01
   Friction velocity        uk    :  0.17856E-01 0.16397E+01
   Dimensionless distance   yplus :  0.19130E+00 0.41472E+02
   Friction thermal sca.    tstar : -0.33652E+03 0.35750E+02
   Rough dim-less th. sca.  tplus :  0.14273E+00 0.12827E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148198
   Nb of faces within the viscous sub-layer     :       4616
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        155 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20233E+00      26   0.18376E-01   0.26784E+02 0.12377E+03 
c  Velocity[X]                                      0.24057E+02 
c  Velocity[Y]                                      0.65529E+00 
c  Velocity[Z]                                      0.20720E+01 
c  Pressure     0.11002E-03     157   0.60836E-02   0.17793E+00 0.55891E+02 
c  k            0.55769E-02      18   0.93134E-03   0.33379E+01 0.88479E+03 
c  omega        0.19173E+07      11   0.33134E-06   0.16006E+14 0.99473E+04 
c  TempC        0.26530E+04      47   0.25537E-01   0.12311E+06 0.30863E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0454          49.667          3.8084          3.8043
v  Velocity[Y]            -6.6395          7.6208       0.0001273      0.00060058
v  Velocity[Z]            -24.601          17.907         -0.1585       -0.066283
v  ǁVelocityǁ            0.012969          50.125          4.0447          3.8739
v  Pressure               -1286.1          219.81          199.64          206.73
v  k                   1.2603e-07           8.619        0.068124        0.053148
v  omega                  0.17144      2.1452e+08          4688.5          1428.2
v  TempC                  -124.87          592.37          29.513          29.025
v  Density                0.39873          2.3264          1.2165          1.2366
v  TurbVisc            9.5981e-16       0.0022902      6.8236e-05      0.00010232
v  CourantNb                    0          31.115         0.70066         0.50034
v  FourierNb            0.0024728           4.199        0.070999        0.087096
v  total_pressure      1.0004e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40815          2.3264          1.1401           1.196


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018321          31.205         0.77166         0.58743


 TIME FOR THE TIME STEP              149:        0.62447E+02

===============================================================


 INSTANT    0.129300000E-01   TIME STEP NUMBER             150
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.137834823E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869856E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62723E+02 0.69879E+01
   Friction velocity        uet   :  0.21465E-02 0.45695E+01
   Friction velocity        uk    :  0.15438E-01 0.16356E+01
   Dimensionless distance   yplus :  0.18776E+00 0.41343E+02
   Friction thermal sca.    tstar : -0.26838E+03 0.36659E+02
   Rough dim-less th. sca.  tplus :  0.14009E+00 0.12820E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148120
   Nb of faces within the viscous sub-layer     :       4684
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        147 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20237E+00      26   0.17536E-01   0.27059E+02 0.12426E+03 
c  Velocity[X]                                      0.24349E+02 
c  Velocity[Y]                                      0.66984E+00 
c  Velocity[Z]                                      0.20404E+01 
c  Pressure     0.10959E-03     133   0.62001E-02   0.17727E+00 0.39215E+02 
c  k            0.55960E-02      18   0.94016E-03   0.33416E+01 0.88271E+03 
c  omega        0.48120E+06      15   0.66143E-06   0.40020E+13 0.98001E+04 
c  TempC        0.26634E+04      47   0.25649E-01   0.12343E+06 0.30782E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0601          50.123          3.8096          3.8069
v  Velocity[Y]            -6.5207          8.1071      0.00014934      0.00060924
v  Velocity[Z]            -24.936          17.873         -0.1597       -0.066761
v  ǁVelocityǁ            0.015294          50.529          4.0474          3.8769
v  Pressure               -1277.9          219.04          198.88          205.94
v  k                   2.7942e-07          8.6122        0.068394        0.053474
v  omega                 0.015992      1.0728e+08          4622.6          1422.8
v  TempC                  -128.08           592.1          29.693          29.251
v  Density                0.40806          2.3819          1.2161          1.2362
v  TurbVisc            3.4457e-15       0.0022904      6.8833e-05      0.00010317
v  CourantNb                    0          29.488         0.70108         0.50071
v  FourierNb            0.0024731           4.199        0.071517        0.087794
v  total_pressure      1.0005e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40806          2.3819          1.1398          1.1956


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017019          29.574          0.7726          0.5885


 TIME FOR THE TIME STEP              150:        0.62004E+02

===============================================================


 INSTANT    0.130300000E-01   TIME STEP NUMBER             151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.701146274E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866189E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60711E+02 0.68402E+01
   Friction velocity        uet   :  0.13061E-02 0.44961E+01
   Friction velocity        uk    :  0.14026E-01 0.16364E+01
   Dimensionless distance   yplus :  0.15578E+00 0.42193E+02
   Friction thermal sca.    tstar : -0.51484E+03 0.60708E+02
   Rough dim-less th. sca.  tplus :  0.11623E+00 0.12868E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     148079
   Nb of faces within the viscous sub-layer     :       4720
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        150 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20241E+00      26   0.17971E-01   0.26762E+02 0.12344E+03 
c  Velocity[X]                                      0.24076E+02 
c  Velocity[Y]                                      0.67012E+00 
c  Velocity[Z]                                      0.20157E+01 
c  Pressure     0.10830E-03     134   0.59904E-02   0.17488E+00 0.28859E+02 
c  k            0.56044E-02      19   0.95098E-03   0.33561E+01 0.88204E+03 
c  omega        0.12093E+06      18   0.13196E-05   0.10010E+13 0.92749E+04 
c  TempC        0.26736E+04      48   0.25527E-01   0.12355E+06 0.30675E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0679          49.621          3.8109          3.8095
v  Velocity[Y]            -6.5336          7.9352      0.00016475      0.00061751
v  Velocity[Z]            -24.539          17.956        -0.16089       -0.067245
v  ǁVelocityǁ            0.013071          50.096            4.05          3.8799
v  Pressure               -1273.1          218.71          198.32          205.36
v  k                   1.3479e-08          8.6715        0.068682        0.053799
v  omega                 0.032602      5.3662e+07          4590.5          1419.6
v  TempC                  -130.09          608.87          29.874          29.476
v  Density                0.40819          2.4345          1.2157          1.2358
v  TurbVisc            1.5232e-14       0.0022902      6.9435e-05      0.00010403
v  CourantNb                    0          31.112          0.7015         0.50108
v  FourierNb            0.0024733           4.199        0.072045        0.088503
v  total_pressure      1.0005e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41286          2.4345          1.1395          1.1952


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018304          31.202         0.77354         0.58958


 TIME FOR THE TIME STEP              151:        0.61714E+02

===============================================================


 INSTANT    0.131300000E-01   TIME STEP NUMBER             152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.109303839E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155865103E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63645E+02 0.70344E+01
   Friction velocity        uet   :  0.27036E-02 0.45856E+01
   Friction velocity        uk    :  0.21911E-01 0.16387E+01
   Dimensionless distance   yplus :  0.27261E+00 0.41381E+02
   Friction thermal sca.    tstar : -0.27233E+03 0.89640E+02
   Rough dim-less th. sca.  tplus :  0.20340E+00 0.12822E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147967
   Nb of faces within the viscous sub-layer     :       4771
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        161 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20245E+00      27   0.17591E-01   0.27021E+02 0.12389E+03 
c  Velocity[X]                                      0.24323E+02 
c  Velocity[Y]                                      0.67063E+00 
c  Velocity[Z]                                      0.20275E+01 
c  Pressure     0.10853E-03     129   0.59936E-02   0.17520E+00 0.20886E+02 
c  k            0.56027E-02      19   0.96982E-03   0.33701E+01 0.88135E+03 
c  omega        0.30431E+05      22   0.26874E-05   0.25057E+12 0.77965E+04 
c  TempC        0.26837E+04      49   0.25275E-01   0.12346E+06 0.30545E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0571          49.854          3.8122          3.8121
v  Velocity[Y]            -6.7778           7.967      0.00018571      0.00062549
v  Velocity[Z]            -24.789          18.048        -0.16209       -0.067729
v  ǁVelocityǁ           0.0078842          50.258          4.0527           3.883
v  Pressure               -1265.4          218.21          197.89          204.96
v  k                   1.0908e-07          8.7745        0.068988        0.054121
v  omega                 0.038527      2.6853e+07          4575.6          1417.5
v  TempC                  -133.04          615.55          30.057          29.702
v  Density                0.40042          2.4688          1.2153          1.2354
v  TurbVisc            7.1926e-14       0.0022901      7.0035e-05      0.00010489
v  CourantNb                    0          29.469         0.70193         0.50145
v  FourierNb            0.0024736           4.199        0.072575        0.089218
v  total_pressure      1.0006e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41569          2.4688          1.1391          1.1948


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013996          29.555          0.7745         0.59066


 TIME FOR THE TIME STEP              152:        0.62074E+02

===============================================================


 INSTANT    0.132300000E-01   TIME STEP NUMBER             153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.228144800E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155862527E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60740E+02 0.70354E+01
   Friction velocity        uet   :  0.14465E-02 0.45471E+01
   Friction velocity        uk    :  0.20000E-01 0.16518E+01
   Dimensionless distance   yplus :  0.23171E+00 0.41347E+02
   Friction thermal sca.    tstar : -0.30450E+03 0.73536E+02
   Rough dim-less th. sca.  tplus :  0.17288E+00 0.12820E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147932
   Nb of faces within the viscous sub-layer     :       4806
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        166 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20250E+00      27   0.18012E-01   0.26801E+02 0.12325E+03 
c  Velocity[X]                                      0.24097E+02 
c  Velocity[Y]                                      0.67089E+00 
c  Velocity[Z]                                      0.20333E+01 
c  Pressure     0.10886E-03     132   0.60242E-02   0.17592E+00 0.19558E+02 
c  k            0.55942E-02      19   0.97274E-03   0.33720E+01 0.87920E+03 
c  omega        0.76747E+04      26   0.66844E-05   0.63987E+11 0.53281E+04 
c  TempC        0.26935E+04      47   0.25838E-01   0.12271E+06 0.30333E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0592          49.228          3.8136          3.8147
v  Velocity[Y]            -6.6914          7.5928      0.00021138      0.00063599
v  Velocity[Z]            -24.583          18.008        -0.16329       -0.068212
v  ǁVelocityǁ            0.010297          49.683          4.0554           3.886
v  Pressure               -1261.1          217.83          197.47          204.59
v  k                   1.0781e-07          8.7634        0.069307        0.054441
v  omega                 0.079483      1.3448e+07          4570.4            1416
v  TempC                  -135.74          587.87          30.242          29.928
v  Density                0.39741          2.5208          1.2149          1.2349
v  TurbVisc            3.4491e-13       0.0022898       7.063e-05      0.00010575
v  CourantNb                    0          30.787         0.70235         0.50182
v  FourierNb            0.0024738           4.199        0.073099        0.089931
v  total_pressure      1.0006e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40238          2.5208          1.1387          1.1944


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0092195          30.877         0.77545         0.59175


 TIME FOR THE TIME STEP              153:        0.62048E+02

===============================================================


 INSTANT    0.133300000E-01   TIME STEP NUMBER             154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.771047242E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155863537E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63436E+02 0.70069E+01
   Friction velocity        uet   :  0.44086E-02 0.44617E+01
   Friction velocity        uk    :  0.18871E-01 0.16471E+01
   Dimensionless distance   yplus :  0.25273E+00 0.41408E+02
   Friction thermal sca.    tstar : -0.41531E+03 0.60639E+02
   Rough dim-less th. sca.  tplus :  0.18857E+00 0.12824E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147821
   Nb of faces within the viscous sub-layer     :       4828
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        168 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20255E+00      26   0.18554E-01   0.26624E+02 0.12270E+03 
c  Velocity[X]                                      0.23954E+02 
c  Velocity[Y]                                      0.65901E+00 
c  Velocity[Z]                                      0.20110E+01 
c  Pressure     0.11003E-03     152   0.60725E-02   0.17749E+00 0.28887E+02 
c  k            0.55827E-02      19   0.96641E-03   0.33776E+01 0.87763E+03 
c  omega        0.19483E+04      28   0.16203E-04   0.16827E+11 0.30718E+04 
c  TempC        0.27029E+04      48   0.25147E-01   0.12407E+06 0.30383E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0517          49.707          3.8149          3.8173
v  Velocity[Y]            -6.6094          7.5831      0.00025483      0.00064993
v  Velocity[Z]            -24.712          18.003         -0.1645         -0.0687
v  ǁVelocityǁ           0.0095754          50.114          4.0582          3.8891
v  Pressure               -1252.9          217.33          196.84          204.03
v  k                   4.3938e-07          8.8853        0.069635        0.054758
v  omega                  0.34626       6.745e+06            4569          1414.9
v  TempC                  -138.15          590.63           30.43          30.154
v  Density                0.41019          2.5702          1.2144          1.2345
v  TurbVisc            6.6314e-13       0.0022897      7.1223e-05      0.00010662
v  CourantNb                    0          29.225         0.70278         0.50219
v  FourierNb            0.0024741           4.199        0.073624        0.090643
v  total_pressure      1.0007e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41616          2.5702          1.1384           1.194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011342          29.311         0.77641         0.59283


 TIME FOR THE TIME STEP              154:        0.63647E+02

===============================================================


 INSTANT    0.134300000E-01   TIME STEP NUMBER             155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.971854548E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155864522E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61641E+02 0.70527E+01
   Friction velocity        uet   :  0.27399E-02 0.45822E+01
   Friction velocity        uk    :  0.18964E-01 0.16600E+01
   Dimensionless distance   yplus :  0.26825E+00 0.42517E+02
   Friction thermal sca.    tstar : -0.41150E+03 0.49714E+02
   Rough dim-less th. sca.  tplus :  0.20015E+00 0.12886E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147739
   Nb of faces within the viscous sub-layer     :       4848
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        172 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20259E+00      27   0.17609E-01   0.27140E+02 0.12374E+03 
c  Velocity[X]                                      0.24412E+02 
c  Velocity[Y]                                      0.65799E+00 
c  Velocity[Z]                                      0.20702E+01 
c  Pressure     0.11033E-03     154   0.59966E-02   0.17780E+00 0.38894E+02 
c  k            0.55734E-02      19   0.94308E-03   0.33804E+01 0.87573E+03 
c  omega        0.51429E+03      32   0.96342E-04   0.55777E+10 0.18267E+04 
c  TempC        0.27119E+04      48   0.24877E-01   0.12378E+06 0.30233E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0426          49.183          3.8164          3.8199
v  Velocity[Y]            -6.5336          7.6062      0.00027481      0.00066256
v  Velocity[Z]            -24.425          17.907         -0.1657       -0.069186
v  ǁVelocityǁ            0.010741          49.625          4.0609          3.8922
v  Pressure               -1248.3           216.5          196.01          203.26
v  k                   2.1249e-07          8.8598        0.069963        0.055076
v  omega                  0.39747      3.3935e+06            4569          1413.8
v  TempC                  -139.28          608.02           30.62           30.38
v  Density                0.40888          2.6162           1.214          1.2341
v  TurbVisc            1.9495e-12       0.0022897      7.1798e-05      0.00010747
v  CourantNb                    0          30.871         0.70321         0.50256
v  FourierNb            0.0024743           4.199        0.074132        0.091339
v  total_pressure      1.0008e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40888          2.6162           1.138          1.1936


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015293           30.96         0.77734          0.5939


 TIME FOR THE TIME STEP              155:        0.63743E+02

===============================================================


 INSTANT    0.135300000E-01   TIME STEP NUMBER             156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.238841847E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867916E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64510E+02 0.71920E+01
   Friction velocity        uet   :  0.44219E-02 0.45860E+01
   Friction velocity        uk    :  0.20203E-01 0.16556E+01
   Dimensionless distance   yplus :  0.21582E+00 0.42073E+02
   Friction thermal sca.    tstar : -0.38458E+03 0.42354E+02
   Rough dim-less th. sca.  tplus :  0.16103E+00 0.12861E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147780
   Nb of faces within the viscous sub-layer     :       4894
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        171 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20264E+00      26   0.18481E-01   0.26769E+02 0.12275E+03 
c  Velocity[X]                                      0.24042E+02 
c  Velocity[Y]                                      0.66645E+00 
c  Velocity[Z]                                      0.20608E+01 
c  Pressure     0.11127E-03     175   0.61887E-02   0.17905E+00 0.68167E+02 
c  k            0.55706E-02      19   0.92847E-03   0.34073E+01 0.87705E+03 
c  omega        0.18777E+03      34   0.16139E-03   0.21247E+10 0.11382E+04 
c  TempC        0.27208E+04      49   0.24725E-01   0.12319E+06 0.30046E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.013          49.665          3.8178          3.8225
v  Velocity[Y]            -6.5499          8.0968      0.00031659      0.00067212
v  Velocity[Z]            -24.623          17.886        -0.16686       -0.069661
v  ǁVelocityǁ            0.013028          50.069          4.0637          3.8952
v  Pressure               -1239.6          215.05          194.62          201.88
v  k                   4.8089e-08          8.8449         0.07028        0.055391
v  omega                0.0068372      1.7174e+06          4570.1          1412.9
v  TempC                  -114.83          588.95          30.813          30.606
v  Density                0.40081          2.6383          1.2136          1.2337
v  TurbVisc            8.9737e-13       0.0022899      7.2378e-05      0.00010833
v  CourantNb                    0           29.24         0.70363         0.50294
v  FourierNb            0.0024746           4.199        0.074643        0.092043
v  total_pressure      1.0009e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40081          2.6383          1.1377          1.1933


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013145          29.325         0.77827         0.59498


 TIME FOR THE TIME STEP              156:        0.65044E+02

===============================================================


 INSTANT    0.136300000E-01   TIME STEP NUMBER             157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.136830071E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870569E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62223E+02 0.70346E+01
   Friction velocity        uet   :  0.37473E-02 0.45121E+01
   Friction velocity        uk    :  0.17169E-01 0.16564E+01
   Dimensionless distance   yplus :  0.26265E+00 0.41981E+02
   Friction thermal sca.    tstar : -0.40425E+03 0.58395E+02
   Rough dim-less th. sca.  tplus :  0.19596E+00 0.12856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147689
   Nb of faces within the viscous sub-layer     :       4926
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        168 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20269E+00      27   0.18769E-01   0.27168E+02 0.12353E+03 
c  Velocity[X]                                      0.24421E+02 
c  Velocity[Y]                                      0.67087E+00 
c  Velocity[Z]                                      0.20761E+01 
c  Pressure     0.11137E-03     177   0.59979E-02   0.17909E+00 0.79691E+02 
c  k            0.55764E-02      19   0.93816E-03   0.34234E+01 0.87702E+03 
c  omega        0.13797E+03      37   0.15755E-03   0.11668E+10 0.84515E+03 
c  TempC        0.27296E+04      48   0.24988E-01   0.12273E+06 0.29877E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0001          49.012          3.8192          3.8251
v  Velocity[Y]            -6.6318           8.055      0.00033872      0.00068319
v  Velocity[Z]            -24.416          17.806        -0.16803       -0.070136
v  ǁVelocityǁ           0.0058927          49.489          4.0664          3.8983
v  Pressure               -1234.8          213.53          193.04          200.29
v  k                    5.513e-07          8.8951         0.07058        0.055704
v  omega                  0.11005      9.9793e+05          4570.8            1412
v  TempC                  -114.35          611.58          31.005          30.832
v  Density                0.40968          2.2309          1.2132          1.2332
v  TurbVisc            2.4465e-13       0.0022898      7.2957e-05      0.00010918
v  CourantNb                    0          30.656         0.70404         0.50332
v  FourierNb            0.0024748          4.2003        0.075157        0.092745
v  total_pressure      1.0009e+05      1.0154e+05      1.0152e+05      1.0153e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41235          2.2309          1.1374          1.1929


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0088839          30.744          0.7792         0.59606


 TIME FOR THE TIME STEP              157:        0.65448E+02

===============================================================


 INSTANT    0.137300000E-01   TIME STEP NUMBER             158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.170893755E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872313E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64591E+02 0.72393E+01
   Friction velocity        uet   :  0.21543E-02 0.45869E+01
   Friction velocity        uk    :  0.12721E-01 0.16578E+01
   Dimensionless distance   yplus :  0.20518E+00 0.43062E+02
   Friction thermal sca.    tstar : -0.32324E+03 0.72903E+02
   Rough dim-less th. sca.  tplus :  0.15308E+00 0.12917E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147581
   Nb of faces within the viscous sub-layer     :       5004
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        166 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20273E+00      27   0.17956E-01   0.27071E+02 0.12317E+03 
c  Velocity[X]                                      0.24253E+02 
c  Velocity[Y]                                      0.68494E+00 
c  Velocity[Z]                                      0.21336E+01 
c  Pressure     0.11167E-03     177   0.60902E-02   0.17943E+00 0.85660E+02 
c  k            0.55901E-02      19   0.95807E-03   0.34348E+01 0.87636E+03 
c  omega        0.13432E+03      35   0.14609E-03   0.75636E+09 0.68051E+03 
c  TempC        0.27384E+04      48   0.25352E-01   0.12235E+06 0.29719E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9834          49.297          3.8207          3.8277
v  Velocity[Y]            -6.6737          7.8731      0.00036322      0.00068978
v  Velocity[Z]            -24.672          17.867        -0.16919       -0.070616
v  ǁVelocityǁ           0.0028007          49.702          4.0691          3.9013
v  Pressure               -1226.7           211.9          191.37          198.59
v  k                   9.6145e-09          8.9837        0.070859        0.056018
v  omega                   0.1275      5.1972e+05          4573.7          1411.2
v  TempC                  -116.24           597.8          31.196          31.057
v  Density                 0.3992          2.2241          1.2128          1.2328
v  TurbVisc             2.168e-12       0.0022901      7.3528e-05      0.00011003
v  CourantNb                    0          29.012         0.70444         0.50369
v  FourierNb            0.0024751          4.2181        0.075658        0.093436
v  total_pressure       1.001e+05      1.0154e+05      1.0152e+05      1.0152e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4063          1.9869           1.137          1.1925


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012532          29.097          0.7801         0.59712


 TIME FOR THE TIME STEP              158:        0.65552E+02

===============================================================


 INSTANT    0.138300000E-01   TIME STEP NUMBER             159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.517221399E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872890E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62187E+02 0.71897E+01
   Friction velocity        uet   :  0.63400E-04 0.45943E+01
   Friction velocity        uk    :  0.16187E-01 0.16695E+01
   Dimensionless distance   yplus :  0.15445E+00 0.42614E+02
   Friction thermal sca.    tstar : -0.28640E+03 0.51935E+02
   Rough dim-less th. sca.  tplus :  0.11523E+00 0.12892E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147489
   Nb of faces within the viscous sub-layer     :       5054
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        153 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20278E+00      27   0.18175E-01   0.26896E+02 0.12263E+03 
c  Velocity[X]                                      0.24103E+02 
c  Velocity[Y]                                      0.68933E+00 
c  Velocity[Z]                                      0.21039E+01 
c  Pressure     0.11162E-03     175   0.60858E-02   0.17935E+00 0.78086E+02 
c  k            0.56103E-02      19   0.97042E-03   0.34377E+01 0.87448E+03 
c  omega        0.13335E+03      35   0.13247E-03   0.80734E+09 0.70197E+03 
c  TempC        0.27472E+04      48   0.24592E-01   0.12374E+06 0.29778E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.954          48.823          3.8221          3.8303
v  Velocity[Y]            -6.7759          8.0666      0.00038991       0.0006974
v  Velocity[Z]            -24.319          17.922        -0.17034       -0.071096
v  ǁVelocityǁ           0.0076348          49.277          4.0718          3.9044
v  Pressure               -1221.5           210.5          189.86          197.05
v  k                   5.5123e-07          9.0092        0.071121        0.056333
v  omega                  0.18091      9.1606e+05          4575.4          1410.4
v  TempC                  -118.94          607.08          31.384          31.282
v  Density                0.40551          2.2509          1.2124          1.2324
v  TurbVisc            4.4968e-14       0.0022904      7.4093e-05      0.00011087
v  CourantNb                    0          30.558         0.70484         0.50406
v  FourierNb            0.0024753          4.3192        0.076151        0.094117
v  total_pressure       1.001e+05      1.0154e+05      1.0151e+05      1.0152e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41067          2.1395          1.1367          1.1921


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0084694          30.646         0.78099         0.59817


 TIME FOR THE TIME STEP              159:        0.65526E+02

===============================================================


 INSTANT    0.139300000E-01   TIME STEP NUMBER             160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.239596951E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871338E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65392E+02 0.71760E+01
   Friction velocity        uet   :  0.96375E-03 0.45600E+01
   Friction velocity        uk    :  0.17972E-01 0.16676E+01
   Dimensionless distance   yplus :  0.19213E+00 0.43654E+02
   Friction thermal sca.    tstar : -0.42274E+03 0.39742E+02
   Rough dim-less th. sca.  tplus :  0.14335E+00 0.12949E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147391
   Nb of faces within the viscous sub-layer     :       5114
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        144 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20282E+00      26   0.18804E-01   0.26814E+02 0.12231E+03 
c  Velocity[X]                                      0.24057E+02 
c  Velocity[Y]                                      0.66942E+00 
c  Velocity[Z]                                      0.20875E+01 
c  Pressure     0.11048E-03     174   0.61214E-02   0.17723E+00 0.72969E+02 
c  k            0.56326E-02      19   0.96734E-03   0.34275E+01 0.87081E+03 
c  omega        0.13403E+03      35   0.16526E-03   0.63943E+09 0.62425E+03 
c  TempC        0.27563E+04      48   0.24469E-01   0.12390E+06 0.29689E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9236          49.216          3.8234          3.8329
v  Velocity[Y]            -6.6197          7.9252      0.00041455      0.00070369
v  Velocity[Z]            -24.512          17.982        -0.17151       -0.071576
v  ǁVelocityǁ            0.010984          49.628          4.0743          3.9074
v  Pressure               -1212.7          209.01          188.42          195.63
v  k                   9.6201e-08          9.0557        0.071372        0.056652
v  omega                  0.32682      5.0589e+05          4577.9          1409.6
v  TempC                  -121.24          613.07          31.571          31.508
v  Density                0.40124          2.2903           1.212          1.2319
v  TurbVisc            2.1713e-12       0.0022903      7.4645e-05      0.00011169
v  CourantNb           6.7009e-09          28.964         0.70523         0.50442
v  FourierNb            0.0024756          4.3989         0.07663        0.094783
v  total_pressure      1.0011e+05      1.0153e+05      1.0151e+05      1.0152e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41615          2.0868          1.1364          1.1917


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0089265          29.049         0.78186          0.5992


 TIME FOR THE TIME STEP              160:        0.65574E+02

===============================================================


 INSTANT    0.140300000E-01   TIME STEP NUMBER             161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.168027514E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870702E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62934E+02 0.72159E+01
   Friction velocity        uet   :  0.84893E-03 0.45932E+01
   Friction velocity        uk    :  0.21093E-01 0.16740E+01
   Dimensionless distance   yplus :  0.26986E+00 0.43070E+02
   Friction thermal sca.    tstar : -0.38266E+03 0.42092E+02
   Rough dim-less th. sca.  tplus :  0.20134E+00 0.12917E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147336
   Nb of faces within the viscous sub-layer     :       5171
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        146 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20286E+00      26   0.18529E-01   0.27378E+02 0.12346E+03 
c  Velocity[X]                                      0.24546E+02 
c  Velocity[Y]                                      0.68014E+00 
c  Velocity[Z]                                      0.21517E+01 
c  Pressure     0.11034E-03     169   0.60566E-02   0.17674E+00 0.62983E+02 
c  k            0.56556E-02      19   0.96303E-03   0.34307E+01 0.86894E+03 
c  omega        0.13363E+03      37   0.14798E-03   0.48612E+09 0.54389E+03 
c  TempC        0.27656E+04      48   0.24235E-01   0.12310E+06 0.29485E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9023          48.387          3.8248          3.8355
v  Velocity[Y]            -6.6608          7.9964      0.00040488      0.00071039
v  Velocity[Z]             -24.16          18.047        -0.17264       -0.072049
v  ǁVelocityǁ            0.010079          48.854          4.0769          3.9104
v  Pressure               -1208.3          207.66          187.19          194.41
v  k                   3.8021e-07          9.1062        0.071614        0.056968
v  omega                  0.37284      3.5188e+05          4579.8          1408.9
v  TempC                  -123.73          605.22          31.755          31.734
v  Density                0.39853           2.325          1.2116          1.2315
v  TurbVisc            3.8339e-13       0.0022901      7.5211e-05      0.00011253
v  CourantNb                    0          30.305         0.70561         0.50479
v  FourierNb            0.0024758          4.4613        0.077124        0.095468
v  total_pressure      1.0012e+05      1.0153e+05      1.0151e+05      1.0152e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41837          2.1704          1.1361          1.1913


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013126          30.393         0.78273         0.60025


 TIME FOR THE TIME STEP              161:        0.64803E+02

===============================================================


 INSTANT    0.141300000E-01   TIME STEP NUMBER             162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.221802325E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868886E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64865E+02 0.73065E+01
   Friction velocity        uet   :  0.39461E-02 0.45946E+01
   Friction velocity        uk    :  0.15129E-01 0.16759E+01
   Dimensionless distance   yplus :  0.16736E+00 0.42957E+02
   Friction thermal sca.    tstar : -0.39570E+03 0.47132E+02
   Rough dim-less th. sca.  tplus :  0.12487E+00 0.12911E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147308
   Nb of faces within the viscous sub-layer     :       5231
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        156 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20291E+00      26   0.17925E-01   0.27018E+02 0.12251E+03 
c  Velocity[X]                                      0.24251E+02 
c  Velocity[Y]                                      0.67298E+00 
c  Velocity[Z]                                      0.20933E+01 
c  Pressure     0.11165E-03     170   0.61422E-02   0.17859E+00 0.64456E+02 
c  k            0.56775E-02      19   0.95045E-03   0.34376E+01 0.86772E+03 
c  omega        0.13371E+03      35   0.19875E-03   0.70467E+09 0.65345E+03 
c  TempC        0.27749E+04      48   0.24691E-01   0.12131E+06 0.29163E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8734          48.677          3.8261          3.8381
v  Velocity[Y]            -6.5865          7.3944      0.00043185      0.00071851
v  Velocity[Z]            -24.469          18.109        -0.17379       -0.072524
v  ǁVelocityǁ            0.010435          49.076          4.0795          3.9134
v  Pressure               -1200.1          206.51          185.92          193.17
v  k                   7.8922e-07          9.0045        0.071848        0.057281
v  omega                 0.087165      1.1559e+06          4583.1          1408.2
v  TempC                  -123.87          598.58          31.939           31.96
v  Density                0.40209          2.3636          1.2112          1.2311
v  TurbVisc            1.5176e-12       0.0022897      7.5791e-05      0.00011339
v  CourantNb                    0            28.6         0.70597         0.50515
v  FourierNb            0.0024761          4.5099        0.077625        0.096166
v  total_pressure      1.0012e+05      1.0153e+05      1.0151e+05      1.0152e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41939          2.1934          1.1357           1.191


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0093288          28.685          0.7836         0.60131


 TIME FOR THE TIME STEP              162:        0.64745E+02

===============================================================


 INSTANT    0.142300000E-01   TIME STEP NUMBER             163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.273506494E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869196E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62865E+02 0.71640E+01
   Friction velocity        uet   :  0.42609E-02 0.45430E+01
   Friction velocity        uk    :  0.14395E-01 0.16715E+01
   Dimensionless distance   yplus :  0.14175E+00 0.42854E+02
   Friction thermal sca.    tstar : -0.32136E+03 0.49864E+02
   Rough dim-less th. sca.  tplus :  0.10576E+00 0.12905E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147174
   Nb of faces within the viscous sub-layer     :       5274
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        149 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20295E+00      27   0.18420E-01   0.26628E+02 0.12148E+03 
c  Velocity[X]                                      0.23844E+02 
c  Velocity[Y]                                      0.67470E+00 
c  Velocity[Z]                                      0.21094E+01 
c  Pressure     0.11239E-03     175   0.60994E-02   0.17990E+00 0.69393E+02 
c  k            0.56991E-02      19   0.92783E-03   0.34431E+01 0.86635E+03 
c  omega        0.13423E+03      35   0.15959E-03   0.48074E+09 0.53951E+03 
c  TempC        0.27842E+04      49   0.24283E-01   0.12269E+06 0.29223E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8546           48.38          3.8275          3.8407
v  Velocity[Y]            -6.5671           7.395      0.00045149      0.00072708
v  Velocity[Z]            -24.131          18.047        -0.17491       -0.073002
v  ǁVelocityǁ           0.0096252          48.839           4.082          3.9165
v  Pressure               -1194.3          204.98          184.54          191.85
v  k                   6.0088e-07          9.1422        0.072084        0.057593
v  omega                  0.11563      7.2957e+05          4584.7          1407.4
v  TempC                  -119.75          593.92           32.12          32.185
v  Density                0.40515          2.3658          1.2108          1.2307
v  TurbVisc            3.1051e-12       0.0022897       7.636e-05      0.00011423
v  CourantNb                    0          30.194         0.70635         0.50552
v  FourierNb            0.0024763          4.5475        0.078113         0.09685
v  total_pressure      1.0013e+05      1.0153e+05      1.0151e+05      1.0152e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41203          2.2467          1.1354          1.1906


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0058222          30.282         0.78447         0.60237


 TIME FOR THE TIME STEP              163:        0.65173E+02

===============================================================


 INSTANT    0.143300000E-01   TIME STEP NUMBER             164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.279386797E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871537E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66553E+02 0.73594E+01
   Friction velocity        uet   :  0.31872E-02 0.46128E+01
   Friction velocity        uk    :  0.97630E-02 0.16795E+01
   Dimensionless distance   yplus :  0.16714E+00 0.43489E+02
   Friction thermal sca.    tstar : -0.24476E+03 0.49856E+02
   Rough dim-less th. sca.  tplus :  0.12471E+00 0.12940E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147078
   Nb of faces within the viscous sub-layer     :       5341
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        126 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20300E+00      27   0.18281E-01   0.26944E+02 0.12207E+03 
c  Velocity[X]                                      0.24114E+02 
c  Velocity[Y]                                      0.68628E+00 
c  Velocity[Z]                                      0.21442E+01 
c  Pressure     0.11267E-03     193   0.61594E-02   0.18027E+00 0.96669E+02 
c  k            0.57179E-02      19   0.90761E-03   0.34418E+01 0.86416E+03 
c  omega        0.13405E+03      35   0.14406E-03   0.46027E+09 0.52730E+03 
c  TempC        0.27935E+04      49   0.24292E-01   0.12233E+06 0.29076E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8257          48.669          3.8288          3.8433
v  Velocity[Y]            -6.5113          7.5701      0.00046945      0.00073262
v  Velocity[Z]            -24.235          18.016        -0.17601       -0.073474
v  ǁVelocityǁ           0.0083477          49.086          4.0845          3.9195
v  Pressure               -1185.7          203.12          182.68          190.01
v  k                   7.3025e-07          9.0785         0.07232        0.057905
v  omega                 0.056406      5.9795e+05            4587          1406.8
v  TempC                  -123.25          596.65          32.301          32.411
v  Density                0.40733          2.3024          1.2104          1.2302
v  TurbVisc            1.9681e-12       0.0022896       7.693e-05      0.00011507
v  CourantNb                    0          28.706         0.70671         0.50588
v  FourierNb            0.0024766          4.5765        0.078601        0.097533
v  total_pressure      1.0014e+05      1.0153e+05      1.0151e+05      1.0152e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41556          2.3024          1.1351          1.1902


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.008852           28.79         0.78531         0.60341


 TIME FOR THE TIME STEP              164:        0.66933E+02

===============================================================


 INSTANT    0.144300000E-01   TIME STEP NUMBER             165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.174902437E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872212E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63777E+02 0.73068E+01
   Friction velocity        uet   :  0.17052E-02 0.45469E+01
   Friction velocity        uk    :  0.18695E-01 0.16786E+01
   Dimensionless distance   yplus :  0.28842E+00 0.42970E+02
   Friction thermal sca.    tstar : -0.22063E+03 0.44418E+02
   Rough dim-less th. sca.  tplus :  0.21520E+00 0.12912E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     147021
   Nb of faces within the viscous sub-layer     :       5382
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        109 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20305E+00      27   0.18133E-01   0.26935E+02 0.12191E+03 
c  Velocity[X]                                      0.24149E+02 
c  Velocity[Y]                                      0.69430E+00 
c  Velocity[Z]                                      0.20924E+01 
c  Pressure     0.11397E-03     195   0.62090E-02   0.18226E+00 0.10737E+03 
c  k            0.57349E-02      19   0.91672E-03   0.34562E+01 0.86400E+03 
c  omega        0.13591E+03      37   0.50584E-03   0.15041E+11 0.28864E+04 
c  TempC        0.28029E+04      50   0.23742E-01   0.12278E+06 0.29027E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7988          48.015          3.8301           3.846
v  Velocity[Y]            -6.6728          7.8342      0.00048225      0.00073763
v  Velocity[Z]            -24.093          18.149        -0.17711       -0.073949
v  ǁVelocityǁ           0.0080933          48.485           4.087          3.9226
v  Pressure               -1180.4          201.13          180.64          187.99
v  k                   3.8239e-07          9.1592        0.072559        0.058215
v  omega                    0.643      5.7608e+06          4592.8          1406.4
v  TempC                  -126.47          587.45          32.482          32.636
v  Density                0.40605          2.3561          1.2101          1.2298
v  TurbVisc             2.878e-12         0.00229      7.7532e-05      0.00011595
v  CourantNb                    0           29.96         0.70705         0.50624
v  FourierNb            0.0024768          4.5988        0.079115        0.098248
v  total_pressure      1.0014e+05      1.0153e+05      1.0151e+05      1.0151e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41673          2.3561          1.1348          1.1899


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012196          30.047         0.78617         0.60449


 TIME FOR THE TIME STEP              165:        0.66532E+02

===============================================================


 INSTANT    0.145300000E-01   TIME STEP NUMBER             166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.144784421E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873990E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66203E+02 0.72692E+01
   Friction velocity        uet   :  0.47239E-02 0.45547E+01
   Friction velocity        uk    :  0.16173E-01 0.16815E+01
   Dimensionless distance   yplus :  0.28155E+00 0.42971E+02
   Friction thermal sca.    tstar : -0.22722E+03 0.60206E+02
   Rough dim-less th. sca.  tplus :  0.21007E+00 0.12912E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146897
   Nb of faces within the viscous sub-layer     :       5421
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         93 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20309E+00      26   0.19063E-01   0.26967E+02 0.12185E+03 
c  Velocity[X]                                      0.24163E+02 
c  Velocity[Y]                                      0.68833E+00 
c  Velocity[Z]                                      0.21158E+01 
c  Pressure     0.11326E-03     211   0.62167E-02   0.18084E+00 0.13381E+03 
c  k            0.57485E-02      19   0.93119E-03   0.34631E+01 0.86289E+03 
c  omega        0.50334E+03      32   0.68063E-04   0.40939E+10 0.15512E+04 
c  TempC        0.28123E+04      48   0.24484E-01   0.12120E+06 0.28737E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7681          48.355          3.8314          3.8486
v  Velocity[Y]            -6.6004          7.9463      0.00050275      0.00074236
v  Velocity[Z]            -24.455          18.021         -0.1782       -0.074417
v  ǁVelocityǁ           0.0095127          48.777          4.0894          3.9256
v  Pressure               -1179.9          198.44          178.18           185.5
v  k                    4.859e-08          9.2984        0.072805        0.058524
v  omega                 0.067581      2.9045e+06          4593.9          1405.6
v  TempC                  -129.68          603.48          32.663          32.863
v  Density                0.41039          2.4079          1.2097          1.2294
v  TurbVisc            1.0769e-12       0.0022901      7.8115e-05      0.00011681
v  CourantNb                    0          28.357          0.7074         0.50661
v  FourierNb             0.002477          4.6159        0.079613         0.09894
v  total_pressure      1.0015e+05      1.0152e+05       1.015e+05      1.0151e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41529          2.4079          1.1345          1.1895


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013186           28.44         0.78701         0.60555


 TIME FOR THE TIME STEP              166:        0.67570E+02

===============================================================


 INSTANT    0.146300000E-01   TIME STEP NUMBER             167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.509751215E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874612E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64260E+02 0.73421E+01
   Friction velocity        uet   :  0.31408E-02 0.46894E+01
   Friction velocity        uk    :  0.95371E-02 0.16953E+01
   Dimensionless distance   yplus :  0.10871E+00 0.44102E+02
   Friction thermal sca.    tstar : -0.61888E+03 0.59054E+02
   Rough dim-less th. sca.  tplus :  0.81109E-01 0.12974E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146809
   Nb of faces within the viscous sub-layer     :       5440
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        100 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20313E+00      27   0.18293E-01   0.27108E+02 0.12204E+03 
c  Velocity[X]                                      0.24233E+02 
c  Velocity[Y]                                      0.68878E+00 
c  Velocity[Z]                                      0.21855E+01 
c  Pressure     0.11739E-03     197   0.64175E-02   0.18745E+00 0.11659E+03 
c  k            0.57596E-02      19   0.94789E-03   0.34713E+01 0.86186E+03 
c  omega        0.18399E+03      35   0.12121E-03   0.12412E+10 0.86073E+03 
c  TempC        0.28215E+04      50   0.24537E-01   0.12321E+06 0.28873E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8174          47.717          3.8327          3.8512
v  Velocity[Y]            -6.5994          7.7828      0.00051077      0.00074766
v  Velocity[Z]            -23.778          18.012        -0.17927       -0.074887
v  ǁVelocityǁ           0.0068616          48.174          4.0918          3.9287
v  Pressure               -1186.8          196.75          176.04          183.36
v  k                   1.9895e-07          9.2445        0.073063        0.058834
v  omega                   3.3747      1.4762e+06          4593.9          1404.8
v  TempC                  -131.79          610.12          32.843          33.088
v  Density                0.40289          2.4618          1.2093           1.229
v  TurbVisc            1.9206e-13         0.00229      7.8702e-05      0.00011767
v  CourantNb                    0          29.934         0.70774         0.50697
v  FourierNb            0.0024773           4.629        0.080116        0.099639
v  total_pressure      1.0014e+05      1.0152e+05       1.015e+05      1.0151e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4125          2.4618          1.1342          1.1891


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0084044          30.021         0.78786         0.60661


 TIME FOR THE TIME STEP              167:        0.66951E+02

===============================================================


 INSTANT    0.147300000E-01   TIME STEP NUMBER             168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.115488590E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875414E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66909E+02 0.74680E+01
   Friction velocity        uet   :  0.16378E-02 0.46383E+01
   Friction velocity        uk    :  0.13093E-01 0.16869E+01
   Dimensionless distance   yplus :  0.14483E+00 0.43568E+02
   Friction thermal sca.    tstar : -0.31787E+03 0.60407E+02
   Rough dim-less th. sca.  tplus :  0.10806E+00 0.12945E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146796
   Nb of faces within the viscous sub-layer     :       5478
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         83 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20318E+00      27   0.18595E-01   0.27107E+02 0.12190E+03 
c  Velocity[X]                                      0.24233E+02 
c  Velocity[Y]                                      0.69924E+00 
c  Velocity[Z]                                      0.21752E+01 
c  Pressure     0.11435E-03     213   0.63712E-02   0.18268E+00 0.13689E+03 
c  k            0.57650E-02      19   0.94116E-03   0.34480E+01 0.85677E+03 
c  omega        0.13867E+03      35   0.14104E-03   0.85150E+09 0.71331E+03 
c  TempC        0.28307E+04      48   0.23536E-01   0.12419E+06 0.28887E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7876          48.083          3.8339          3.8538
v  Velocity[Y]            -6.4114          7.9277      0.00053749      0.00075154
v  Velocity[Z]            -24.127          18.021        -0.18034       -0.075353
v  ǁVelocityǁ           0.0076034          48.498          4.0942          3.9317
v  Pressure               -1188.4          193.94          173.56          180.88
v  k                   6.5672e-08           9.267        0.073334        0.059146
v  omega                  0.38057      8.0803e+05          4595.8          1404.1
v  TempC                  -134.54          607.99          33.025          33.314
v  Density                0.39986          2.4985          1.2089          1.2285
v  TurbVisc            8.9444e-13         0.00229      7.9273e-05       0.0001185
v  CourantNb                    0          28.251         0.70806         0.50733
v  FourierNb            0.0024775          4.6391         0.08061         0.10032
v  total_pressure      1.0014e+05      1.0152e+05       1.015e+05      1.0151e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41723          2.4985          1.1339          1.1888


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011019          28.334         0.78867         0.60765


 TIME FOR THE TIME STEP              168:        0.67554E+02

===============================================================


 INSTANT    0.148300000E-01   TIME STEP NUMBER             169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.131922818E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873937E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64573E+02 0.72465E+01
   Friction velocity        uet   :  0.14003E-02 0.45814E+01
   Friction velocity        uk    :  0.15626E-01 0.16915E+01
   Dimensionless distance   yplus :  0.16770E+00 0.43544E+02
   Friction thermal sca.    tstar : -0.42662E+03 0.57585E+02
   Rough dim-less th. sca.  tplus :  0.12513E+00 0.12943E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146623
   Nb of faces within the viscous sub-layer     :       5529
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         86 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20323E+00      27   0.18585E-01   0.27256E+02 0.12210E+03 
c  Velocity[X]                                      0.24439E+02 
c  Velocity[Y]                                      0.69643E+00 
c  Velocity[Z]                                      0.21202E+01 
c  Pressure     0.11370E-03     175   0.62184E-02   0.18166E+00 0.86858E+02 
c  k            0.57647E-02      19   0.92827E-03   0.34418E+01 0.85390E+03 
c  omega        0.13526E+03      37   0.12927E-03   0.59608E+09 0.59661E+03 
c  TempC        0.28399E+04      50   0.23560E-01   0.12309E+06 0.28659E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8527          47.454          3.8352          3.8564
v  Velocity[Y]             -6.398          7.8079      0.00053918      0.00075659
v  Velocity[Z]            -23.766          17.988        -0.18138       -0.075813
v  ǁVelocityǁ           0.0079056          47.928          4.0966          3.9347
v  Pressure               -1193.1          192.56          172.01          179.33
v  k                   2.8733e-07          9.3544        0.073614        0.059457
v  omega                  0.29826      5.7714e+05          4597.9          1403.5
v  TempC                  -137.11          620.52          33.208           33.54
v  Density                0.40082           2.548          1.2085          1.2281
v  TurbVisc            2.9482e-13       0.0022898      7.9844e-05      0.00011934
v  CourantNb                    0          29.581          0.7084         0.50769
v  FourierNb            0.0024778          4.6468        0.081107           0.101
v  total_pressure      1.0013e+05      1.0152e+05       1.015e+05       1.015e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41341           2.548          1.1336          1.1884


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013741          29.667         0.78951          0.6087


 TIME FOR THE TIME STEP              169:        0.65246E+02

===============================================================


 INSTANT    0.149300000E-01   TIME STEP NUMBER             170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.224009228E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872547E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67143E+02 0.74164E+01
   Friction velocity        uet   :  0.10442E-02 0.46241E+01
   Friction velocity        uk    :  0.15631E-01 0.16969E+01
   Dimensionless distance   yplus :  0.16717E+00 0.43597E+02
   Friction thermal sca.    tstar : -0.62307E+03 0.66160E+02
   Rough dim-less th. sca.  tplus :  0.12473E+00 0.12946E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146622
   Nb of faces within the viscous sub-layer     :       5561
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         81 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20328E+00      28   0.18508E-01   0.27221E+02 0.12189E+03 
c  Velocity[X]                                      0.24356E+02 
c  Velocity[Y]                                      0.69258E+00 
c  Velocity[Z]                                      0.21731E+01 
c  Pressure     0.11415E-03     194   0.62399E-02   0.18201E+00 0.10287E+03 
c  k            0.57605E-02      19   0.92437E-03   0.34529E+01 0.85330E+03 
c  omega        0.13482E+03      36   0.12146E-03   0.48307E+09 0.53681E+03 
c  TempC        0.28488E+04      49   0.24231E-01   0.12234E+06 0.28472E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8287          47.805          3.8365           3.859
v  Velocity[Y]            -6.4146          7.8407      0.00055685      0.00076297
v  Velocity[Z]            -24.042          17.978        -0.18242       -0.076283
v  ǁVelocityǁ           0.0084284          48.213           4.099          3.9378
v  Pressure               -1201.1          190.48          170.15           177.5
v  k                   1.7643e-08          9.2359        0.073901        0.059765
v  omega                  0.09687      5.7715e+05          4599.1          1402.8
v  TempC                   -139.7          607.82          33.394          33.767
v  Density                0.39521          2.5961          1.2081          1.2277
v  TurbVisc            1.2108e-12       0.0022896      8.0428e-05       0.0001202
v  CourantNb                    0          28.006         0.70872         0.50805
v  FourierNb             0.002478          4.6526        0.081614         0.10171
v  total_pressure      1.0012e+05      1.0152e+05       1.015e+05       1.015e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40795          2.5961          1.1332           1.188


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01496          28.089         0.79033         0.60975


 TIME FOR THE TIME STEP              170:        0.66569E+02

===============================================================


 INSTANT    0.150300000E-01   TIME STEP NUMBER             171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.775752407E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872859E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65412E+02 0.74605E+01
   Friction velocity        uet   :  0.40794E-03 0.46163E+01
   Friction velocity        uk    :  0.13384E-01 0.16904E+01
   Dimensionless distance   yplus :  0.13610E+00 0.44681E+02
   Friction thermal sca.    tstar : -0.47578E+03 0.77939E+02
   Rough dim-less th. sca.  tplus :  0.10154E+00 0.13005E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146523
   Nb of faces within the viscous sub-layer     :       5593
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         80 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20333E+00      28   0.18359E-01   0.26977E+02 0.12121E+03 
c  Velocity[X]                                      0.24131E+02 
c  Velocity[Y]                                      0.69109E+00 
c  Velocity[Z]                                      0.21546E+01 
c  Pressure     0.11475E-03     197   0.63149E-02   0.18273E+00 0.11469E+03 
c  k            0.57568E-02      19   0.90890E-03   0.34669E+01 0.85312E+03 
c  omega        0.13492E+03      36   0.11496E-03   0.70164E+09 0.64604E+03 
c  TempC        0.28574E+04      47   0.24049E-01   0.12328E+06 0.28484E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8896          47.342          3.8379          3.8616
v  Velocity[Y]            -6.6747          7.6444      0.00057089      0.00076829
v  Velocity[Z]            -23.865          17.875        -0.18342       -0.076747
v  ǁVelocityǁ            0.009979          47.814          4.1015          3.9408
v  Pressure               -1204.6          188.67          168.08          175.49
v  k                   1.6076e-07          9.3487        0.074194        0.060073
v  omega                 0.090302      9.1703e+05          4600.6          1402.2
v  TempC                   -141.1          594.31          33.581          33.993
v  Density                 0.4009          2.6465          1.2077          1.2273
v  TurbVisc            1.1516e-13       0.0022896      8.0993e-05      0.00012104
v  CourantNb                    0          29.602         0.70905         0.50841
v  FourierNb            0.0024782          4.6571        0.082105         0.10239
v  total_pressure      1.0012e+05      1.0151e+05      1.0149e+05       1.015e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41246          2.6465          1.1329          1.1877


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013725          29.688         0.79116          0.6108


 TIME FOR THE TIME STEP              171:        0.67196E+02

===============================================================


 INSTANT    0.151300000E-01   TIME STEP NUMBER             172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.298831938E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874620E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68349E+02 0.73707E+01
   Friction velocity        uet   :  0.16258E-02 0.46309E+01
   Friction velocity        uk    :  0.15571E-01 0.16972E+01
   Dimensionless distance   yplus :  0.18591E+00 0.43798E+02
   Friction thermal sca.    tstar : -0.33506E+03 0.90852E+02
   Rough dim-less th. sca.  tplus :  0.13871E+00 0.12957E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146492
   Nb of faces within the viscous sub-layer     :       5635
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         65 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20338E+00      27   0.19352E-01   0.27132E+02 0.12143E+03 
c  Velocity[X]                                      0.24266E+02 
c  Velocity[Y]                                      0.69597E+00 
c  Velocity[Z]                                      0.21699E+01 
c  Pressure     0.11421E-03     210   0.62617E-02   0.18160E+00 0.13715E+03 
c  k            0.57540E-02      19   0.89809E-03   0.34793E+01 0.85270E+03 
c  omega        0.13535E+03      35   0.15292E-03   0.63114E+09 0.61227E+03 
c  TempC        0.28658E+04      49   0.23970E-01   0.12376E+06 0.28443E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8463           47.63          3.8393          3.8642
v  Velocity[Y]            -6.4886          7.5043      0.00060586      0.00077336
v  Velocity[Z]            -23.974          18.314        -0.18442       -0.077211
v  ǁVelocityǁ           0.0052919          48.053          4.1039          3.9438
v  Pressure               -1208.6          186.25           165.7          173.11
v  k                   2.7481e-07          9.4776        0.074484        0.060381
v  omega                  0.10061      5.7798e+05          4602.8          1401.6
v  TempC                  -133.18          598.62           33.77          34.218
v  Density                0.40715          2.6745          1.2073          1.2268
v  TurbVisc             7.471e-13       0.0022901      8.1548e-05      0.00012186
v  CourantNb                    0          27.931         0.70938         0.50878
v  FourierNb            0.0024785          4.6605        0.082587         0.10306
v  total_pressure      1.0012e+05      1.0151e+05      1.0149e+05       1.015e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41435          2.6745          1.1326          1.1873


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010029          28.013         0.79197         0.61183


 TIME FOR THE TIME STEP              172:        0.67689E+02

===============================================================


 INSTANT    0.152300000E-01   TIME STEP NUMBER             173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.574343975E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873711E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65932E+02 0.75061E+01
   Friction velocity        uet   :  0.12419E-02 0.46914E+01
   Friction velocity        uk    :  0.19261E-01 0.17119E+01
   Dimensionless distance   yplus :  0.21850E+00 0.43577E+02
   Friction thermal sca.    tstar : -0.31225E+03 0.96414E+02
   Rough dim-less th. sca.  tplus :  0.16303E+00 0.12945E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146360
   Nb of faces within the viscous sub-layer     :       5679
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         75 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20342E+00      27   0.18952E-01   0.27460E+02 0.12203E+03 
c  Velocity[X]                                      0.24585E+02 
c  Velocity[Y]                                      0.70421E+00 
c  Velocity[Z]                                      0.21698E+01 
c  Pressure     0.11536E-03     196   0.64385E-02   0.18341E+00 0.12335E+03 
c  k            0.57549E-02      19   0.90619E-03   0.34914E+01 0.85226E+03 
c  omega        0.13528E+03      37   0.18924E-03   0.78722E+09 0.68283E+03 
c  TempC        0.28742E+04      48   0.23240E-01   0.12381E+06 0.28353E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8809          47.066          3.8407          3.8668
v  Velocity[Y]            -6.3481          7.6048      0.00060425      0.00077532
v  Velocity[Z]            -23.548          17.897        -0.18544        -0.07768
v  ǁVelocityǁ           0.0059178          47.501          4.1063          3.9469
v  Pressure               -1215.2          184.36           163.6             171
v  k                   1.4484e-07          9.4498        0.074764        0.060688
v  omega                  0.17454      9.6216e+05          4604.4            1401
v  TempC                  -115.71          593.61          33.958          34.444
v  Density                0.40513          2.5234          1.2069          1.2264
v  TurbVisc             1.243e-12       0.0022904      8.2119e-05      0.00012271
v  CourantNb                    0          29.268         0.70972         0.50914
v  FourierNb            0.0024787          4.6631        0.083084         0.10375
v  total_pressure      1.0011e+05      1.0151e+05      1.0149e+05       1.015e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4152          2.2686          1.1323           1.187


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0073258          29.353          0.7928         0.61289


 TIME FOR THE TIME STEP              173:        0.67044E+02

===============================================================


 INSTANT    0.153300000E-01   TIME STEP NUMBER             174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.440857652E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875040E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68592E+02 0.75252E+01
   Friction velocity        uet   :  0.69282E-03 0.46122E+01
   Friction velocity        uk    :  0.99667E-02 0.17054E+01
   Dimensionless distance   yplus :  0.10204E+00 0.44692E+02
   Friction thermal sca.    tstar : -0.34056E+03 0.13097E+03
   Rough dim-less th. sca.  tplus :  0.76134E-01 0.13005E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146258
   Nb of faces within the viscous sub-layer     :       5704
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         73 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20347E+00      27   0.19039E-01   0.27466E+02 0.12191E+03 
c  Velocity[X]                                      0.24613E+02 
c  Velocity[Y]                                      0.70331E+00 
c  Velocity[Z]                                      0.21493E+01 
c  Pressure     0.11465E-03     195   0.63795E-02   0.18232E+00 0.12420E+03 
c  k            0.57603E-02      19   0.91908E-03   0.35100E+01 0.85263E+03 
c  omega        0.13621E+03      36   0.22512E-03   0.38528E+10 0.14955E+04 
c  TempC        0.28825E+04      48   0.23274E-01   0.12326E+06 0.28196E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8203          47.362          3.8421          3.8694
v  Velocity[Y]            -6.2442          7.6428      0.00060429      0.00077757
v  Velocity[Z]            -23.932          18.211        -0.18641       -0.078144
v  ǁVelocityǁ           0.0090818          47.773          4.1088          3.9499
v  Pressure               -1219.7          182.24           161.5           168.9
v  k                   2.2248e-07          9.4454        0.075028        0.060994
v  omega                 0.064402       2.839e+06          4607.5          1400.5
v  TempC                  -125.67          616.69          34.147           34.67
v  Density                0.40747          2.2433          1.2065           1.226
v  TurbVisc            6.7483e-13       0.0022901      8.2681e-05      0.00012355
v  CourantNb                    0          27.707         0.71005         0.50951
v  FourierNb            0.0024789          4.6651         0.08357         0.10443
v  total_pressure      1.0011e+05      1.0151e+05      1.0149e+05      1.0149e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40747          2.0485           1.132          1.1866


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0061499          27.789         0.79362         0.61394


 TIME FOR THE TIME STEP              174:        0.66664E+02

===============================================================


 INSTANT    0.154300000E-01   TIME STEP NUMBER             175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.279552494E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873724E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66463E+02 0.73505E+01
   Friction velocity        uet   :  0.31206E-03 0.45520E+01
   Friction velocity        uk    :  0.33192E-02 0.17080E+01
   Dimensionless distance   yplus :  0.59352E-01 0.43985E+02
   Friction thermal sca.    tstar : -0.11451E+04 0.84859E+02
   Rough dim-less th. sca.  tplus :  0.44284E-01 0.12967E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146101
   Nb of faces within the viscous sub-layer     :       5747
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         73 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20351E+00      27   0.18731E-01   0.27313E+02 0.12144E+03 
c  Velocity[X]                                      0.24440E+02 
c  Velocity[Y]                                      0.69733E+00 
c  Velocity[Z]                                      0.21756E+01 
c  Pressure     0.11444E-03     198   0.61820E-02   0.18203E+00 0.12812E+03 
c  k            0.57706E-02      19   0.93220E-03   0.35287E+01 0.85296E+03 
c  omega        0.17188E+03      35   0.12171E-03   0.11423E+10 0.81999E+03 
c  TempC        0.28908E+04      52   0.23721E-01   0.12331E+06 0.28108E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8816          46.902          3.8436           3.872
v  Velocity[Y]            -6.0794          7.5599      0.00062081      0.00078865
v  Velocity[Z]            -23.476          17.829        -0.18738       -0.078607
v  ǁVelocityǁ           0.0092984          47.354          4.1112           3.953
v  Pressure               -1227.5          180.32          159.34          166.76
v  k                   1.9512e-07            9.58         0.07528        0.061301
v  omega               0.00018888      1.4452e+06          4607.2          1399.8
v  TempC                  -131.36          609.32          34.333          34.895
v  Density                0.39691          2.3947          1.2061          1.2256
v  TurbVisc            1.0051e-12         0.00229      8.3246e-05       0.0001244
v  CourantNb                    0          29.208         0.71037         0.50987
v  FourierNb            0.0024792          4.6666        0.084058         0.10511
v  total_pressure       1.001e+05      1.0151e+05      1.0148e+05      1.0149e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39691          2.0707          1.1317          1.1862


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0083651          29.292         0.79443         0.61498


 TIME FOR THE TIME STEP              175:        0.66656E+02

===============================================================


 INSTANT    0.155300000E-01   TIME STEP NUMBER             176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.110906390E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874945E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69641E+02 0.75911E+01
   Friction velocity        uet   :  0.10438E-02 0.46093E+01
   Friction velocity        uk    :  0.18619E-01 0.17155E+01
   Dimensionless distance   yplus :  0.20882E+00 0.44976E+02
   Friction thermal sca.    tstar : -0.47714E+03 0.95732E+02
   Rough dim-less th. sca.  tplus :  0.15581E+00 0.13020E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     146030
   Nb of faces within the viscous sub-layer     :       5773
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         64 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20356E+00      28   0.19309E-01   0.27402E+02 0.12151E+03 
c  Velocity[X]                                      0.24515E+02 
c  Velocity[Y]                                      0.69430E+00 
c  Velocity[Z]                                      0.21929E+01 
c  Pressure     0.11286E-03     195   0.60920E-02   0.17941E+00 0.12299E+03 
c  k            0.57843E-02      19   0.93538E-03   0.35297E+01 0.85104E+03 
c  omega        0.13852E+03      36   0.16339E-03   0.13066E+10 0.87594E+03 
c  TempC        0.28991E+04      50   0.23396E-01   0.12440E+06 0.28139E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9398          49.156          3.8449          3.8746
v  Velocity[Y]            -6.2018          7.6235      0.00065332      0.00079714
v  Velocity[Z]            -23.697          18.169        -0.18833       -0.079069
v  ǁVelocityǁ            0.011337          49.165          4.1136           3.956
v  Pressure               -1234.7          178.04           157.3          164.73
v  k                   2.1914e-07          9.4543        0.075522         0.06161
v  omega               3.9333e-05      1.3586e+06          4608.5          1399.2
v  TempC                  -136.07           657.1          34.519           35.12
v  Density                0.40022          2.4908          1.2057          1.2251
v  TurbVisc            8.8096e-13         0.00229      8.3806e-05      0.00012523
v  CourantNb                    0          27.592         0.71068         0.51023
v  FourierNb            0.0024794          4.6677         0.08454         0.10579
v  total_pressure      1.0009e+05       1.015e+05      1.0148e+05      1.0149e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40756          2.1906          1.1314          1.1859


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011392          27.673         0.79522         0.61602


 TIME FOR THE TIME STEP              176:        0.66899E+02

===============================================================


 INSTANT    0.156300000E-01   TIME STEP NUMBER             177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.207162857E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873703E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67144E+02 0.75433E+01
   Friction velocity        uet   :  0.12117E-02 0.46023E+01
   Friction velocity        uk    :  0.13021E-01 0.17071E+01
   Dimensionless distance   yplus :  0.15343E+00 0.44122E+02
   Friction thermal sca.    tstar : -0.33615E+03 0.86798E+02
   Rough dim-less th. sca.  tplus :  0.11447E+00 0.12975E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     145877
   Nb of faces within the viscous sub-layer     :       5818
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         77 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20360E+00      28   0.18422E-01   0.27513E+02 0.12162E+03 
c  Velocity[X]                                      0.24650E+02 
c  Velocity[Y]                                      0.70016E+00 
c  Velocity[Z]                                      0.21632E+01 
c  Pressure     0.11650E-03     192   0.63284E-02   0.18539E+00 0.11646E+03 
c  k            0.57994E-02      19   0.92863E-03   0.35220E+01 0.84804E+03 
c  omega        0.13814E+03      37   0.22530E-03   0.24854E+10 0.12031E+04 
c  TempC        0.29075E+04      48   0.22973E-01   0.12448E+06 0.28057E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8764           47.76          3.8464          3.8772
v  Velocity[Y]            -6.5022          7.6637      0.00066856      0.00080106
v  Velocity[Z]            -23.401          17.935        -0.18927       -0.079531
v  ǁVelocityǁ            0.011441          47.804           4.116           3.959
v  Pressure               -1236.9          176.21          155.41          162.83
v  k                   2.3267e-07          9.5581         0.07576         0.06192
v  omega               3.3539e-05      2.3207e+06          4611.1          1398.7
v  TempC                  -121.14          613.01          34.703          35.346
v  Density                0.37966          2.5765          1.2053          1.2247
v  TurbVisc             9.889e-13       0.0022898      8.4362e-05      0.00012606
v  CourantNb                    0          28.916           0.711         0.51059
v  FourierNb            0.0024796          4.6686         0.08502         0.10646
v  total_pressure      1.0009e+05       1.015e+05      1.0148e+05      1.0149e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.37966           2.173          1.1312          1.1855


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011573              29         0.79602         0.61705


 TIME FOR THE TIME STEP              177:        0.66742E+02

===============================================================


 INSTANT    0.157300000E-01   TIME STEP NUMBER             178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.195540148E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873443E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69552E+02 0.75066E+01
   Friction velocity        uet   :  0.26394E-02 0.46426E+01
   Friction velocity        uk    :  0.10340E-01 0.17131E+01
   Dimensionless distance   yplus :  0.10876E+00 0.43954E+02
   Friction thermal sca.    tstar : -0.31561E+03 0.10432E+03
   Rough dim-less th. sca.  tplus :  0.81144E-01 0.12966E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     145752
   Nb of faces within the viscous sub-layer     :       5834
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         67 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20365E+00      28   0.18806E-01   0.27391E+02 0.12122E+03 
c  Velocity[X]                                      0.24502E+02 
c  Velocity[Y]                                      0.69958E+00 
c  Velocity[Z]                                      0.21890E+01 
c  Pressure     0.11532E-03     210   0.62817E-02   0.18308E+00 0.14473E+03 
c  k            0.58142E-02      19   0.92130E-03   0.35312E+01 0.84723E+03 
c  omega        0.14890E+03      35   0.13510E-03   0.92782E+09 0.73787E+03 
c  TempC        0.29160E+04      48   0.22897E-01   0.12297E+06 0.27795E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8245          47.692          3.8477          3.8798
v  Velocity[Y]            -6.3952          7.6115       0.0006659      0.00080136
v  Velocity[Z]              -23.5          18.299        -0.19021       -0.079993
v  ǁVelocityǁ           0.0091732          47.724          4.1183           3.962
v  Pressure               -1241.4          173.88          153.04           160.5
v  k                   2.4708e-07          9.4986        0.075986        0.062226
v  omega               1.1742e-05       1.186e+06          4611.2          1398.1
v  TempC                  -129.86          599.61          34.887          35.572
v  Density                0.39855          2.3235           1.205          1.2243
v  TurbVisc            1.0495e-12       0.0022897       8.494e-05       0.0001269
v  CourantNb                    0          27.294         0.71131         0.51095
v  FourierNb            0.0024799          4.6693        0.085516         0.10715
v  total_pressure      1.0008e+05       1.015e+05      1.0148e+05      1.0149e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39855          2.2279          1.1309          1.1852


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012273          27.398         0.79683          0.6181


 TIME FOR THE TIME STEP              178:        0.67447E+02

===============================================================


 INSTANT    0.158300000E-01   TIME STEP NUMBER             179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.563917478E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873853E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67702E+02 0.76225E+01
   Friction velocity        uet   :  0.12565E-02 0.47112E+01
   Friction velocity        uk    :  0.10301E-01 0.17128E+01
   Dimensionless distance   yplus :  0.12503E+00 0.43894E+02
   Friction thermal sca.    tstar : -0.37661E+03 0.84988E+02
   Rough dim-less th. sca.  tplus :  0.93287E-01 0.12962E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     145674
   Nb of faces within the viscous sub-layer     :       5848
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         60 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20370E+00      27   0.19012E-01   0.27507E+02 0.12135E+03 
c  Velocity[X]                                      0.24535E+02 
c  Velocity[Y]                                      0.71796E+00 
c  Velocity[Z]                                      0.22543E+01 
c  Pressure     0.11655E-03     199   0.64289E-02   0.18510E+00 0.13685E+03 
c  k            0.58306E-02      19   0.91132E-03   0.35483E+01 0.84747E+03 
c  omega        0.13693E+03      36   0.12484E-03   0.47896E+09 0.53054E+03 
c  TempC        0.29244E+04      48   0.22958E-01   0.12270E+06 0.27675E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9731          47.218          3.8492          3.8825
v  Velocity[Y]            -6.3395          7.6797        0.000663      0.00080152
v  Velocity[Z]            -23.115          17.974        -0.19111       -0.080452
v  ǁVelocityǁ           0.0057903           47.26          4.1207          3.9651
v  Pressure               -1250.3          171.77          150.86          158.33
v  k                   2.5941e-07          9.5529        0.076215        0.062531
v  omega               1.0338e-05      6.1781e+05            4611          1397.5
v  TempC                  -137.16          609.08          35.069          35.797
v  Density                0.40467          2.4648          1.2046          1.2238
v  TurbVisc            1.1139e-12       0.0022901      8.5523e-05      0.00012775
v  CourantNb                    0           28.84         0.71163         0.51132
v  FourierNb            0.0024801          4.6698        0.086016         0.10784
v  total_pressure      1.0007e+05       1.015e+05      1.0148e+05      1.0148e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40645           2.282          1.1306          1.1848


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0097192          28.925         0.79764         0.61915


 TIME FOR THE TIME STEP              179:        0.66855E+02

===============================================================


 INSTANT    0.159300000E-01   TIME STEP NUMBER             180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.968162123E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875656E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69868E+02 0.76928E+01
   Friction velocity        uet   :  0.23969E-02 0.46073E+01
   Friction velocity        uk    :  0.16762E-01 0.17126E+01
   Dimensionless distance   yplus :  0.18131E+00 0.45122E+02
   Friction thermal sca.    tstar : -0.30071E+03 0.82123E+02
   Rough dim-less th. sca.  tplus :  0.13528E+00 0.13028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     145535
   Nb of faces within the viscous sub-layer     :       5867
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         59 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20375E+00      27   0.18944E-01   0.27295E+02 0.12075E+03 
c  Velocity[X]                                      0.24392E+02 
c  Velocity[Y]                                      0.72614E+00 
c  Velocity[Z]                                      0.21777E+01 
c  Pressure     0.11764E-03     216   0.64946E-02   0.18679E+00 0.16866E+03 
c  k            0.58475E-02      19   0.89934E-03   0.35642E+01 0.84758E+03 
c  omega        0.13605E+03      35   0.12204E-03   0.48874E+09 0.53562E+03 
c  TempC        0.29330E+04      50   0.23140E-01   0.12286E+06 0.27604E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9226          47.413          3.8505          3.8851
v  Velocity[Y]            -6.2554          7.6716      0.00065549      0.00080258
v  Velocity[Z]            -23.426          18.461        -0.19201       -0.080915
v  ǁVelocityǁ           0.0066947          47.455           4.123          3.9681
v  Pressure               -1256.1          169.33           148.2          155.69
v  k                   3.0925e-07          9.6377        0.076443        0.062835
v  omega               1.2142e-05      5.8036e+05          4612.4          1396.9
v  TempC                  -138.92          602.72          35.251          36.023
v  Density                0.40033          2.5971          1.2042          1.2234
v  TurbVisc            1.1691e-12       0.0022905      8.6096e-05      0.00012858
v  CourantNb                    0          27.051         0.71192         0.51168
v  FourierNb            0.0024803          4.6701        0.086504         0.10852
v  total_pressure      1.0007e+05      1.0149e+05      1.0147e+05      1.0148e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41394          2.3351          1.1303          1.1845


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0064408          27.131         0.79842         0.62019


 TIME FOR THE TIME STEP              180:        0.68338E+02

===============================================================


 INSTANT    0.160300000E-01   TIME STEP NUMBER             181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.166597583E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875482E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67304E+02 0.75209E+01
   Friction velocity        uet   :  0.91999E-03 0.46133E+01
   Friction velocity        uk    :  0.81066E-02 0.17209E+01
   Dimensionless distance   yplus :  0.13963E+00 0.44475E+02
   Friction thermal sca.    tstar : -0.33670E+03 0.13121E+03
   Rough dim-less th. sca.  tplus :  0.10418E+00 0.12994E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     145394
   Nb of faces within the viscous sub-layer     :       5899
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         59 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20379E+00      27   0.18694E-01   0.27244E+02 0.12051E+03 
c  Velocity[X]                                      0.24285E+02 
c  Velocity[Y]                                      0.72908E+00 
c  Velocity[Z]                                      0.22294E+01 
c  Pressure     0.11782E-03     211   0.63193E-02   0.18673E+00 0.16100E+03 
c  k            0.58639E-02      19   0.89752E-03   0.35728E+01 0.84680E+03 
c  omega        0.13616E+03      37   0.18346E-03   0.85604E+09 0.70750E+03 
c  TempC        0.29414E+04      48   0.22974E-01   0.12329E+06 0.27565E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9804          47.918          3.8519          3.8877
v  Velocity[Y]            -6.1122          7.5789      0.00066357      0.00080992
v  Velocity[Z]            -23.109          17.783        -0.19291        -0.08137
v  ǁVelocityǁ           0.0081221          47.948          4.1253          3.9712
v  Pressure               -1259.9          166.95          145.73          153.22
v  k                   3.2993e-07          9.6854        0.076675         0.06314
v  omega               1.4648e-05      8.2139e+05          4614.5          1396.4
v  TempC                  -128.35          611.58          35.432          36.248
v  Density                0.40323          2.6313          1.2038           1.223
v  TurbVisc            1.3931e-12       0.0022903      8.6688e-05      0.00012943
v  CourantNb                    0          28.308         0.71221         0.51204
v  FourierNb            0.0024805          4.6704        0.087007         0.10921
v  total_pressure      1.0007e+05      1.0149e+05      1.0147e+05      1.0148e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41589          2.3861            1.13          1.1841


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0084369          28.392         0.79922         0.62125


 TIME FOR THE TIME STEP              181:        0.68041E+02

===============================================================


 INSTANT    0.161300000E-01   TIME STEP NUMBER             182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.462306267E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875591E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70087E+02 0.77253E+01
   Friction velocity        uet   :  0.19642E-02 0.47297E+01
   Friction velocity        uk    :  0.12422E-01 0.17234E+01
   Dimensionless distance   yplus :  0.13577E+00 0.44466E+02
   Friction thermal sca.    tstar : -0.43265E+03 0.99939E+02
   Rough dim-less th. sca.  tplus :  0.10130E+00 0.12993E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     145229
   Nb of faces within the viscous sub-layer     :       5939
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20384E+00      27   0.18949E-01   0.27302E+02 0.12051E+03 
c  Velocity[X]                                      0.24373E+02 
c  Velocity[Y]                                      0.71527E+00 
c  Velocity[Z]                                      0.22138E+01 
c  Pressure     0.11573E-03     213   0.63031E-02   0.18335E+00 0.16859E+03 
c  k            0.58772E-02      19   0.91066E-03   0.35840E+01 0.84635E+03 
c  omega        0.13662E+03      36   0.17320E-03   0.92020E+09 0.73276E+03 
c  TempC        0.29499E+04      48   0.22933E-01   0.12328E+06 0.27477E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0246          47.694          3.8533          3.8903
v  Velocity[Y]             -5.976          7.6244      0.00067928      0.00081417
v  Velocity[Z]            -23.065          18.241        -0.19378       -0.081825
v  ǁVelocityǁ           0.0063273          47.752          4.1275          3.9742
v  Pressure               -1268.1          164.33          143.18          150.67
v  k                   4.0709e-07          9.4823        0.076908        0.063443
v  omega               1.9903e-05      7.8628e+05          4615.9          1395.9
v  TempC                  -132.76          607.44          35.612          36.474
v  Density                 0.3992          2.4392          1.2034          1.2226
v  TurbVisc            1.4857e-12       0.0022901      8.7284e-05      0.00013028
v  CourantNb                    0          27.012          0.7125          0.5124
v  FourierNb            0.0024808          4.6706        0.087512         0.10991
v  total_pressure      1.0006e+05      1.0149e+05      1.0147e+05      1.0148e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40925          2.4392          1.1297          1.1838


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0067256           27.13         0.80002         0.62231


 TIME FOR THE TIME STEP              182:        0.67662E+02

===============================================================


 INSTANT    0.162300000E-01   TIME STEP NUMBER             183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.708494714E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874478E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67929E+02 0.77298E+01
   Friction velocity        uet   :  0.37108E-02 0.46510E+01
   Friction velocity        uk    :  0.12613E-01 0.17126E+01
   Dimensionless distance   yplus :  0.13157E+00 0.44734E+02
   Friction thermal sca.    tstar : -0.48469E+03 0.74013E+02
   Rough dim-less th. sca.  tplus :  0.98169E-01 0.13008E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     145085
   Nb of faces within the viscous sub-layer     :       5958
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20389E+00      28   0.18630E-01   0.27330E+02 0.12044E+03 
c  Velocity[X]                                      0.24441E+02 
c  Velocity[Y]                                      0.70767E+00 
c  Velocity[Z]                                      0.21816E+01 
c  Pressure     0.11443E-03     196   0.62994E-02   0.18111E+00 0.14013E+03 
c  k            0.58871E-02      19   0.92533E-03   0.35984E+01 0.84622E+03 
c  omega        0.13689E+03      36   0.16062E-03   0.66830E+09 0.62435E+03 
c  TempC        0.29585E+04      49   0.23500E-01   0.12257E+06 0.27311E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0734          47.414          3.8546          3.8929
v  Velocity[Y]             -6.342          7.4608      0.00067754      0.00081848
v  Velocity[Z]            -22.787          17.997        -0.19466       -0.082285
v  ǁVelocityǁ           0.0085433          47.456          4.1298          3.9772
v  Pressure               -1272.7          162.41          141.08          148.58
v  k                   4.6705e-07          9.5571        0.077158        0.063747
v  omega               4.9972e-05      7.1454e+05          4616.8          1395.4
v  TempC                  -133.98          605.78          35.791          36.699
v  Density                0.40108          2.5157           1.203          1.2221
v  TurbVisc            1.8326e-12         0.00229      8.7883e-05      0.00013114
v  CourantNb                    0          28.297         0.71279         0.51276
v  FourierNb             0.002481          4.6708        0.088024         0.11061
v  total_pressure      1.0005e+05      1.0149e+05      1.0147e+05      1.0147e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41401          2.4898          1.1294          1.1834


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0080569           28.38         0.80081         0.62337


 TIME FOR THE TIME STEP              183:        0.66850E+02

===============================================================


 INSTANT    0.163300000E-01   TIME STEP NUMBER             184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.218324110E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874947E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70673E+02 0.76735E+01
   Friction velocity        uet   :  0.20096E-02 0.46158E+01
   Friction velocity        uk    :  0.12397E-01 0.17148E+01
   Dimensionless distance   yplus :  0.12928E+00 0.46016E+02
   Friction thermal sca.    tstar : -0.33116E+03 0.14745E+03
   Rough dim-less th. sca.  tplus :  0.96455E-01 0.13075E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     144970
   Nb of faces within the viscous sub-layer     :       5977
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         59 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20394E+00      28   0.19982E-01   0.27086E+02 0.11978E+03 
c  Velocity[X]                                      0.24175E+02 
c  Velocity[Y]                                      0.69812E+00 
c  Velocity[Z]                                      0.22136E+01 
c  Pressure     0.11553E-03     210   0.62897E-02   0.18240E+00 0.16670E+03 
c  k            0.58909E-02      19   0.93386E-03   0.36084E+01 0.84551E+03 
c  omega        0.13861E+03      36   0.77440E-03   0.48419E+11 0.46966E+04 
c  TempC        0.29668E+04      49   0.23058E-01   0.12381E+06 0.27364E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1095          48.175           3.856          3.8955
v  Velocity[Y]            -6.2059          7.4085      0.00066882      0.00081726
v  Velocity[Z]            -22.795          18.276        -0.19552       -0.082745
v  ǁVelocityǁ           0.0080226          48.204           4.132          3.9802
v  Pressure               -1278.7          159.68          138.64          146.14
v  k                   5.4562e-07           9.777        0.077418        0.064051
v  omega               0.00011292      1.0351e+07          4624.3          1395.4
v  TempC                  -135.82          609.99          35.972          36.924
v  Density                0.40183          2.5378          1.2027          1.2217
v  TurbVisc            2.1019e-12         0.00229      8.8474e-05      0.00013198
v  CourantNb                    0           27.48         0.71306         0.51311
v  FourierNb            0.0024812          4.6709        0.088529          0.1113
v  total_pressure      1.0005e+05      1.0148e+05      1.0146e+05      1.0147e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41298          2.5378          1.1291          1.1831


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010873          27.594         0.80159         0.62442


 TIME FOR THE TIME STEP              184:        0.68207E+02

===============================================================


 INSTANT    0.164300000E-01   TIME STEP NUMBER             185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.136898960E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874063E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68536E+02 0.76764E+01
   Friction velocity        uet   :  0.13190E-02 0.47451E+01
   Friction velocity        uk    :  0.16029E-01 0.17359E+01
   Dimensionless distance   yplus :  0.18767E+00 0.45272E+02
   Friction thermal sca.    tstar : -0.51032E+03 0.96275E+02
   Rough dim-less th. sca.  tplus :  0.14002E+00 0.13036E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     144882
   Nb of faces within the viscous sub-layer     :       5982
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         57 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20398E+00      28   0.19277E-01   0.27756E+02 0.12112E+03 
c  Velocity[X]                                      0.24834E+02 
c  Velocity[Y]                                      0.71192E+00 
c  Velocity[Z]                                      0.22097E+01 
c  Pressure     0.11770E-03     210   0.64815E-02   0.18604E+00 0.16011E+03 
c  k            0.58880E-02      19   0.93238E-03   0.35925E+01 0.84164E+03 
c  omega        0.16744E+04      30   0.81215E-04   0.85146E+11 0.57589E+04 
c  TempC        0.29752E+04      52   0.22899E-01   0.12440E+06 0.27344E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1295          48.393          3.8574          3.8981
v  Velocity[Y]            -6.1797          7.4466      0.00065084      0.00081726
v  Velocity[Z]            -22.392          18.099        -0.19639       -0.083205
v  ǁVelocityǁ             0.01132          48.445          4.1343          3.9833
v  Pressure               -1287.7          157.47           136.3          143.83
v  k                   6.3588e-07          9.7661          0.0777        0.064358
v  omega               0.00034636      1.0564e+07          4627.7          1395.3
v  TempC                  -138.28          612.67          36.154           37.15
v  Density                0.39992          2.5717          1.2023          1.2213
v  TurbVisc            2.4548e-12       0.0022899      8.9048e-05      0.00013282
v  CourantNb                    0          27.992         0.71335         0.51348
v  FourierNb            0.0024815           4.671        0.089026         0.11199
v  total_pressure      1.0004e+05      1.0148e+05      1.0146e+05      1.0147e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41551          2.5717          1.1288          1.1827


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013654          28.074         0.80237         0.62546


 TIME FOR THE TIME STEP              185:        0.67686E+02

===============================================================


 INSTANT    0.165300000E-01   TIME STEP NUMBER             186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.351094017E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874247E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70820E+02 0.78539E+01
   Friction velocity        uet   :  0.11868E-02 0.46979E+01
   Friction velocity        uk    :  0.14737E-01 0.17328E+01
   Dimensionless distance   yplus :  0.16548E+00 0.46411E+02
   Friction thermal sca.    tstar : -0.30753E+03 0.14934E+03
   Rough dim-less th. sca.  tplus :  0.12347E+00 0.13095E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     144788
   Nb of faces within the viscous sub-layer     :       6009
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         56 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20404E+00      28   0.18931E-01   0.27888E+02 0.12128E+03 
c  Velocity[X]                                      0.24910E+02 
c  Velocity[Y]                                      0.72701E+00 
c  Velocity[Z]                                      0.22510E+01 
c  Pressure     0.11780E-03     210   0.64238E-02   0.18609E+00 0.16370E+03 
c  k            0.58780E-02      19   0.94096E-03   0.35892E+01 0.83936E+03 
c  omega        0.25997E+04      29   0.27325E-04   0.22238E+11 0.33833E+04 
c  TempC        0.29834E+04      49   0.22300E-01   0.12356E+06 0.27167E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1407          48.075          3.8588          3.9007
v  Velocity[Y]            -6.0714          7.4637      0.00064826      0.00081508
v  Velocity[Z]            -22.759          18.588        -0.19722       -0.083661
v  ǁVelocityǁ            0.010355           48.12          4.1365          3.9863
v  Pressure               -1291.6          154.89          133.96           141.5
v  k                   1.5489e-07          9.7949        0.077996        0.064663
v  omega               0.00085049      5.3079e+06          4624.8          1394.3
v  TempC                  -140.52          631.05           36.34          37.375
v  Density                0.39871          2.6186          1.2019          1.2209
v  TurbVisc            2.8603e-12       0.0022898      8.9632e-05      0.00013366
v  CourantNb           5.0873e-08          26.386         0.71363         0.51383
v  FourierNb            0.0024817          4.6711        0.089535         0.11268
v  total_pressure      1.0003e+05      1.0148e+05      1.0146e+05      1.0147e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41632          2.6186          1.1285          1.1824


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015993          26.465         0.80317         0.62652


 TIME FOR THE TIME STEP              186:        0.67787E+02

===============================================================


 INSTANT    0.166300000E-01   TIME STEP NUMBER             187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.482089603E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874296E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68297E+02 0.76857E+01
   Friction velocity        uet   :  0.67031E-03 0.46582E+01
   Friction velocity        uk    :  0.11769E-01 0.17378E+01
   Dimensionless distance   yplus :  0.13220E+00 0.45654E+02
   Friction thermal sca.    tstar : -0.32376E+03 0.10656E+03
   Rough dim-less th. sca.  tplus :  0.98639E-01 0.13056E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     144595
   Nb of faces within the viscous sub-layer     :       5998
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20408E+00      28   0.19096E-01   0.27452E+02 0.12020E+03 
c  Velocity[X]                                      0.24541E+02 
c  Velocity[Y]                                      0.70991E+00 
c  Velocity[Z]                                      0.22016E+01 
c  Pressure     0.11723E-03     211   0.63652E-02   0.18534E+00 0.16899E+03 
c  k            0.58657E-02      19   0.94417E-03   0.36031E+01 0.83928E+03 
c  omega        0.67806E+03      32   0.56922E-04   0.61541E+10 0.18589E+04 
c  TempC        0.29914E+04      49   0.22836E-01   0.12264E+06 0.26982E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1432          47.897          3.8603          3.9033
v  Velocity[Y]            -6.0794           7.345      0.00066455      0.00082445
v  Velocity[Z]            -22.329           18.06        -0.19804       -0.084113
v  ǁVelocityǁ             0.01125          47.937          4.1388          3.9893
v  Pressure               -1295.4          152.74          131.58          139.14
v  k                   8.3669e-08           9.985        0.078301        0.064964
v  omega               0.00046097      2.6795e+06          4622.8          1393.5
v  TempC                  -116.61          598.94          36.528          37.601
v  Density                 0.3906          2.6629          1.2015          1.2204
v  TurbVisc            2.5528e-12       0.0022898      9.0222e-05      0.00013452
v  CourantNb                    0          27.732         0.71392          0.5142
v  FourierNb            0.0024819          4.6711        0.090047         0.11339
v  total_pressure      1.0003e+05      1.0148e+05      1.0146e+05      1.0146e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41841          2.6629          1.1283           1.182


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016818          27.814         0.80396         0.62758


 TIME FOR THE TIME STEP              187:        0.67689E+02

===============================================================


 INSTANT    0.167300000E-01   TIME STEP NUMBER             188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.168538454E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874895E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71314E+02 0.79250E+01
   Friction velocity        uet   :  0.26946E-02 0.47154E+01
   Friction velocity        uk    :  0.97942E-02 0.17490E+01
   Dimensionless distance   yplus :  0.11006E+00 0.45439E+02
   Friction thermal sca.    tstar : -0.35778E+03 0.94233E+02
   Rough dim-less th. sca.  tplus :  0.82119E-01 0.13045E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     144512
   Nb of faces within the viscous sub-layer     :       6027
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20413E+00      27   0.19200E-01   0.27442E+02 0.12005E+03 
c  Velocity[X]                                      0.24460E+02 
c  Velocity[Y]                                      0.72300E+00 
c  Velocity[Z]                                      0.22595E+01 
c  Pressure     0.11884E-03     217   0.64337E-02   0.18791E+00 0.19213E+03 
c  k            0.58549E-02      19   0.94455E-03   0.36223E+01 0.83989E+03 
c  omega        0.22094E+03      34   0.11020E-03   0.21732E+10 0.11170E+04 
c  TempC        0.29990E+04      50   0.22472E-01   0.12361E+06 0.27006E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1474          48.554          3.8619           3.906
v  Velocity[Y]             -6.028          7.4194      0.00068677      0.00083174
v  Velocity[Z]            -22.304          18.203        -0.19885       -0.084569
v  ǁVelocityǁ           0.0048392          48.607          4.1412          3.9924
v  Pressure               -1304.8          150.05           128.9          136.51
v  k                   3.3009e-07          9.8838        0.078607        0.065263
v  omega               0.00024842      1.3646e+06          4622.5          1392.8
v  TempC                  -119.86          621.21          36.719          37.827
v  Density                0.40498          2.2561          1.2011            1.22
v  TurbVisc            6.2676e-13       0.0022901      9.0796e-05      0.00013535
v  CourantNb                    0           27.18         0.71421         0.51456
v  FourierNb            0.0024822          4.6712        0.090546         0.11408
v  total_pressure      1.0002e+05      1.0148e+05      1.0145e+05      1.0146e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41644          2.2561           1.128          1.1817


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01399          27.299         0.80475         0.62864


 TIME FOR THE TIME STEP              188:        0.67766E+02

===============================================================


 INSTANT    0.168300000E-01   TIME STEP NUMBER             189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.782316945E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876039E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68460E+02 0.78262E+01
   Friction velocity        uet   :  0.27638E-02 0.46908E+01
   Friction velocity        uk    :  0.12791E-01 0.17435E+01
   Dimensionless distance   yplus :  0.13464E+00 0.45417E+02
   Friction thermal sca.    tstar : -0.38467E+03 0.14389E+03
   Rough dim-less th. sca.  tplus :  0.10046E+00 0.13044E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     144372
   Nb of faces within the viscous sub-layer     :       6037
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20419E+00      28   0.18815E-01   0.27325E+02 0.11967E+03 
c  Velocity[X]                                      0.24399E+02 
c  Velocity[Y]                                      0.71499E+00 
c  Velocity[Z]                                      0.22111E+01 
c  Pressure     0.11528E-03     215   0.62505E-02   0.18192E+00 0.19590E+03 
c  k            0.58485E-02      19   0.94097E-03   0.36353E+01 0.83978E+03 
c  omega        0.14563E+03      36   0.23629E-03   0.41890E+10 0.15413E+04 
c  TempC        0.30064E+04      49   0.22660E-01   0.12272E+06 0.26826E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.137          47.822          3.8634          3.9086
v  Velocity[Y]            -6.3329          7.4633      0.00068704      0.00083388
v  Velocity[Z]            -22.144          17.968        -0.19966       -0.085025
v  ǁVelocityǁ            0.013057          47.872          4.1435          3.9954
v  Pressure               -1310.6          147.57          126.29          133.87
v  k                   8.6991e-09          9.9579        0.078908        0.065563
v  omega               0.00012377      2.1119e+06          4623.8          1392.4
v  TempC                  -122.98          592.68          36.911          38.052
v  Density                 0.3949           2.304          1.2007          1.2196
v  TurbVisc            1.4524e-12       0.0022903       9.137e-05      0.00013619
v  CourantNb                    0          27.392         0.71449         0.51492
v  FourierNb            0.0024824          4.6712        0.091048         0.11477
v  total_pressure      1.0001e+05      1.0147e+05      1.0145e+05      1.0146e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41781           2.304          1.1277          1.1813


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013731          27.474         0.80554         0.62969


 TIME FOR THE TIME STEP              189:        0.68084E+02

===============================================================


 INSTANT    0.169300000E-01   TIME STEP NUMBER             190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.459477483E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875898E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70555E+02 0.78188E+01
   Friction velocity        uet   :  0.30508E-02 0.46412E+01
   Friction velocity        uk    :  0.13165E-01 0.17458E+01
   Dimensionless distance   yplus :  0.14800E+00 0.45424E+02
   Friction thermal sca.    tstar : -0.39481E+03 0.88346E+02
   Rough dim-less th. sca.  tplus :  0.11043E+00 0.13044E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     144233
   Nb of faces within the viscous sub-layer     :       6077
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20424E+00      29   0.20538E-01   0.27400E+02 0.11971E+03 
c  Velocity[X]                                      0.24445E+02 
c  Velocity[Y]                                      0.71330E+00 
c  Velocity[Z]                                      0.22418E+01 
c  Pressure     0.11584E-03     209   0.62531E-02   0.18222E+00 0.18954E+03 
c  k            0.58471E-02      19   0.94723E-03   0.36610E+01 0.84115E+03 
c  omega        0.18394E+03      35   0.11460E-03   0.14551E+10 0.91458E+03 
c  TempC        0.30138E+04      51   0.22445E-01   0.12362E+06 0.26844E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1064          48.061          3.8649          3.9112
v  Velocity[Y]            -6.2144          7.4519      0.00069292      0.00083622
v  Velocity[Z]            -22.358          18.323        -0.20044       -0.085477
v  ǁVelocityǁ           0.0096552          48.088          4.1458          3.9984
v  Pressure               -1317.2          144.84          123.84          131.37
v  k                    6.289e-08          9.7724        0.079195        0.065862
v  omega               0.00010666      1.0826e+06          4624.6          1391.8
v  TempC                  -125.95          594.71          37.105          38.278
v  Density                0.40791          2.3519          1.2003          1.2192
v  TurbVisc            3.8262e-14         0.00229      9.1955e-05      0.00013705
v  CourantNb                    0          27.667          0.7148         0.51529
v  FourierNb            0.0024826          4.6712        0.091556         0.11547
v  total_pressure      1.0001e+05      1.0147e+05      1.0145e+05      1.0146e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4181          2.3519          1.1274           1.181


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014234          27.782         0.80635         0.63076


 TIME FOR THE TIME STEP              190:        0.67624E+02

===============================================================


 INSTANT    0.170300000E-01   TIME STEP NUMBER             191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.129053739E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873288E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69083E+02 0.78508E+01
   Friction velocity        uet   :  0.29986E-02 0.47149E+01
   Friction velocity        uk    :  0.91796E-02 0.17344E+01
   Dimensionless distance   yplus :  0.10490E+00 0.45259E+02
   Friction thermal sca.    tstar : -0.42579E+03 0.78583E+02
   Rough dim-less th. sca.  tplus :  0.78267E-01 0.13035E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     144031
   Nb of faces within the viscous sub-layer     :       6075
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20428E+00      28   0.18938E-01   0.28024E+02 0.12094E+03 
c  Velocity[X]                                      0.25041E+02 
c  Velocity[Y]                                      0.72082E+00 
c  Velocity[Z]                                      0.22620E+01 
c  Pressure     0.11854E-03     209   0.64437E-02   0.18680E+00 0.16850E+03 
c  k            0.58516E-02      19   0.95452E-03   0.36782E+01 0.84150E+03 
c  omega        0.14215E+03      36   0.45023E-03   0.17660E+11 0.30451E+04 
c  TempC        0.30212E+04      50   0.22624E-01   0.12238E+06 0.26629E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0852          48.047          3.8665          3.9138
v  Velocity[Y]            -6.1523            7.38      0.00068861      0.00083565
v  Velocity[Z]             -21.93          18.405        -0.20123       -0.085938
v  ǁVelocityǁ           0.0061605          48.094          4.1482          4.0015
v  Pressure               -1326.9          142.72          121.65          129.18
v  k                   1.0657e-07          9.8573        0.079466        0.066161
v  omega               8.6302e-05      4.5407e+06          4630.1          1391.7
v  TempC                  -129.05          604.95          37.298          38.503
v  Density                0.40696          2.3993          1.1999          1.2187
v  TurbVisc            2.7147e-13         0.00229      9.2525e-05      0.00013788
v  CourantNb                    0          27.343         0.71508         0.51565
v  FourierNb            0.0024829          4.6712        0.092052         0.11615
v  total_pressure           99998      1.0147e+05      1.0145e+05      1.0145e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41304          2.3993          1.1271          1.1806


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014615          27.425         0.80714         0.63181


 TIME FOR THE TIME STEP              191:        0.68084E+02

===============================================================


 INSTANT    0.171300000E-01   TIME STEP NUMBER             192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.993169113E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871907E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70920E+02 0.80254E+01
   Friction velocity        uet   :  0.13881E-02 0.46433E+01
   Friction velocity        uk    :  0.12636E-01 0.17388E+01
   Dimensionless distance   yplus :  0.20196E+00 0.45419E+02
   Friction thermal sca.    tstar : -0.29689E+03 0.69373E+02
   Rough dim-less th. sca.  tplus :  0.15069E+00 0.13044E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     143881
   Nb of faces within the viscous sub-layer     :       6109
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20433E+00      28   0.19285E-01   0.27368E+02 0.11939E+03 
c  Velocity[X]                                      0.24352E+02 
c  Velocity[Y]                                      0.72509E+00 
c  Velocity[Z]                                      0.22910E+01 
c  Pressure     0.11744E-03     210   0.62526E-02   0.18492E+00 0.18044E+03 
c  k            0.58608E-02      19   0.96663E-03   0.37009E+01 0.84235E+03 
c  omega        0.42887E+03      34   0.10343E-03   0.91660E+10 0.22420E+04 
c  TempC        0.30285E+04      50   0.22734E-01   0.12331E+06 0.26651E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0656          48.614          3.8681          3.9164
v  Velocity[Y]            -6.0344          7.3821      0.00067276      0.00083017
v  Velocity[Z]            -22.044          17.995        -0.20201       -0.086394
v  ǁVelocityǁ           0.0049722          48.664          4.1506          4.0045
v  Pressure               -1332.1          140.35          119.28          126.88
v  k                   1.6506e-08          10.017        0.079723        0.066461
v  omega                0.0001449      2.3545e+06          4629.8          1391.2
v  TempC                  -131.92          624.69           37.49          38.728
v  Density                0.40221          2.4509          1.1995          1.2183
v  TurbVisc            5.4551e-13       0.0022899      9.3105e-05      0.00013873
v  CourantNb                    0          25.743         0.71537         0.51601
v  FourierNb            0.0024831          4.6713        0.092556         0.11685
v  total_pressure           99993      1.0147e+05      1.0144e+05      1.0145e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40274          2.4509          1.1269          1.1803


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011551          25.858         0.80792         0.63286


 TIME FOR THE TIME STEP              192:        0.67777E+02

===============================================================


 INSTANT    0.172300000E-01   TIME STEP NUMBER             193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.102136354E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874178E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68517E+02 0.77738E+01
   Friction velocity        uet   :  0.92517E-03 0.46870E+01
   Friction velocity        uk    :  0.14061E-01 0.17548E+01
   Dimensionless distance   yplus :  0.19454E+00 0.45490E+02
   Friction thermal sca.    tstar : -0.38483E+03 0.65542E+02
   Rough dim-less th. sca.  tplus :  0.14515E+00 0.13047E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     143722
   Nb of faces within the viscous sub-layer     :       6142
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20438E+00      28   0.18944E-01   0.27602E+02 0.11977E+03 
c  Velocity[X]                                      0.24615E+02 
c  Velocity[Y]                                      0.72873E+00 
c  Velocity[Z]                                      0.22583E+01 
c  Pressure     0.11996E-03     211   0.63734E-02   0.18894E+00 0.18249E+03 
c  k            0.58717E-02      19   0.97416E-03   0.36832E+01 0.83843E+03 
c  omega        0.24055E+03      36   0.12286E-03   0.29966E+10 0.13034E+04 
c  TempC        0.30359E+04      50   0.21787E-01   0.12463E+06 0.26715E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0259          48.958          3.8698           3.919
v  Velocity[Y]            -5.9442          7.5013       0.0006642      0.00082931
v  Velocity[Z]            -21.651          17.974        -0.20278       -0.086854
v  ǁVelocityǁ           0.0079516          48.992          4.1529          4.0075
v  Pressure               -1335.8          138.03          116.95           124.6
v  k                   2.7247e-07          9.9544        0.079973        0.066765
v  omega               0.00010283       1.202e+06          4629.2          1390.5
v  TempC                  -134.58             604          37.681          38.953
v  Density                0.39337          2.5008          1.1991          1.2179
v  TurbVisc            7.3406e-14         0.00229      9.3656e-05      0.00013954
v  CourantNb                    0          27.579         0.71566         0.51638
v  FourierNb            0.0024833          4.6713        0.093039         0.11752
v  total_pressure           99989      1.0146e+05      1.0144e+05      1.0145e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39337          2.5008          1.1266          1.1799


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012823          27.696          0.8087          0.6339


 TIME FOR THE TIME STEP              193:        0.67898E+02

===============================================================


 INSTANT    0.173300000E-01   TIME STEP NUMBER             194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.451468427E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874699E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71249E+02 0.80044E+01
   Friction velocity        uet   :  0.84643E-03 0.48054E+01
   Friction velocity        uk    :  0.10348E-01 0.17479E+01
   Dimensionless distance   yplus :  0.14744E+00 0.46655E+02
   Friction thermal sca.    tstar : -0.31314E+03 0.60529E+02
   Rough dim-less th. sca.  tplus :  0.11000E+00 0.13108E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     143670
   Nb of faces within the viscous sub-layer     :       6179
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20443E+00      27   0.19371E-01   0.27694E+02 0.11985E+03 
c  Velocity[X]                                      0.24718E+02 
c  Velocity[Y]                                      0.71950E+00 
c  Velocity[Z]                                      0.22564E+01 
c  Pressure     0.11656E-03     228   0.62984E-02   0.18316E+00 0.24148E+03 
c  k            0.58821E-02      19   0.97555E-03   0.36640E+01 0.83439E+03 
c  omega        0.14857E+03      36   0.26971E-03   0.25409E+10 0.12013E+04 
c  TempC        0.30434E+04      51   0.21493E-01   0.12351E+06 0.26516E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.991          48.832          3.8713          3.9217
v  Velocity[Y]            -5.9335          7.4563      0.00067529       0.0008304
v  Velocity[Z]            -21.731          18.381        -0.20351       -0.087308
v  ǁVelocityǁ           0.0065283          48.885          4.1552          4.0106
v  Pressure               -1344.6           135.3             114          121.64
v  k                   9.0603e-08          9.9941        0.080216        0.067069
v  omega               0.00011265      1.4468e+06          4630.6            1390
v  TempC                     -137          602.29          37.872          39.179
v  Density                0.40265          2.5488          1.1987          1.2175
v  TurbVisc            7.8957e-13       0.0022898      9.4219e-05      0.00014036
v  CourantNb                    0           27.49         0.71595         0.51674
v  FourierNb            0.0024836          4.6713        0.093533          0.1182
v  total_pressure           99980      1.0146e+05      1.0144e+05      1.0145e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40758          2.5488          1.1263          1.1796


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0099981          27.611         0.80948         0.63494


 TIME FOR THE TIME STEP              194:        0.69278E+02

===============================================================


 INSTANT    0.174300000E-01   TIME STEP NUMBER             195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.182682501E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874645E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68758E+02 0.79107E+01
   Friction velocity        uet   :  0.17498E-02 0.47097E+01
   Friction velocity        uk    :  0.15314E-01 0.17540E+01
   Dimensionless distance   yplus :  0.20901E+00 0.46077E+02
   Friction thermal sca.    tstar : -0.51669E+03 0.64712E+02
   Rough dim-less th. sca.  tplus :  0.15594E+00 0.13078E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     143520
   Nb of faces within the viscous sub-layer     :       6197
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20448E+00      28   0.19578E-01   0.27410E+02 0.11911E+03 
c  Velocity[X]                                      0.24493E+02 
c  Velocity[Y]                                      0.71277E+00 
c  Velocity[Z]                                      0.22036E+01 
c  Pressure     0.11743E-03     224   0.62835E-02   0.18450E+00 0.22249E+03 
c  k            0.58942E-02      19   0.96789E-03   0.36706E+01 0.83348E+03 
c  omega        0.14353E+03      36   0.15831E-03   0.83779E+09 0.69270E+03 
c  TempC        0.30510E+04      50   0.22226E-01   0.12240E+06 0.26319E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9617          48.154          3.8729          3.9243
v  Velocity[Y]              -6.29           7.317      0.00067982      0.00083444
v  Velocity[Z]            -21.388          18.209        -0.20426       -0.087766
v  ǁVelocityǁ           0.0050127          48.205          4.1576          4.0136
v  Pressure               -1347.5           132.9          111.38          118.98
v  k                   1.9383e-07          10.196        0.080456        0.067369
v  omega               1.1433e-05      7.4839e+05            4629          1389.4
v  TempC                  -138.43           607.7          38.061          39.404
v  Density                0.40344           2.594          1.1983           1.217
v  TurbVisc            3.9787e-13       0.0022902      9.4807e-05      0.00014122
v  CourantNb                    0           26.76         0.71622          0.5171
v  FourierNb            0.0024838          4.6713        0.094051         0.11891
v  total_pressure           99977      1.0146e+05      1.0144e+05      1.0144e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41417           2.594           1.126          1.1793


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0094895          26.842         0.81027         0.63601


 TIME FOR THE TIME STEP              195:        0.69176E+02

===============================================================


 INSTANT    0.175300000E-01   TIME STEP NUMBER             196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.515787910E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872400E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71189E+02 0.79933E+01
   Friction velocity        uet   :  0.37944E-02 0.46844E+01
   Friction velocity        uk    :  0.15544E-01 0.17677E+01
   Dimensionless distance   yplus :  0.21582E+00 0.45979E+02
   Friction thermal sca.    tstar : -0.39549E+03 0.52240E+02
   Rough dim-less th. sca.  tplus :  0.16103E+00 0.13073E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     143421
   Nb of faces within the viscous sub-layer     :       6210
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20453E+00      28   0.20619E-01   0.27440E+02 0.11905E+03 
c  Velocity[X]                                      0.24446E+02 
c  Velocity[Y]                                      0.72388E+00 
c  Velocity[Z]                                      0.22699E+01 
c  Pressure     0.11641E-03     197   0.62468E-02   0.18228E+00 0.18266E+03 
c  k            0.59087E-02      19   0.94715E-03   0.36895E+01 0.83413E+03 
c  omega        0.13847E+03      36   0.15957E-03   0.88827E+09 0.71293E+03 
c  TempC        0.30584E+04      50   0.22387E-01   0.12277E+06 0.26282E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9366          51.168          3.8745          3.9269
v  Velocity[Y]            -6.1798          7.3425      0.00069383      0.00083338
v  Velocity[Z]            -21.551          18.464          -0.205       -0.088226
v  ǁVelocityǁ           0.0063546          51.176          4.1598          4.0166
v  Pressure               -1349.6          130.44           109.2          116.83
v  k                   5.1765e-08          10.077        0.080691        0.067668
v  omega               9.0072e-07       7.402e+05          4629.9          1388.9
v  TempC                  -113.19          587.83          38.252           39.63
v  Density                0.40096          2.6216          1.1979          1.2166
v  TurbVisc            7.8527e-13       0.0022904       9.539e-05      0.00014206
v  CourantNb                    0          27.899          0.7165         0.51746
v  FourierNb             0.002484          4.6713         0.09456          0.1196
v  total_pressure           99975      1.0146e+05      1.0143e+05      1.0144e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40669          2.6216          1.1257          1.1789


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0097466          28.016         0.81106         0.63707


 TIME FOR THE TIME STEP              196:        0.66699E+02

===============================================================


 INSTANT    0.176300000E-01   TIME STEP NUMBER             197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.298161174E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875371E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69001E+02 0.79783E+01
   Friction velocity        uet   :  0.22021E-02 0.48348E+01
   Friction velocity        uk    :  0.16040E-01 0.17638E+01
   Dimensionless distance   yplus :  0.21645E+00 0.46383E+02
   Friction thermal sca.    tstar : -0.33517E+03 0.66952E+02
   Rough dim-less th. sca.  tplus :  0.16150E+00 0.13094E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     143228
   Nb of faces within the viscous sub-layer     :       6228
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20457E+00      28   0.19866E-01   0.28020E+02 0.12018E+03 
c  Velocity[X]                                      0.24989E+02 
c  Velocity[Y]                                      0.74077E+00 
c  Velocity[Z]                                      0.22905E+01 
c  Pressure     0.11910E-03     211   0.63756E-02   0.18658E+00 0.20615E+03 
c  k            0.59270E-02      19   0.92881E-03   0.37121E+01 0.83521E+03 
c  omega        0.13853E+03      37   0.13440E-03   0.57063E+09 0.57159E+03 
c  TempC        0.30659E+04      50   0.22035E-01   0.12265E+06 0.26194E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8996          49.721          3.8761          3.9295
v  Velocity[Y]            -6.1264          7.3437      0.00068397      0.00083692
v  Velocity[Z]            -21.213          18.183        -0.20572        -0.08868
v  ǁVelocityǁ            0.010523          49.763          4.1621          4.0197
v  Pressure               -1358.2          128.45          106.81          114.45
v  k                   1.3533e-07          10.179        0.080917        0.067965
v  omega               3.4023e-08      5.8191e+05          4630.3          1388.5
v  TempC                   -106.5           599.4           38.44          39.855
v  Density                0.41021          2.2079          1.1975          1.2162
v  TurbVisc            3.1286e-13       0.0022903      9.5983e-05       0.0001429
v  CourantNb                    0          27.592         0.71679         0.51783
v  FourierNb            0.0024843          4.6713        0.095075         0.12031
v  total_pressure           99967      1.0145e+05      1.0143e+05      1.0144e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41691          2.2079          1.1255          1.1786


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0073023          27.713         0.81186         0.63814


 TIME FOR THE TIME STEP              197:        0.68041E+02

===============================================================


 INSTANT    0.177300000E-01   TIME STEP NUMBER             198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.541190499E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874817E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70687E+02 0.80583E+01
   Friction velocity        uet   :  0.23557E-02 0.47485E+01
   Friction velocity        uk    :  0.10283E-01 0.17687E+01
   Dimensionless distance   yplus :  0.10800E+00 0.46527E+02
   Friction thermal sca.    tstar : -0.34137E+03 0.56101E+02
   Rough dim-less th. sca.  tplus :  0.80578E-01 0.13101E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     143098
   Nb of faces within the viscous sub-layer     :       6283
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20462E+00      28   0.19525E-01   0.27735E+02 0.11944E+03 
c  Velocity[X]                                      0.24709E+02 
c  Velocity[Y]                                      0.73813E+00 
c  Velocity[Z]                                      0.22883E+01 
c  Pressure     0.11953E-03     213   0.65612E-02   0.18725E+00 0.21987E+03 
c  k            0.59475E-02      19   0.93261E-03   0.37331E+01 0.83614E+03 
c  omega        0.14401E+03      36   0.25529E-02   0.15592E+12 0.68693E+04 
c  TempC        0.30734E+04      51   0.21468E-01   0.12279E+06 0.26133E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8901          48.967          3.8777          3.9321
v  Velocity[Y]             -6.099          7.2257      0.00071872      0.00084937
v  Velocity[Z]            -21.317          18.377        -0.20644        -0.08914
v  ǁVelocityǁ            0.011055          49.013          4.1644          4.0227
v  Pressure                 -1364          125.74           104.3          111.97
v  k                    8.065e-08          10.369        0.081133        0.068259
v  omega               1.8822e-09      1.9798e+07          4645.9          1389.1
v  TempC                  -102.69          634.21          38.628          40.081
v  Density                0.40477          2.1193          1.1972          1.2158
v  TurbVisc            6.6161e-13       0.0022901      9.6591e-05      0.00014376
v  CourantNb                    0          26.218         0.71704         0.51819
v  FourierNb            0.0024845          4.6713        0.095606         0.12103
v  total_pressure           99961      1.0145e+05      1.0143e+05      1.0144e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40902          2.1193          1.1252          1.1782


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0065971          26.335         0.81265         0.63922


 TIME FOR THE TIME STEP              198:        0.68171E+02

===============================================================


 INSTANT    0.178300000E-01   TIME STEP NUMBER             199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.607921476E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874376E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68763E+02 0.79462E+01
   Friction velocity        uet   :  0.30051E-02 0.46719E+01
   Friction velocity        uk    :  0.17149E-01 0.17862E+01
   Dimensionless distance   yplus :  0.19348E+00 0.46511E+02
   Friction thermal sca.    tstar : -0.26592E+03 0.49915E+02
   Rough dim-less th. sca.  tplus :  0.14436E+00 0.13100E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     142924
   Nb of faces within the viscous sub-layer     :       6320
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20468E+00      28   0.20064E-01   0.27769E+02 0.11939E+03 
c  Velocity[X]                                      0.24729E+02 
c  Velocity[Y]                                      0.73830E+00 
c  Velocity[Z]                                      0.23026E+01 
c  Pressure     0.11833E-03     211   0.62919E-02   0.18518E+00 0.22075E+03 
c  k            0.59688E-02      20   0.94190E-03   0.37437E+01 0.83585E+03 
c  omega        0.50262E+04      27   0.36502E-04   0.46635E+11 0.45828E+04 
c  TempC        0.30810E+04      50   0.21817E-01   0.12185E+06 0.25959E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9482          48.555          3.8793          3.9348
v  Velocity[Y]            -6.0939          7.2512      0.00073122      0.00085339
v  Velocity[Z]            -21.036          18.221        -0.20712       -0.089595
v  ǁVelocityǁ           0.0094045          48.592          4.1667          4.0258
v  Pressure               -1368.6          123.42          101.87          109.53
v  k                   9.3113e-08           10.44        0.081346        0.068554
v  omega               7.9388e-09      9.9201e+06          4643.6          1388.4
v  TempC                  -109.21          597.11          38.813          40.306
v  Density                0.38924           2.072          1.1968          1.2153
v  TurbVisc            3.9331e-13       0.0022899      9.7196e-05      0.00014461
v  CourantNb                    0          28.133         0.71732         0.51855
v  FourierNb            0.0024847          4.6713        0.096134         0.12174
v  total_pressure           99956      1.0145e+05      1.0143e+05      1.0143e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40269           2.072          1.1249          1.1779


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0076381          28.251         0.81345         0.64029


 TIME FOR THE TIME STEP              199:        0.67524E+02

===============================================================


 INSTANT    0.179300000E-01   TIME STEP NUMBER             200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.348030471E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874980E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71515E+02 0.81359E+01
   Friction velocity        uet   :  0.34316E-02 0.47541E+01
   Friction velocity        uk    :  0.15899E-01 0.17883E+01
   Dimensionless distance   yplus :  0.15295E+00 0.46813E+02
   Friction thermal sca.    tstar : -0.29453E+03 0.47155E+02
   Rough dim-less th. sca.  tplus :  0.11411E+00 0.13116E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     142821
   Nb of faces within the viscous sub-layer     :       6351
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20473E+00      27   0.19485E-01   0.27663E+02 0.11904E+03 
c  Velocity[X]                                      0.24602E+02 
c  Velocity[Y]                                      0.73179E+00 
c  Velocity[Z]                                      0.23298E+01 
c  Pressure     0.11937E-03     228   0.63220E-02   0.18671E+00 0.26437E+03 
c  k            0.59885E-02      20   0.95574E-03   0.37538E+01 0.83541E+03 
c  omega        0.26431E+04      29   0.34663E-04   0.12015E+11 0.25313E+04 
c  TempC        0.30888E+04      51   0.22190E-01   0.12279E+06 0.25984E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8764          51.584          3.8809          3.9374
v  Velocity[Y]            -6.1218          7.1157      0.00072129      0.00085316
v  Velocity[Z]            -21.024          18.319         -0.2078       -0.090051
v  ǁVelocityǁ            0.011223          51.591          4.1689          4.0288
v  Pressure                 -1374          120.64          98.986          106.69
v  k                   7.6801e-08          10.465        0.081561         0.06885
v  omega               2.7765e-08      4.9811e+06          4641.4          1387.8
v  TempC                  -115.63          612.88          38.999          40.531
v  Density                0.40583          2.1543          1.1964          1.2149
v  TurbVisc            4.5534e-13       0.0022898      9.7815e-05      0.00014546
v  CourantNb                    0          27.703         0.71758         0.51891
v  FourierNb             0.002485          4.6713        0.096677         0.12246
v  total_pressure           99951      1.0145e+05      1.0142e+05      1.0143e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41755          2.1543          1.1247          1.1775


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010892          27.826         0.81426         0.64137


 TIME FOR THE TIME STEP              200:        0.68797E+02

===============================================================


 INSTANT    0.180300000E-01   TIME STEP NUMBER             201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.212517942E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874876E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68918E+02 0.80337E+01
   Friction velocity        uet   :  0.39606E-02 0.47548E+01
   Friction velocity        uk    :  0.11089E-01 0.17921E+01
   Dimensionless distance   yplus :  0.12267E+00 0.46899E+02
   Friction thermal sca.    tstar : -0.29179E+03 0.45847E+02
   Rough dim-less th. sca.  tplus :  0.91526E-01 0.13120E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     142685
   Nb of faces within the viscous sub-layer     :       6404
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20478E+00      27   0.20944E-01   0.27750E+02 0.11910E+03 
c  Velocity[X]                                      0.24705E+02 
c  Velocity[Y]                                      0.73512E+00 
c  Velocity[Z]                                      0.23104E+01 
c  Pressure     0.11884E-03     212   0.62669E-02   0.18570E+00 0.24017E+03 
c  k            0.60032E-02      19   0.95554E-03   0.37352E+01 0.83159E+03 
c  omega        0.35821E+03      35   0.17893E-03   0.57882E+10 0.17859E+04 
c  TempC        0.30965E+04      50   0.21498E-01   0.12432E+06 0.26073E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8801           49.36          3.8825            3.94
v  Velocity[Y]            -6.4004          7.0605      0.00070811      0.00084809
v  Velocity[Z]            -20.871          18.234        -0.20849        -0.09051
v  ǁVelocityǁ            0.011736          49.416          4.1712          4.0318
v  Pressure               -1380.5          118.08          96.485          104.16
v  k                    6.373e-08          10.567         0.08179        0.069151
v  omega               7.3562e-08      2.5114e+06          4641.3          1387.4
v  TempC                  -121.63          599.81          39.182          40.756
v  Density                0.39861          2.2422           1.196          1.2145
v  TurbVisc            3.7565e-13       0.0022897      9.8413e-05      0.00014629
v  CourantNb                    0          25.842         0.71785         0.51927
v  FourierNb            0.0024852          4.6713        0.097202         0.12316
v  total_pressure           99944      1.0144e+05      1.0142e+05      1.0143e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41231          2.2114          1.1244          1.1772


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014172          25.959         0.81506         0.64243


 TIME FOR THE TIME STEP              201:        0.68072E+02

===============================================================


 INSTANT    0.181300000E-01   TIME STEP NUMBER             202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.174177142E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875674E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70987E+02 0.80226E+01
   Friction velocity        uet   :  0.16547E-02 0.47026E+01
   Friction velocity        uk    :  0.17654E-01 0.17971E+01
   Dimensionless distance   yplus :  0.22328E+00 0.47217E+02
   Friction thermal sca.    tstar : -0.34384E+03 0.44259E+02
   Rough dim-less th. sca.  tplus :  0.16659E+00 0.13136E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     142540
   Nb of faces within the viscous sub-layer     :       6451
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20483E+00      28   0.20080E-01   0.28002E+02 0.11952E+03 
c  Velocity[X]                                      0.24940E+02 
c  Velocity[Y]                                      0.73641E+00 
c  Velocity[Z]                                      0.23256E+01 
c  Pressure     0.11781E-03     210   0.64163E-02   0.18350E+00 0.23292E+03 
c  k            0.60092E-02      19   0.94769E-03   0.37194E+01 0.82812E+03 
c  omega        0.19098E+03      36   0.18777E-03   0.20819E+10 0.10811E+04 
c  TempC        0.31044E+04      51   0.21572E-01   0.12383E+06 0.25948E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9522          49.213           3.884          3.9426
v  Velocity[Y]            -6.3119          7.1915      0.00071126      0.00084683
v  Velocity[Z]            -21.007          18.468        -0.20916       -0.090967
v  ǁVelocityǁ             0.01309          49.258          4.1733          4.0349
v  Pressure               -1386.2          115.56          94.087          101.77
v  k                   5.4147e-08          10.356        0.082033        0.069451
v  omega                8.574e-08       1.276e+06          4643.5          1387.1
v  TempC                  -125.14          599.25          39.367          40.981
v  Density                0.40458          2.3309          1.1956          1.2141
v  TurbVisc            3.1172e-13       0.0022896      9.9013e-05      0.00014712
v  CourantNb                    0          28.205         0.71811         0.51963
v  FourierNb            0.0024855          4.6713        0.097738         0.12387
v  total_pressure           99939      1.0144e+05      1.0142e+05      1.0143e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41338          2.1757          1.1241          1.1769


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015839          28.323         0.81585          0.6435


 TIME FOR THE TIME STEP              202:        0.68255E+02

===============================================================


 INSTANT    0.182300000E-01   TIME STEP NUMBER             203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.955958774E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874247E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69338E+02 0.80583E+01
   Friction velocity        uet   :  0.29277E-02 0.47881E+01
   Friction velocity        uk    :  0.12286E-01 0.17847E+01
   Dimensionless distance   yplus :  0.15528E+00 0.47454E+02
   Friction thermal sca.    tstar : -0.24728E+03 0.44074E+02
   Rough dim-less th. sca.  tplus :  0.11585E+00 0.13148E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     142411
   Nb of faces within the viscous sub-layer     :       6493
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20487E+00      28   0.19848E-01   0.28058E+02 0.11951E+03 
c  Velocity[X]                                      0.24930E+02 
c  Velocity[Y]                                      0.76471E+00 
c  Velocity[Z]                                      0.23635E+01 
c  Pressure     0.11853E-03     214   0.64772E-02   0.18455E+00 0.24482E+03 
c  k            0.60092E-02      20   0.94314E-03   0.37264E+01 0.82736E+03 
c  omega        0.14409E+03      36   0.15649E-03   0.88390E+09 0.70613E+03 
c  TempC        0.31120E+04      50   0.21949E-01   0.12249E+06 0.25735E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8796          49.278          3.8856          3.9453
v  Velocity[Y]            -6.3075          7.1745      0.00071167      0.00085068
v  Velocity[Z]            -20.521          18.232        -0.20984       -0.091437
v  ǁVelocityǁ            0.012856          49.333          4.1755          4.0379
v  Pressure               -1395.2          113.21          91.612          99.312
v  k                   4.5661e-08          10.401        0.082289        0.069747
v  omega                1.069e-07      6.5722e+05          4644.4          1386.6
v  TempC                  -127.51          598.77          39.553          41.208
v  Density                0.40484          2.3863          1.1952          1.2137
v  TurbVisc            2.6481e-13       0.0022897      9.9627e-05      0.00014797
v  CourantNb                    0          27.957         0.71837         0.51999
v  FourierNb            0.0024857          4.6713        0.098294         0.12459
v  total_pressure           99930      1.0144e+05      1.0142e+05      1.0142e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41338          2.2823          1.1238          1.1765


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017384           28.08         0.81667         0.64459


 TIME FOR THE TIME STEP              203:        0.68155E+02

===============================================================


 INSTANT    0.183300000E-01   TIME STEP NUMBER             204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.255695900E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875251E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71543E+02 0.81662E+01
   Friction velocity        uet   :  0.26634E-02 0.47335E+01
   Friction velocity        uk    :  0.13434E-01 0.17845E+01
   Dimensionless distance   yplus :  0.14668E+00 0.47258E+02
   Friction thermal sca.    tstar : -0.33091E+03 0.41596E+02
   Rough dim-less th. sca.  tplus :  0.10944E+00 0.13138E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     142292
   Nb of faces within the viscous sub-layer     :       6505
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20493E+00      29   0.20027E-01   0.27424E+02 0.11804E+03 
c  Velocity[X]                                      0.24279E+02 
c  Velocity[Y]                                      0.75340E+00 
c  Velocity[Z]                                      0.23923E+01 
c  Pressure     0.11639E-03     195   0.62380E-02   0.18118E+00 0.21479E+03 
c  k            0.60065E-02      20   0.92555E-03   0.37403E+01 0.82749E+03 
c  omega        0.13974E+03      36   0.14053E-03   0.91086E+09 0.71619E+03 
c  TempC        0.31196E+04      51   0.21443E-01   0.12323E+06 0.25740E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8747          49.688          3.8872          3.9479
v  Velocity[Y]            -6.2695           7.169      0.00071007      0.00084977
v  Velocity[Z]            -20.779           17.99        -0.21051       -0.091899
v  ǁVelocityǁ           0.0075151          49.734          4.1778          4.0409
v  Pressure               -1400.6          110.91          89.504          97.202
v  k                   3.8448e-08          10.488        0.082555        0.070041
v  omega               1.2572e-07      7.9588e+05            4646          1386.3
v  TempC                  -129.89          601.42          39.742          41.433
v  Density                0.40506           2.425          1.1948          1.2132
v  TurbVisc            2.2328e-13       0.0022902      0.00010023       0.0001488
v  CourantNb                    0          26.227         0.71863         0.52035
v  FourierNb             0.002486          4.6713        0.098831          0.1253
v  total_pressure           99924      1.0144e+05      1.0141e+05      1.0142e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4145          2.2918          1.1236          1.1762


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.019119          26.345         0.81746         0.64566


 TIME FOR THE TIME STEP              204:        0.67069E+02

===============================================================


 INSTANT    0.184300000E-01   TIME STEP NUMBER             205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.421666155E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874847E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69277E+02 0.80768E+01
   Friction velocity        uet   :  0.29738E-02 0.47420E+01
   Friction velocity        uk    :  0.11185E-01 0.17958E+01
   Dimensionless distance   yplus :  0.13369E+00 0.47087E+02
   Friction thermal sca.    tstar : -0.37319E+03 0.41187E+02
   Rough dim-less th. sca.  tplus :  0.99751E-01 0.13130E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     142140
   Nb of faces within the viscous sub-layer     :       6558
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20498E+00      28   0.21018E-01   0.28077E+02 0.11931E+03 
c  Velocity[X]                                      0.25013E+02 
c  Velocity[Y]                                      0.75272E+00 
c  Velocity[Z]                                      0.23113E+01 
c  Pressure     0.11843E-03     192   0.63154E-02   0.18440E+00 0.20242E+03 
c  k            0.60047E-02      20   0.91190E-03   0.37453E+01 0.82665E+03 
c  omega        0.13985E+03      37   0.12419E-03   0.55609E+09 0.55979E+03 
c  TempC        0.31269E+04      50   0.21857E-01   0.12281E+06 0.25624E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8593          49.505          3.8889          3.9505
v  Velocity[Y]            -6.1952          7.1179      0.00071963      0.00085587
v  Velocity[Z]            -20.564           18.04        -0.21117       -0.092362
v  ǁVelocityǁ            0.011577          49.544          4.1801           4.044
v  Pressure               -1405.4          109.19          87.574          95.253
v  k                   3.1934e-08          10.492        0.082826        0.070335
v  omega               2.6006e-07      5.8455e+05          4646.6          1385.9
v  TempC                  -132.95          600.27          39.932          41.659
v  Density                0.40383          2.4654          1.1944          1.2128
v  TurbVisc            1.8798e-13       0.0022906      0.00010082      0.00014963
v  CourantNb                    0          27.915         0.71892         0.52072
v  FourierNb            0.0024862          4.6713        0.099366         0.12601
v  total_pressure           99920      1.0143e+05      1.0141e+05      1.0142e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41556          2.3479          1.1233          1.1758


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017565          28.034         0.81828         0.64673


 TIME FOR THE TIME STEP              205:        0.67112E+02

===============================================================


 INSTANT    0.185300000E-01   TIME STEP NUMBER             206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.185973686E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873704E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71545E+02 0.82861E+01
   Friction velocity        uet   :  0.45503E-02 0.48314E+01
   Friction velocity        uk    :  0.17493E-01 0.17930E+01
   Dimensionless distance   yplus :  0.23998E+00 0.46893E+02
   Friction thermal sca.    tstar : -0.28180E+03 0.39275E+02
   Rough dim-less th. sca.  tplus :  0.17905E+00 0.13120E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     142072
   Nb of faces within the viscous sub-layer     :       6588
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20502E+00      27   0.19485E-01   0.28216E+02 0.11948E+03 
c  Velocity[X]                                      0.25111E+02 
c  Velocity[Y]                                      0.74987E+00 
c  Velocity[Z]                                      0.23547E+01 
c  Pressure     0.11943E-03     196   0.63387E-02   0.18602E+00 0.21224E+03 
c  k            0.60045E-02      20   0.91854E-03   0.37596E+01 0.82686E+03 
c  omega        0.13962E+03      36   0.11584E-03   0.42569E+09 0.48955E+03 
c  TempC        0.31341E+04      51   0.21328E-01   0.12379E+06 0.25656E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8857          49.454          3.8905          3.9531
v  Velocity[Y]             -6.155          7.1753      0.00075262      0.00086272
v  Velocity[Z]            -20.592          18.379        -0.21182       -0.092827
v  ǁVelocityǁ           0.0087266          49.514          4.1823           4.047
v  Pressure               -1416.2          107.21          85.516          93.253
v  k                   2.7306e-08          10.557         0.08309        0.070628
v  omega               7.1661e-07      5.8422e+05          4648.1          1385.5
v  TempC                  -134.95          597.14          40.124          41.884
v  Density                0.40437          2.5191           1.194          1.2124
v  TurbVisc            1.5611e-13       0.0022903      0.00010143      0.00015049
v  CourantNb                    0          28.021         0.71921         0.52108
v  FourierNb            0.0024865          4.6713         0.09992         0.12674
v  total_pressure           99909      1.0143e+05      1.0141e+05      1.0142e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41314          2.4067           1.123          1.1755


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013552          28.144         0.81913         0.64783


 TIME FOR THE TIME STEP              206:        0.66943E+02

===============================================================


 INSTANT    0.186300000E-01   TIME STEP NUMBER             207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.280304277E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873645E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69323E+02 0.81705E+01
   Friction velocity        uet   :  0.42665E-02 0.47188E+01
   Friction velocity        uk    :  0.14032E-01 0.18007E+01
   Dimensionless distance   yplus :  0.14122E+00 0.46884E+02
   Friction thermal sca.    tstar : -0.32537E+03 0.41813E+02
   Rough dim-less th. sca.  tplus :  0.10537E+00 0.13119E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141888
   Nb of faces within the viscous sub-layer     :       6619
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20508E+00      28   0.19752E-01   0.27841E+02 0.11856E+03 
c  Velocity[X]                                      0.24792E+02 
c  Velocity[Y]                                      0.74864E+00 
c  Velocity[Z]                                      0.23007E+01 
c  Pressure     0.11777E-03     199   0.61826E-02   0.18312E+00 0.23338E+03 
c  k            0.60088E-02      20   0.92771E-03   0.37779E+01 0.82751E+03 
c  omega        0.13977E+03      36   0.18722E-03   0.93744E+09 0.72491E+03 
c  TempC        0.31413E+04      50   0.21608E-01   0.12279E+06 0.25482E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0262          49.258          3.8923          3.9558
v  Velocity[Y]            -6.4551          7.1592       0.0007735      0.00087134
v  Velocity[Z]            -20.042          18.088        -0.21244       -0.093292
v  ǁVelocityǁ           0.0080809          49.306          4.1847          4.0501
v  Pressure               -1426.5             105          83.331          91.102
v  k                   2.3917e-08          10.695         0.08335         0.07092
v  omega               2.0018e-06      9.5262e+05          4649.9          1385.3
v  TempC                     -135             615          40.315           42.11
v  Density                0.40582          2.5556          1.1937           1.212
v  TurbVisc            1.3348e-13       0.0022902      0.00010203      0.00015134
v  CourantNb           3.0378e-08          26.309         0.71948         0.52145
v  FourierNb            0.0024867          4.6713         0.10046         0.12746
v  total_pressure           99898      1.0143e+05      1.0141e+05      1.0142e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41117          2.4629          1.1227          1.1752


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0090995          26.427         0.81994         0.64891


 TIME FOR THE TIME STEP              207:        0.66801E+02

===============================================================


 INSTANT    0.187300000E-01   TIME STEP NUMBER             208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.349238425E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876006E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71840E+02 0.82328E+01
   Friction velocity        uet   :  0.30091E-02 0.47035E+01
   Friction velocity        uk    :  0.10660E-01 0.18087E+01
   Dimensionless distance   yplus :  0.18785E+00 0.47093E+02
   Friction thermal sca.    tstar : -0.36986E+03 0.42076E+02
   Rough dim-less th. sca.  tplus :  0.14015E+00 0.13130E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141770
   Nb of faces within the viscous sub-layer     :       6664
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20513E+00      28   0.19952E-01   0.27765E+02 0.11828E+03 
c  Velocity[X]                                      0.24679E+02 
c  Velocity[Y]                                      0.73684E+00 
c  Velocity[Z]                                      0.23498E+01 
c  Pressure     0.11763E-03     210   0.63616E-02   0.18247E+00 0.27961E+03 
c  k            0.60180E-02      20   0.93849E-03   0.38033E+01 0.82887E+03 
c  omega        0.14068E+03      36   0.14700E-03   0.95637E+09 0.73118E+03 
c  TempC        0.31484E+04      51   0.21971E-01   0.12266E+06 0.25399E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8061          51.938           3.894          3.9584
v  Velocity[Y]            -6.3417          7.0875      0.00076853      0.00086773
v  Velocity[Z]            -20.089          18.399        -0.21305       -0.093758
v  ǁVelocityǁ            0.011527          51.944           4.187          4.0531
v  Pressure               -1430.3          102.55           80.82          88.589
v  k                   2.2571e-08          10.537        0.083593        0.071213
v  omega               2.8414e-06      8.2402e+05          4653.4          1385.1
v  TempC                  -118.68          620.56          40.507          42.335
v  Density                0.39766          2.5565          1.1933          1.2115
v  TurbVisc             1.169e-13         0.00229      0.00010263      0.00015218
v  CourantNb                    0          27.984         0.71975         0.52181
v  FourierNb            0.0024869          4.6713           0.101         0.12818
v  total_pressure           99895      1.0143e+05      1.0141e+05      1.0141e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40456          2.5008          1.1225          1.1748


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011124          28.103         0.82075         0.64999


 TIME FOR THE TIME STEP              208:        0.67983E+02

===============================================================


 INSTANT    0.188300000E-01   TIME STEP NUMBER             209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.366915921E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874536E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69199E+02 0.82491E+01
   Friction velocity        uet   :  0.18394E-02 0.48331E+01
   Friction velocity        uk    :  0.95477E-02 0.18010E+01
   Dimensionless distance   yplus :  0.12466E+00 0.47229E+02
   Friction thermal sca.    tstar : -0.35289E+03 0.41299E+02
   Rough dim-less th. sca.  tplus :  0.93012E-01 0.13137E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141621
   Nb of faces within the viscous sub-layer     :       6677
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20518E+00      28   0.20635E-01   0.27981E+02 0.11861E+03 
c  Velocity[X]                                      0.24828E+02 
c  Velocity[Y]                                      0.76153E+00 
c  Velocity[Z]                                      0.23910E+01 
c  Pressure     0.11789E-03     198   0.62656E-02   0.18253E+00 0.24321E+03 
c  k            0.60321E-02      20   0.93674E-03   0.37984E+01 0.82675E+03 
c  omega        0.14054E+03      38   0.13076E-03   0.72837E+09 0.63794E+03 
c  TempC        0.31554E+04      51   0.21552E-01   0.12443E+06 0.25514E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8502          50.736          3.8958           3.961
v  Velocity[Y]            -6.5907           7.058      0.00076161      0.00087091
v  Velocity[Z]            -19.795           18.13        -0.21365        -0.09422
v  ǁVelocityǁ             0.01213          50.782          4.1894          4.0562
v  Pressure               -1437.4          100.45          78.703          86.456
v  k                   2.1862e-08          10.646         0.08383         0.07151
v  omega               2.2822e-06      6.3611e+05          4654.4          1384.8
v  TempC                  -114.21           596.9          40.697          42.559
v  Density                0.39519          2.2865          1.1929          1.2111
v  TurbVisc            1.1031e-13       0.0022899      0.00010321        0.000153
v  CourantNb                    0          28.129         0.72005         0.52218
v  FourierNb            0.0024872          4.6713         0.10153         0.12888
v  total_pressure           99888      1.0143e+05       1.014e+05      1.0141e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39519          2.2865          1.1222          1.1745


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0089285          28.253         0.82159         0.65106


 TIME FOR THE TIME STEP              209:        0.67280E+02

===============================================================


 INSTANT    0.189300000E-01   TIME STEP NUMBER             210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.100302846E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875806E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71041E+02 0.83813E+01
   Friction velocity        uet   :  0.27204E-02 0.47966E+01
   Friction velocity        uk    :  0.14528E-01 0.18050E+01
   Dimensionless distance   yplus :  0.20758E+00 0.47457E+02
   Friction thermal sca.    tstar : -0.39911E+03 0.39441E+02
   Rough dim-less th. sca.  tplus :  0.15488E+00 0.13148E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141495
   Nb of faces within the viscous sub-layer     :       6712
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20523E+00      29   0.19706E-01   0.28425E+02 0.11943E+03 
c  Velocity[X]                                      0.25230E+02 
c  Velocity[Y]                                      0.75983E+00 
c  Velocity[Z]                                      0.24350E+01 
c  Pressure     0.11801E-03     210   0.63597E-02   0.18261E+00 0.28943E+03 
c  k            0.60487E-02      20   0.92510E-03   0.37680E+01 0.82179E+03 
c  omega        0.14044E+03      37   0.23294E-03   0.80009E+09 0.66791E+03 
c  TempC        0.31626E+04      52   0.21108E-01   0.12494E+06 0.25497E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7224          49.759          3.8975          3.9637
v  Velocity[Y]            -6.7118          7.0207      0.00075355      0.00087252
v  Velocity[Z]            -19.933          18.483        -0.21429         -0.0947
v  ǁVelocityǁ            0.010004          49.829          4.1916          4.0592
v  Pressure                 -1449          97.851          76.234          83.986
v  k                   2.2485e-08          10.741        0.084054         0.07181
v  omega               1.3407e-06      9.9794e+05          4656.3          1384.5
v  TempC                  -117.94          602.17          40.886          42.784
v  Density                0.40593          2.2221          1.1925          1.2107
v  TurbVisc            1.0685e-13       0.0022897      0.00010379      0.00015381
v  CourantNb                    0          26.641         0.72034         0.52255
v  FourierNb            0.0024875          4.6713         0.10206         0.12957
v  total_pressure           99876      1.0142e+05       1.014e+05      1.0141e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40967          2.2221          1.1219          1.1741


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0078747           26.76          0.8224         0.65212


 TIME FOR THE TIME STEP              210:        0.68479E+02

===============================================================


 INSTANT    0.190300000E-01   TIME STEP NUMBER             211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.357118024E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874354E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69137E+02 0.83551E+01
   Friction velocity        uet   :  0.29209E-02 0.47300E+01
   Friction velocity        uk    :  0.15858E-01 0.18160E+01
   Dimensionless distance   yplus :  0.17021E+00 0.47783E+02
   Friction thermal sca.    tstar : -0.24875E+03 0.38079E+02
   Rough dim-less th. sca.  tplus :  0.12700E+00 0.13165E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141344
   Nb of faces within the viscous sub-layer     :       6759
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20529E+00      28   0.21224E-01   0.28195E+02 0.11882E+03 
c  Velocity[X]                                      0.25062E+02 
c  Velocity[Y]                                      0.75466E+00 
c  Velocity[Z]                                      0.23779E+01 
c  Pressure     0.11779E-03     196   0.62218E-02   0.18174E+00 0.25860E+03 
c  k            0.60698E-02      20   0.91545E-03   0.37623E+01 0.81965E+03 
c  omega        0.14120E+03      36   0.16049E-03   0.63481E+09 0.59477E+03 
c  TempC        0.31700E+04      50   0.21416E-01   0.12369E+06 0.25302E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.788          49.525          3.8992          3.9663
v  Velocity[Y]            -6.7759          7.1425      0.00074915       0.0008746
v  Velocity[Z]            -19.527          18.262        -0.21491       -0.095176
v  ǁVelocityǁ           0.0065429           49.59          4.1939          4.0622
v  Pressure               -1450.4          95.586           74.08          81.834
v  k                   2.3468e-08            10.8        0.084266        0.072107
v  omega               4.0323e-07      5.8251e+05          4657.8          1384.2
v  TempC                  -121.44          583.58          41.074           43.01
v  Density                0.40349          2.2755          1.1921          1.2103
v  TurbVisc            1.0988e-13       0.0022901      0.00010439      0.00015464
v  CourantNb                    0           28.35         0.72062         0.52291
v  FourierNb            0.0024877          4.6713          0.1026         0.13028
v  total_pressure           99875      1.0142e+05       1.014e+05      1.0141e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41705          2.2755          1.1216          1.1738


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010331          28.469         0.82321         0.65319


 TIME FOR THE TIME STEP              211:        0.67050E+02

===============================================================


 INSTANT    0.191300000E-01   TIME STEP NUMBER             212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.328340200E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875386E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71378E+02 0.84205E+01
   Friction velocity        uet   :  0.19955E-02 0.48251E+01
   Friction velocity        uk    :  0.15790E-01 0.18162E+01
   Dimensionless distance   yplus :  0.14462E+00 0.47604E+02
   Friction thermal sca.    tstar : -0.25332E+03 0.37327E+02
   Rough dim-less th. sca.  tplus :  0.10790E+00 0.13156E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141261
   Nb of faces within the viscous sub-layer     :       6815
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20533E+00      28   0.20178E-01   0.28363E+02 0.11906E+03 
c  Velocity[X]                                      0.25261E+02 
c  Velocity[Y]                                      0.73802E+00 
c  Velocity[Z]                                      0.23646E+01 
c  Pressure     0.11781E-03     194   0.61220E-02   0.18164E+00 0.24665E+03 
c  k            0.60944E-02      20   0.90949E-03   0.37867E+01 0.82099E+03 
c  omega        0.14069E+03      37   0.35886E-03   0.14292E+10 0.88966E+03 
c  TempC        0.31774E+04      52   0.21181E-01   0.12244E+06 0.25106E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6859          49.856          3.9009          3.9689
v  Velocity[Y]            -7.0138          7.1816      0.00075867      0.00087991
v  Velocity[Z]            -19.735          18.538        -0.21547       -0.095646
v  ǁVelocityǁ           0.0089058          49.916          4.1962          4.0653
v  Pressure               -1459.5          93.932           72.06          79.831
v  k                   8.3691e-09          10.832        0.084459          0.0724
v  omega                2.811e-08       1.444e+06          4660.3            1384
v  TempC                  -124.97          591.65           41.26          43.235
v  Density                0.41224           2.328          1.1917          1.2098
v  TurbVisc            1.1468e-13       0.0022903        0.000105      0.00015548
v  CourantNb                    0           28.29         0.72089         0.52328
v  FourierNb             0.002488          4.6713         0.10315           0.131
v  total_pressure           99865      1.0142e+05       1.014e+05       1.014e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4123           2.328          1.1213          1.1734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011811          28.414         0.82403         0.65428


 TIME FOR THE TIME STEP              212:        0.66989E+02

===============================================================


 INSTANT    0.192300000E-01   TIME STEP NUMBER             213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.111129535E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873950E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68525E+02 0.83081E+01
   Friction velocity        uet   :  0.41947E-03 0.47818E+01
   Friction velocity        uk    :  0.19385E-01 0.18209E+01
   Dimensionless distance   yplus :  0.22740E+00 0.47536E+02
   Friction thermal sca.    tstar : -0.28126E+03 0.37010E+02
   Rough dim-less th. sca.  tplus :  0.16967E+00 0.13152E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141167
   Nb of faces within the viscous sub-layer     :       6859
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20538E+00      28   0.20655E-01   0.28045E+02 0.11826E+03 
c  Velocity[X]                                      0.24884E+02 
c  Velocity[Y]                                      0.75239E+00 
c  Velocity[Z]                                      0.24086E+01 
c  Pressure     0.11772E-03     196   0.62594E-02   0.18106E+00 0.25342E+03 
c  k            0.61242E-02      19   0.89949E-03   0.38230E+01 0.82365E+03 
c  omega        0.14573E+03      37   0.21607E-03   0.13995E+10 0.87952E+03 
c  TempC        0.31849E+04      51   0.21663E-01   0.12228E+06 0.25024E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7501          50.226          3.9026          3.9716
v  Velocity[Y]            -7.2579          7.1467      0.00076428      0.00088263
v  Velocity[Z]            -19.305          18.309        -0.21608       -0.096121
v  ǁVelocityǁ           0.0096031          50.281          4.1985          4.0683
v  Pressure               -1473.2          91.893          70.034          77.822
v  k                   1.7151e-08          10.899        0.084641        0.072693
v  omega               8.2983e-09      1.2598e+06            4663          1383.8
v  TempC                  -128.19          611.33          41.443           43.46
v  Density                 0.4084          2.3835          1.1913          1.2094
v  TurbVisc            4.3817e-14         0.00229      0.00010562      0.00015633
v  CourantNb                    0          26.567         0.72116         0.52364
v  FourierNb            0.0024882          4.6713          0.1037         0.13172
v  total_pressure           99852      1.0142e+05       1.014e+05       1.014e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41555          2.3835          1.1211          1.1731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013725          26.687         0.82486         0.65537


 TIME FOR THE TIME STEP              213:        0.67311E+02

===============================================================


 INSTANT    0.193300000E-01   TIME STEP NUMBER             214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.348093148E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874889E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69507E+02 0.83356E+01
   Friction velocity        uet   :  0.31279E-02 0.46777E+01
   Friction velocity        uk    :  0.90200E-02 0.18235E+01
   Dimensionless distance   yplus :  0.87139E-01 0.47746E+02
   Friction thermal sca.    tstar : -0.40894E+03 0.36473E+02
   Rough dim-less th. sca.  tplus :  0.65015E-01 0.13163E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     141011
   Nb of faces within the viscous sub-layer     :       6885
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20544E+00      28   0.20381E-01   0.27923E+02 0.11789E+03 
c  Velocity[X]                                      0.24778E+02 
c  Velocity[Y]                                      0.75976E+00 
c  Velocity[Z]                                      0.23858E+01 
c  Pressure     0.11778E-03     195   0.63261E-02   0.18089E+00 0.26983E+03 
c  k            0.61563E-02      20   0.89285E-03   0.38343E+01 0.82352E+03 
c  omega        0.14256E+03      36   0.15403E-03   0.64559E+09 0.59812E+03 
c  TempC        0.31925E+04      52   0.21361E-01   0.12329E+06 0.25061E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7037          49.391          3.9043          3.9742
v  Velocity[Y]            -7.7622          7.1635      0.00077554       0.0008884
v  Velocity[Z]            -19.546          18.703        -0.21666       -0.096603
v  ǁVelocityǁ           0.0092547          49.451          4.2007          4.0714
v  Pressure               -1479.1          89.845          67.917          75.738
v  k                   2.9886e-08          10.637        0.084817        0.072986
v  omega               5.9738e-09      6.5034e+05          4663.4          1383.4
v  TempC                  -130.32          610.92          41.624          43.685
v  Density                0.39931          2.4364           1.191           1.209
v  TurbVisc            8.1697e-14       0.0022898      0.00010623      0.00015716
v  CourantNb                    0          28.345         0.72145         0.52401
v  FourierNb            0.0024885          4.6713         0.10424         0.13244
v  total_pressure           99846      1.0141e+05      1.0139e+05       1.014e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41806          2.4364          1.1208          1.1728


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015748          28.466         0.82569         0.65645


 TIME FOR THE TIME STEP              214:        0.66984E+02

===============================================================


 INSTANT    0.194300000E-01   TIME STEP NUMBER             215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.542653365E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874247E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69271E+02 0.84312E+01
   Friction velocity        uet   :  0.43137E-02 0.47899E+01
   Friction velocity        uk    :  0.14012E-01 0.18080E+01
   Dimensionless distance   yplus :  0.15456E+00 0.48009E+02
   Friction thermal sca.    tstar : -0.36190E+03 0.36246E+02
   Rough dim-less th. sca.  tplus :  0.11532E+00 0.13176E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     140868
   Nb of faces within the viscous sub-layer     :       6924
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20548E+00      28   0.20468E-01   0.28491E+02 0.11896E+03 
c  Velocity[X]                                      0.25241E+02 
c  Velocity[Y]                                      0.77376E+00 
c  Velocity[Z]                                      0.24758E+01 
c  Pressure     0.12013E-03     198   0.64101E-02   0.18436E+00 0.29183E+03 
c  k            0.61881E-02      20   0.89066E-03   0.38244E+01 0.82103E+03 
c  omega        0.14119E+03      37   0.14481E-03   0.57106E+09 0.56221E+03 
c  TempC        0.32002E+04      50   0.21387E-01   0.12346E+06 0.25013E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.728          49.096          3.9059          3.9768
v  Velocity[Y]            -7.9518          7.1656      0.00078009      0.00089344
v  Velocity[Z]            -19.172          18.096        -0.21723       -0.097082
v  ǁVelocityǁ            0.010053          49.149           4.203          4.0744
v  Pressure               -1487.1          87.664          65.727          73.546
v  k                   3.2914e-08          10.758        0.084998         0.07328
v  omega               7.2941e-09      5.8303e+05          4665.1          1383.2
v  TempC                  -109.35          589.65            41.8           43.91
v  Density                 0.3995          2.4727          1.1906          1.2086
v  TurbVisc            1.4591e-13       0.0022897      0.00010685      0.00015799
v  CourantNb                    0          27.976         0.72172         0.52438
v  FourierNb            0.0024887          4.6713         0.10479         0.13315
v  total_pressure           99838      1.0141e+05      1.0139e+05       1.014e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41646          2.4727          1.1205          1.1724


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016578          28.101         0.82651         0.65753


 TIME FOR THE TIME STEP              215:        0.67093E+02

===============================================================


 INSTANT    0.195300000E-01   TIME STEP NUMBER             216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.132983169E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155876195E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68380E+02 0.84783E+01
   Friction velocity        uet   :  0.47217E-02 0.47219E+01
   Friction velocity        uk    :  0.15026E-01 0.18130E+01
   Dimensionless distance   yplus :  0.17301E+00 0.47812E+02
   Friction thermal sca.    tstar : -0.41852E+03 0.35518E+02
   Rough dim-less th. sca.  tplus :  0.12908E+00 0.13166E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     140770
   Nb of faces within the viscous sub-layer     :       6965
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20554E+00      29   0.20738E-01   0.28118E+02 0.11805E+03 
c  Velocity[X]                                      0.24946E+02 
c  Velocity[Y]                                      0.77797E+00 
c  Velocity[Z]                                      0.23937E+01 
c  Pressure     0.11918E-03     195   0.62419E-02   0.18248E+00 0.29220E+03 
c  k            0.62153E-02      20   0.89789E-03   0.38182E+01 0.81897E+03 
c  omega        0.14121E+03      37   0.13946E-03   0.49102E+09 0.52093E+03 
c  TempC        0.32083E+04      51   0.21489E-01   0.12302E+06 0.24903E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7035          53.225          3.9075          3.9795
v  Velocity[Y]            -8.1615           7.122      0.00078585      0.00089355
v  Velocity[Z]            -19.217          18.732        -0.21781       -0.097564
v  ǁVelocityǁ            0.009725          53.233          4.2051          4.0775
v  Pressure               -1497.5          85.467          63.588          71.411
v  k                   3.6156e-08          10.894        0.085187        0.073573
v  omega               1.4165e-08      5.8274e+05          4666.5          1382.9
v  TempC                  -116.01          600.19          41.977          44.135
v  Density                0.40934          2.1562          1.1902          1.2081
v  TurbVisc            1.6067e-13       0.0022896      0.00010749      0.00015884
v  CourantNb           2.9988e-08          26.799         0.72198         0.52475
v  FourierNb             0.002489          4.6713         0.10535         0.13389
v  total_pressure           99827      1.0141e+05      1.0139e+05       1.014e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41915          2.1562          1.1203          1.1721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011201           26.92         0.82733         0.65863


 TIME FOR THE TIME STEP              216:        0.67183E+02

===============================================================


 INSTANT    0.196300000E-01   TIME STEP NUMBER             217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.253896979E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155875036E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69139E+02 0.84165E+01
   Friction velocity        uet   :  0.49765E-02 0.47558E+01
   Friction velocity        uk    :  0.11288E-01 0.18259E+01
   Dimensionless distance   yplus :  0.12089E+00 0.48195E+02
   Friction thermal sca.    tstar : -0.35148E+03 0.35067E+02
   Rough dim-less th. sca.  tplus :  0.90195E-01 0.13185E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     140613
   Nb of faces within the viscous sub-layer     :       7001
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20559E+00      29   0.21211E-01   0.28158E+02 0.11802E+03 
c  Velocity[X]                                      0.24974E+02 
c  Velocity[Y]                                      0.76379E+00 
c  Velocity[Z]                                      0.24195E+01 
c  Pressure     0.11923E-03     192   0.63441E-02   0.18268E+00 0.27740E+03 
c  k            0.62355E-02      20   0.90233E-03   0.38225E+01 0.81801E+03 
c  omega        0.14149E+03      37   0.13027E-03   0.62357E+09 0.58625E+03 
c  TempC        0.32163E+04      51   0.21645E-01   0.12382E+06 0.24920E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7193          50.714          3.9091          3.9821
v  Velocity[Y]            -8.3469          7.1767       0.0007925      0.00089424
v  Velocity[Z]            -18.801          18.365        -0.21836       -0.098039
v  ǁVelocityǁ           0.0090592           50.76          4.2073          4.0806
v  Pressure                 -1501          83.629          61.633          69.438
v  k                   2.5901e-08          10.877        0.085396        0.073868
v  omega               3.6151e-08      7.2978e+05          4668.5          1382.6
v  TempC                  -116.62          585.12          42.151           44.36
v  Density                 0.4044          2.2476          1.1898          1.2077
v  TurbVisc            1.7647e-13       0.0022896      0.00010812      0.00015968
v  CourantNb                    0          28.604         0.72226         0.52511
v  FourierNb            0.0024892          4.6713         0.10591          0.1346
v  total_pressure           99824      1.0141e+05      1.0139e+05      1.0139e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41501          2.2476            1.12          1.1718


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012583          28.725         0.82816         0.65971


 TIME FOR THE TIME STEP              217:        0.66940E+02

===============================================================


 INSTANT    0.197300000E-01   TIME STEP NUMBER             218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.192636507E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874225E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67227E+02 0.85350E+01
   Friction velocity        uet   :  0.55746E-02 0.48762E+01
   Friction velocity        uk    :  0.16500E-01 0.18218E+01
   Dimensionless distance   yplus :  0.17912E+00 0.48220E+02
   Friction thermal sca.    tstar : -0.42948E+03 0.34630E+02
   Rough dim-less th. sca.  tplus :  0.13364E+00 0.13186E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     140492
   Nb of faces within the viscous sub-layer     :       7056
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20564E+00      29   0.20074E-01   0.28468E+02 0.11855E+03 
c  Velocity[X]                                      0.25216E+02 
c  Velocity[Y]                                      0.76171E+00 
c  Velocity[Z]                                      0.24899E+01 
c  Pressure     0.11762E-03     195   0.60674E-02   0.17974E+00 0.30769E+03 
c  k            0.62436E-02      20   0.90330E-03   0.38343E+01 0.81783E+03 
c  omega        0.14179E+03      37   0.12755E-03   0.53122E+09 0.54068E+03 
c  TempC        0.32244E+04      52   0.20917E-01   0.12373E+06 0.24847E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7285          50.373          3.9107          3.9847
v  Velocity[Y]            -8.3435          7.1974      0.00083155      0.00090382
v  Velocity[Z]            -18.836           18.61         -0.2189       -0.098518
v  ǁVelocityǁ           0.0093262          50.428          4.2094          4.0836
v  Pressure               -1510.4          81.247          59.493          67.313
v  k                   9.4932e-09           10.92         0.08563        0.074164
v  omega               1.1696e-07      5.8252e+05          4670.6          1382.4
v  TempC                  -120.08           587.4          42.327          44.585
v  Density                0.41151          2.2563          1.1895          1.2073
v  TurbVisc            1.1164e-13       0.0022896      0.00010874      0.00016052
v  CourantNb                    0          28.584         0.72252         0.52547
v  FourierNb            0.0024895          4.6713         0.10645         0.13532
v  total_pressure           99815      1.0141e+05      1.0138e+05      1.0139e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41365          2.2563          1.1197          1.1714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0089171           28.71         0.82898         0.66079


 TIME FOR THE TIME STEP              218:        0.66915E+02

===============================================================


 INSTANT    0.198300000E-01   TIME STEP NUMBER             219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.205921333E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874383E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68176E+02 0.84225E+01
   Friction velocity        uet   :  0.18383E-02 0.47941E+01
   Friction velocity        uk    :  0.15717E-01 0.18290E+01
   Dimensionless distance   yplus :  0.16829E+00 0.48300E+02
   Friction thermal sca.    tstar : -0.43126E+03 0.34612E+02
   Rough dim-less th. sca.  tplus :  0.12556E+00 0.13190E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     140373
   Nb of faces within the viscous sub-layer     :       7092
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20570E+00      29   0.19932E-01   0.28160E+02 0.11778E+03 
c  Velocity[X]                                      0.24929E+02 
c  Velocity[Y]                                      0.78031E+00 
c  Velocity[Z]                                      0.24510E+01 
c  Pressure     0.11839E-03     191   0.59975E-02   0.18035E+00 0.29993E+03 
c  k            0.62402E-02      20   0.91304E-03   0.38440E+01 0.81747E+03 
c  omega        0.14187E+03      38   0.14883E-03   0.88294E+09 0.69568E+03 
c  TempC        0.32325E+04      51   0.21622E-01   0.12316E+06 0.24726E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7221          50.618          3.9123          3.9874
v  Velocity[Y]            -8.2345          7.1669       0.0008176      0.00090334
v  Velocity[Z]            -18.531          18.401        -0.21947       -0.099009
v  ǁVelocityǁ           0.0093936           50.68          4.2116          4.0867
v  Pressure               -1525.2           79.69          57.495            65.3
v  k                   4.6367e-08          10.841        0.085893        0.074457
v  omega               4.0662e-07      9.8417e+05          4672.8          1382.2
v  TempC                  -123.59          604.32          42.505          44.811
v  Density                0.41042          2.3073          1.1891          1.2069
v  TurbVisc             4.384e-14       0.0022895      0.00010938      0.00016138
v  CourantNb                    0          27.066         0.72279         0.52584
v  FourierNb            0.0024898          4.6713         0.10703         0.13606
v  total_pressure           99800       1.014e+05      1.0138e+05      1.0139e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41042          2.3073          1.1194          1.1711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0074474          27.187         0.82982          0.6619


 TIME FOR THE TIME STEP              219:        0.66955E+02

===============================================================


 INSTANT    0.199300000E-01   TIME STEP NUMBER             220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.128568473E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873569E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65523E+02 0.84933E+01
   Friction velocity        uet   :  0.16040E-02 0.47109E+01
   Friction velocity        uk    :  0.79189E-02 0.18215E+01
   Dimensionless distance   yplus :  0.13238E+00 0.48237E+02
   Friction thermal sca.    tstar : -0.44873E+03 0.35582E+02
   Rough dim-less th. sca.  tplus :  0.98773E-01 0.13187E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     140222
   Nb of faces within the viscous sub-layer     :       7129
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20576E+00      28   0.20544E-01   0.27913E+02 0.11715E+03 
c  Velocity[X]                                      0.24686E+02 
c  Velocity[Y]                                      0.76465E+00 
c  Velocity[Z]                                      0.24625E+01 
c  Pressure     0.11694E-03     176   0.61664E-02   0.17791E+00 0.24513E+03 
c  k            0.62283E-02      20   0.90830E-03   0.38401E+01 0.81572E+03 
c  omega        0.14264E+03      37   0.16819E-03   0.99270E+09 0.73680E+03 
c  TempC        0.32403E+04      52   0.22207E-01   0.12357E+06 0.24703E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8253          51.212          3.9139            3.99
v  Velocity[Y]            -7.4744          7.2263      0.00082222      0.00090685
v  Velocity[Z]            -18.593          18.914        -0.22003       -0.099502
v  ǁVelocityǁ           0.0099497          51.266          4.2138          4.0897
v  Pressure               -1527.3           78.05          55.865          63.695
v  k                   4.9877e-08          11.005        0.086178        0.074747
v  omega               1.6333e-06      9.6271e+05          4675.2            1382
v  TempC                  -126.83          589.68          42.687          45.036
v  Density                 0.4025          2.3615          1.1887          1.2064
v  TurbVisc             2.262e-13         0.00229      0.00011001      0.00016223
v  CourantNb                    0          28.858         0.72306         0.52621
v  FourierNb              0.00249          4.6713         0.10759         0.13679
v  total_pressure           99798       1.014e+05      1.0138e+05      1.0139e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4163          2.3615          1.1192          1.1707


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0075378          28.981         0.83065         0.66299


 TIME FOR THE TIME STEP              220:        0.65857E+02

===============================================================


 INSTANT    0.200300000E-01   TIME STEP NUMBER             221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.237518679E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872744E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66825E+02 0.85802E+01
   Friction velocity        uet   :  0.20923E-02 0.49165E+01
   Friction velocity        uk    :  0.14149E-01 0.18352E+01
   Dimensionless distance   yplus :  0.16881E+00 0.48357E+02
   Friction thermal sca.    tstar : -0.45696E+03 0.39866E+02
   Rough dim-less th. sca.  tplus :  0.12595E+00 0.13193E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     140053
   Nb of faces within the viscous sub-layer     :       7184
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20581E+00      29   0.20858E-01   0.28436E+02 0.11812E+03 
c  Velocity[X]                                      0.25184E+02 
c  Velocity[Y]                                      0.78157E+00 
c  Velocity[Z]                                      0.24706E+01 
c  Pressure     0.11792E-03     177   0.60941E-02   0.17920E+00 0.25160E+03 
c  k            0.62135E-02      20   0.89365E-03   0.38290E+01 0.81326E+03 
c  omega        0.14301E+03      37   0.34555E-03   0.32856E+10 0.13306E+04 
c  TempC        0.32476E+04      51   0.21681E-01   0.12462E+06 0.24745E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.794          50.541          3.9156          3.9926
v  Velocity[Y]            -8.0331          7.3351      0.00084879       0.0009132
v  Velocity[Z]            -18.295          18.468        -0.22056       -0.099996
v  ǁVelocityǁ            0.010885          50.599          4.2161          4.0928
v  Pressure               -1537.2          76.384          54.249          62.086
v  k                   5.3239e-08          11.248         0.08648        0.075038
v  omega               6.8568e-06       1.612e+06          4678.9            1382
v  TempC                  -129.03          584.52          42.872          45.261
v  Density                0.40933          2.4137          1.1883           1.206
v  TurbVisc            2.4329e-13       0.0022902      0.00011061      0.00016306
v  CourantNb                    0          28.334         0.72335         0.52658
v  FourierNb            0.0024903          4.6713         0.10813          0.1375
v  total_pressure           99788       1.014e+05      1.0138e+05      1.0139e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40933          2.4137          1.1189          1.1704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0088479           28.46         0.83148         0.66407


 TIME FOR THE TIME STEP              221:        0.66203E+02

===============================================================


 INSTANT    0.201300000E-01   TIME STEP NUMBER             222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.187173949E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873824E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64017E+02 0.86766E+01
   Friction velocity        uet   :  0.39742E-02 0.48277E+01
   Friction velocity        uk    :  0.93130E-02 0.18499E+01
   Dimensionless distance   yplus :  0.11196E+00 0.48472E+02
   Friction thermal sca.    tstar : -0.56721E+03 0.44695E+02
   Rough dim-less th. sca.  tplus :  0.83535E-01 0.13199E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     139951
   Nb of faces within the viscous sub-layer     :       7216
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         57 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20587E+00      30   0.20406E-01   0.28763E+02 0.11867E+03 
c  Velocity[X]                                      0.25454E+02 
c  Velocity[Y]                                      0.79415E+00 
c  Velocity[Z]                                      0.25150E+01 
c  Pressure     0.11925E-03     177   0.59974E-02   0.18115E+00 0.25667E+03 
c  k            0.61988E-02      20   0.88992E-03   0.38260E+01 0.81170E+03 
c  omega        0.16388E+03      37   0.15162E-03   0.10923E+10 0.77078E+03 
c  TempC        0.32548E+04      53   0.21577E-01   0.12410E+06 0.24631E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8249          51.201          3.9173          3.9953
v  Velocity[Y]            -8.1998          7.3504      0.00086504      0.00091544
v  Velocity[Z]            -18.391          18.684        -0.22115        -0.10051
v  ǁVelocityǁ            0.010116          51.264          4.2184          4.0958
v  Pressure               -1545.7          74.529          52.621          60.485
v  k                   5.6621e-08          11.039        0.086788        0.075329
v  omega               3.0973e-05      8.2136e+05          4679.7          1381.6
v  TempC                  -116.27          612.23           43.06          45.486
v  Density                0.41179          2.4506          1.1879          1.2056
v  TurbVisc            2.5965e-13         0.00229      0.00011122      0.00016389
v  CourantNb                    0          27.275         0.72364         0.52695
v  FourierNb            0.0024905          4.6713         0.10868         0.13821
v  total_pressure           99779       1.014e+05      1.0138e+05      1.0139e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41586          2.4506          1.1186          1.1701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0075118          27.397         0.83232         0.66516


 TIME FOR THE TIME STEP              222:        0.66481E+02

===============================================================


 INSTANT    0.202300000E-01   TIME STEP NUMBER             223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.122068538E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872287E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65133E+02 0.86979E+01
   Friction velocity        uet   :  0.31750E-02 0.47999E+01
   Friction velocity        uk    :  0.11942E-01 0.18370E+01
   Dimensionless distance   yplus :  0.17057E+00 0.48851E+02
   Friction thermal sca.    tstar : -0.72192E+03 0.34182E+02
   Rough dim-less th. sca.  tplus :  0.12727E+00 0.13217E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     139753
   Nb of faces within the viscous sub-layer     :       7246
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         55 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20593E+00      29   0.22415E-01   0.28675E+02 0.11837E+03 
c  Velocity[X]                                      0.25392E+02 
c  Velocity[Y]                                      0.78891E+00 
c  Velocity[Z]                                      0.24948E+01 
c  Pressure     0.12078E-03     176   0.61581E-02   0.18312E+00 0.25857E+03 
c  k            0.61893E-02      20   0.89725E-03   0.38533E+01 0.81344E+03 
c  omega        0.14453E+03      38   0.16074E-03   0.12232E+10 0.81487E+03 
c  TempC        0.32617E+04      51   0.20801E-01   0.12404E+06 0.24564E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7851          50.552          3.9191          3.9979
v  Velocity[Y]            -8.3846          7.3049      0.00084793      0.00091486
v  Velocity[Z]            -17.999          18.388        -0.22174        -0.10102
v  ǁVelocityǁ            0.013779          50.603          4.2208          4.0989
v  Pressure               -1547.2          73.046           51.05           58.91
v  k                   6.0073e-08          11.171        0.087091        0.075616
v  omega               0.00013896      1.3076e+06          4681.3          1381.3
v  TempC                  -114.92          618.59          43.251          45.711
v  Density                0.39891          2.2512          1.1875          1.2052
v  TurbVisc            2.7613e-13       0.0022901      0.00011182      0.00016475
v  CourantNb                    0          28.911         0.72396         0.52732
v  FourierNb            0.0024908          4.6713         0.10922         0.13893
v  total_pressure           99778       1.014e+05      1.0138e+05      1.0138e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39891          2.2512          1.1183          1.1697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0063758          29.033         0.83318         0.66625


 TIME FOR THE TIME STEP              223:        0.65675E+02

===============================================================


 INSTANT    0.203300000E-01   TIME STEP NUMBER             224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.139705882E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873762E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63042E+02 0.87861E+01
   Friction velocity        uet   :  0.44557E-02 0.48733E+01
   Friction velocity        uk    :  0.69315E-02 0.18438E+01
   Dimensionless distance   yplus :  0.11909E+00 0.48659E+02
   Friction thermal sca.    tstar : -0.12499E+04 0.34070E+02
   Rough dim-less th. sca.  tplus :  0.88858E-01 0.13208E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     139570
   Nb of faces within the viscous sub-layer     :       7272
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         61 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20598E+00      29   0.21194E-01   0.28992E+02 0.11890E+03 
c  Velocity[X]                                      0.25645E+02 
c  Velocity[Y]                                      0.78121E+00 
c  Velocity[Z]                                      0.25654E+01 
c  Pressure     0.11977E-03     191   0.61472E-02   0.18170E+00 0.32462E+03 
c  k            0.61859E-02      20   0.90743E-03   0.38735E+01 0.81448E+03 
c  omega        0.14453E+03      37   0.12674E-03   0.60640E+09 0.57427E+03 
c  TempC        0.32686E+04      53   0.20531E-01   0.12176E+06 0.24276E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7855          53.139           3.921          4.0005
v  Velocity[Y]            -8.4191           7.267      0.00087061         0.00092
v  Velocity[Z]            -17.996          18.943         -0.2223        -0.10153
v  ǁVelocityǁ            0.012828          53.146          4.2232           4.102
v  Pressure               -1554.9          71.088          49.117          56.989
v  k                   4.9358e-08          10.982        0.087375        0.075902
v  omega               0.00064733      6.7529e+05          4681.4            1381
v  TempC                  -120.22          609.12          43.442          45.936
v  Density                0.39606          2.2321          1.1871          1.2048
v  TurbVisc            2.9291e-13         0.00229      0.00011242      0.00016558
v  CourantNb                    0          28.783         0.72427         0.52769
v  FourierNb            0.0024911          4.6713         0.10976         0.13964
v  total_pressure           99770       1.014e+05      1.0137e+05      1.0138e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40966          2.2321          1.1181          1.1694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0087045          28.909         0.83403         0.66733


 TIME FOR THE TIME STEP              224:        0.67014E+02

===============================================================


 INSTANT    0.204300000E-01   TIME STEP NUMBER             225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.725520861E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872415E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63954E+02 0.88409E+01
   Friction velocity        uet   :  0.44037E-02 0.48365E+01
   Friction velocity        uk    :  0.46255E-02 0.18340E+01
   Dimensionless distance   yplus :  0.78769E-01 0.49015E+02
   Friction thermal sca.    tstar : -0.64243E+03 0.34392E+02
   Rough dim-less th. sca.  tplus :  0.58770E-01 0.13225E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     139472
   Nb of faces within the viscous sub-layer     :       7292
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         60 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20603E+00      29   0.20132E-01   0.28295E+02 0.11734E+03 
c  Velocity[X]                                      0.25008E+02 
c  Velocity[Y]                                      0.78190E+00 
c  Velocity[Z]                                      0.25057E+01 
c  Pressure     0.11760E-03     172   0.59974E-02   0.17802E+00 0.25435E+03 
c  k            0.61899E-02      20   0.92260E-03   0.38924E+01 0.81531E+03 
c  omega        0.14302E+03      38   0.12834E-03   0.77082E+09 0.64679E+03 
c  TempC        0.32755E+04      51   0.21616E-01   0.12224E+06 0.24263E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7533          51.804          3.9228          4.0032
v  Velocity[Y]            -8.4174          7.1845      0.00087381      0.00091931
v  Velocity[Z]            -17.868          18.566        -0.22288        -0.10204
v  ǁVelocityǁ            0.010469          51.865          4.2256          4.1051
v  Pressure                 -1571          69.846          47.657          55.525
v  k                   6.7229e-08          11.239        0.087646        0.076189
v  omega                0.0031591      5.8253e+05          4683.2          1380.8
v  TempC                  -126.56             613          43.633          46.161
v  Density                0.40031          2.3095          1.1867          1.2043
v  TurbVisc            3.0918e-13       0.0022899      0.00011302      0.00016643
v  CourantNb                    0          27.043         0.72459         0.52807
v  FourierNb            0.0024913          4.6713         0.11029         0.14035
v  total_pressure           99754      1.0139e+05      1.0137e+05      1.0138e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41701          2.3095          1.1178           1.169


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011001          27.165         0.83488         0.66841


 TIME FOR THE TIME STEP              225:        0.65702E+02

===============================================================


 INSTANT    0.205300000E-01   TIME STEP NUMBER             226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.272104488E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872080E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61501E+02 0.88025E+01
   Friction velocity        uet   :  0.10705E-02 0.47820E+01
   Friction velocity        uk    :  0.12788E-01 0.18508E+01
   Dimensionless distance   yplus :  0.21770E+00 0.48803E+02
   Friction thermal sca.    tstar : -0.50226E+03 0.34573E+02
   Rough dim-less th. sca.  tplus :  0.16243E+00 0.13215E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     139309
   Nb of faces within the viscous sub-layer     :       7356
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         69 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20609E+00      29   0.21052E-01   0.28203E+02 0.11703E+03 
c  Velocity[X]                                      0.24953E+02 
c  Velocity[Y]                                      0.79070E+00 
c  Velocity[Z]                                      0.24600E+01 
c  Pressure     0.11679E-03     177   0.62590E-02   0.17599E+00 0.29082E+03 
c  k            0.61984E-02      21   0.92115E-03   0.38664E+01 0.81122E+03 
c  omega        0.14317E+03      37   0.13650E-03   0.56711E+09 0.55446E+03 
c  TempC        0.32822E+04      53   0.21535E-01   0.12431E+06 0.24408E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7266          50.686          3.9246          4.0058
v  Velocity[Y]            -8.4327           7.243      0.00088904      0.00092471
v  Velocity[Z]            -17.935          19.036        -0.22344        -0.10256
v  ǁVelocityǁ            0.012706          50.756           4.228          4.1081
v  Pressure               -1578.2          67.916          45.994          53.892
v  k                   7.0967e-08          11.102        0.087904        0.076482
v  omega                 0.015707      5.8213e+05          4685.7          1380.6
v  TempC                   -143.7          601.75          43.824          46.385
v  Density                0.39856          2.4094          1.1863          1.2039
v  TurbVisc            3.2767e-13       0.0022898      0.00011358      0.00016722
v  CourantNb                    0          29.297         0.72491         0.52844
v  FourierNb            0.0024916          4.6713         0.11079         0.14102
v  total_pressure           99747      1.0139e+05      1.0137e+05      1.0138e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41803          2.2963          1.1175          1.1687


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013248          29.421          0.8357         0.66945


 TIME FOR THE TIME STEP              226:        0.65820E+02

===============================================================


 INSTANT    0.206300000E-01   TIME STEP NUMBER             227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.169464132E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873006E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62494E+02 0.88332E+01
   Friction velocity        uet   :  0.45831E-02 0.48661E+01
   Friction velocity        uk    :  0.15594E-01 0.18436E+01
   Dimensionless distance   yplus :  0.23488E+00 0.48834E+02
   Friction thermal sca.    tstar : -0.41446E+03 0.39567E+02
   Rough dim-less th. sca.  tplus :  0.17525E+00 0.13216E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     139255
   Nb of faces within the viscous sub-layer     :       7398
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         65 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20615E+00      30   0.21919E-01   0.28793E+02 0.11813E+03 
c  Velocity[X]                                      0.25456E+02 
c  Velocity[Y]                                      0.79412E+00 
c  Velocity[Z]                                      0.25436E+01 
c  Pressure     0.11844E-03     177   0.61706E-02   0.17796E+00 0.30834E+03 
c  k            0.62098E-02      20   0.91917E-03   0.38364E+01 0.80662E+03 
c  omega        0.14374E+03      38   0.57525E-03   0.95649E+10 0.22213E+04 
c  TempC        0.32891E+04      51   0.21044E-01   0.12445E+06 0.24363E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7129          50.718          3.9264          4.0085
v  Velocity[Y]            -8.7448          7.3302      0.00088997      0.00092927
v  Velocity[Z]             -17.48          18.686        -0.22402        -0.10308
v  ǁVelocityǁ            0.012965          50.774          4.2305          4.1112
v  Pressure               -1586.2          66.479          44.309          52.208
v  k                   1.9182e-08          11.118        0.088158        0.076779
v  omega                  0.32893      3.7844e+06          4690.5          1380.7
v  TempC                  -126.02           639.9          44.012           46.61
v  Density                0.40368          2.7283           1.186          1.2035
v  TurbVisc            3.4584e-13       0.0022902      0.00011415      0.00016802
v  CourantNb                    0          28.883         0.72522         0.52881
v  FourierNb            0.0024918          4.6713          0.1113         0.14169
v  total_pressure           99739      1.0139e+05      1.0137e+05      1.0138e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41453          2.3464          1.1172          1.1684


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015428          29.011         0.83652          0.6705


 TIME FOR THE TIME STEP              227:        0.66472E+02

===============================================================


 INSTANT    0.207300000E-01   TIME STEP NUMBER             228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.257243297E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155874011E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60464E+02 0.88202E+01
   Friction velocity        uet   :  0.31310E-02 0.48273E+01
   Friction velocity        uk    :  0.17876E-01 0.18426E+01
   Dimensionless distance   yplus :  0.18914E+00 0.49129E+02
   Friction thermal sca.    tstar : -0.33511E+03 0.34937E+02
   Rough dim-less th. sca.  tplus :  0.14112E+00 0.13231E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     139120
   Nb of faces within the viscous sub-layer     :       7465
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         66 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20620E+00      29   0.21609E-01   0.28982E+02 0.11839E+03 
c  Velocity[X]                                      0.25575E+02 
c  Velocity[Y]                                      0.82143E+00 
c  Velocity[Z]                                      0.25852E+01 
c  Pressure     0.12071E-03     177   0.62134E-02   0.18133E+00 0.32841E+03 
c  k            0.62218E-02      20   0.91780E-03   0.38296E+01 0.80454E+03 
c  omega        0.35450E+03      36   0.12017E-03   0.29421E+10 0.12515E+04 
c  TempC        0.32961E+04      52   0.20823E-01   0.12313E+06 0.24174E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6838          54.357          3.9283          4.0111
v  Velocity[Y]             -7.869          7.3542      0.00088384      0.00092605
v  Velocity[Z]            -17.521          18.717        -0.22462        -0.10361
v  ǁVelocityǁ            0.011276          54.366          4.2329          4.1143
v  Pressure               -1598.2          64.749          42.569          50.469
v  k                   3.7361e-08          11.376        0.088402        0.077073
v  omega                  0.39219      1.9169e+06          4692.9          1380.6
v  TempC                  -129.19          647.12          44.201          46.835
v  Density                0.38682          2.4004          1.1856          1.2031
v  TurbVisc            8.1817e-14       0.0022904      0.00011474      0.00016885
v  CourantNb                    0          27.188         0.72553         0.52918
v  FourierNb            0.0024921          4.6713         0.11182         0.14239
v  total_pressure           99727      1.0139e+05      1.0137e+05      1.0138e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41832          2.4004           1.117           1.168


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014848          27.311         0.83736         0.67157


 TIME FOR THE TIME STEP              228:        0.65956E+02

===============================================================


 INSTANT    0.208300000E-01   TIME STEP NUMBER             229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.363191271E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873492E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61267E+02 0.89219E+01
   Friction velocity        uet   :  0.17855E-02 0.48206E+01
   Friction velocity        uk    :  0.10855E-01 0.18648E+01
   Dimensionless distance   yplus :  0.10597E+00 0.49406E+02
   Friction thermal sca.    tstar : -0.32915E+03 0.35430E+02
   Rough dim-less th. sca.  tplus :  0.79064E-01 0.13244E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     139008
   Nb of faces within the viscous sub-layer     :       7512
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         68 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20626E+00      29   0.21952E-01   0.28757E+02 0.11781E+03 
c  Velocity[X]                                      0.25356E+02 
c  Velocity[Y]                                      0.81389E+00 
c  Velocity[Z]                                      0.25870E+01 
c  Pressure     0.11888E-03     160   0.61828E-02   0.17833E+00 0.26112E+03 
c  k            0.62365E-02      21   0.89703E-03   0.38341E+01 0.80383E+03 
c  omega        0.19567E+03      37   0.35975E-03   0.13780E+11 0.26308E+04 
c  TempC        0.33031E+04      51   0.20608E-01   0.12146E+06 0.23950E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6859          52.055          3.9301          4.0138
v  Velocity[Y]            -7.9644          7.4242      0.00090692      0.00093192
v  Velocity[Z]            -17.322          18.648        -0.22519        -0.10413
v  ǁVelocityǁ           0.0053789          52.114          4.2354          4.1174
v  Pressure               -1601.4          63.593          41.229          49.122
v  k                   3.4107e-08          11.343        0.088635        0.077364
v  omega                  0.35644      4.5417e+06          4699.4          1380.7
v  TempC                  -131.42          607.49          44.388           47.06
v  Density                0.38378          2.4533          1.1852          1.2026
v  TurbVisc            1.6712e-13       0.0022902      0.00011532      0.00016968
v  CourantNb                    0            29.3         0.72587         0.52956
v  FourierNb            0.0024923          4.6713         0.11234         0.14308
v  total_pressure           99724      1.0139e+05      1.0137e+05      1.0137e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41664          2.4533          1.1167          1.1677


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011562          29.424         0.83821         0.67264


 TIME FOR THE TIME STEP              229:        0.64516E+02

===============================================================


 INSTANT    0.209300000E-01   TIME STEP NUMBER             230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.258703770E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873458E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59257E+02 0.90039E+01
   Friction velocity        uet   :  0.15882E-02 0.49648E+01
   Friction velocity        uk    :  0.14371E-01 0.18594E+01
   Dimensionless distance   yplus :  0.19975E+00 0.49450E+02
   Friction thermal sca.    tstar : -0.32461E+03 0.35918E+02
   Rough dim-less th. sca.  tplus :  0.14904E+00 0.13246E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     138811
   Nb of faces within the viscous sub-layer     :       7583
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         68 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20631E+00      29   0.20257E-01   0.28624E+02 0.11742E+03 
c  Velocity[X]                                      0.25229E+02 
c  Velocity[Y]                                      0.81246E+00 
c  Velocity[Z]                                      0.25826E+01 
c  Pressure     0.11922E-03     176   0.60673E-02   0.17869E+00 0.30713E+03 
c  k            0.62525E-02      21   0.87998E-03   0.38527E+01 0.80468E+03 
c  omega        0.31874E+03      35   0.12951E-03   0.75133E+10 0.19711E+04 
c  TempC        0.33103E+04      53   0.20831E-01   0.12183E+06 0.23928E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7115          51.658          3.9319          4.0164
v  Velocity[Y]            -8.0692          7.4208      0.00095255      0.00094384
v  Velocity[Z]            -17.266          19.058        -0.22576        -0.10467
v  ǁVelocityǁ           0.0090404           51.72          4.2378          4.1205
v  Pressure               -1611.3          61.691          39.668           47.58
v  k                   2.6226e-08          11.361        0.088858        0.077653
v  omega                  0.07588      3.6022e+06          4702.2          1380.6
v  TempC                  -130.87          600.87          44.574          47.285
v  Density                0.40105          2.4919          1.1848          1.2022
v  TurbVisc            1.5253e-13         0.00229      0.00011591      0.00017051
v  CourantNb            4.229e-08          29.073         0.72619         0.52993
v  FourierNb            0.0024926          4.6713         0.11285         0.14378
v  total_pressure           99714      1.0139e+05      1.0136e+05      1.0137e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41314          2.4919          1.1164          1.1674


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01087          29.202         0.83904         0.67371


 TIME FOR THE TIME STEP              230:        0.66254E+02

===============================================================


 INSTANT    0.210300000E-01   TIME STEP NUMBER             231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.299321202E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871722E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59735E+02 0.90485E+01
   Friction velocity        uet   :  0.29312E-02 0.48625E+01
   Friction velocity        uk    :  0.15079E-01 0.18628E+01
   Dimensionless distance   yplus :  0.16548E+00 0.49949E+02
   Friction thermal sca.    tstar : -0.48204E+03 0.36695E+02
   Rough dim-less th. sca.  tplus :  0.12347E+00 0.13270E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     138672
   Nb of faces within the viscous sub-layer     :       7652
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         67 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20638E+00      29   0.20912E-01   0.28189E+02 0.11640E+03 
c  Velocity[X]                                      0.24850E+02 
c  Velocity[Y]                                      0.80013E+00 
c  Velocity[Z]                                      0.25382E+01 
c  Pressure     0.11729E-03     158   0.60000E-02   0.17540E+00 0.25786E+03 
c  k            0.62704E-02      20   0.87900E-03   0.38480E+01 0.80306E+03 
c  omega        0.19684E+03      37   0.13731E-03   0.24413E+10 0.11374E+04 
c  TempC        0.33173E+04      51   0.20479E-01   0.12248E+06 0.23934E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6604           51.78          3.9337           4.019
v  Velocity[Y]            -8.0637          7.3646      0.00096544      0.00094779
v  Velocity[Z]             -16.98          18.625        -0.22639        -0.10522
v  ǁVelocityǁ            0.010338          51.845          4.2402          4.1236
v  Pressure               -1626.2          60.531          38.429          46.319
v  k                   3.8801e-09          11.534         0.08908        0.077943
v  omega                 0.034641      1.8228e+06          4702.7          1380.3
v  TempC                  -134.23          603.32          44.759           47.51
v  Density                0.40409          2.4822          1.1844          1.2018
v  TurbVisc            1.2572e-13       0.0022898      0.00011651      0.00017135
v  CourantNb                    0          27.369         0.72651          0.5303
v  FourierNb            0.0024929          4.6713         0.11337         0.14448
v  total_pressure           99699      1.0139e+05      1.0136e+05      1.0137e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41779          2.3245          1.1162           1.167


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012948          27.493         0.83988         0.67478


 TIME FOR THE TIME STEP              231:        0.64672E+02

===============================================================


 INSTANT    0.211300000E-01   TIME STEP NUMBER             232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.327751202E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872373E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58064E+02 0.89135E+01
   Friction velocity        uet   :  0.29293E-02 0.47874E+01
   Friction velocity        uk    :  0.16645E-01 0.18727E+01
   Dimensionless distance   yplus :  0.17558E+00 0.49709E+02
   Friction thermal sca.    tstar : -0.32732E+03 0.37553E+02
   Rough dim-less th. sca.  tplus :  0.13100E+00 0.13259E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     138524
   Nb of faces within the viscous sub-layer     :       7709
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         72 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20643E+00      29   0.21550E-01   0.28344E+02 0.11660E+03 
c  Velocity[X]                                      0.24916E+02 
c  Velocity[Y]                                      0.79273E+00 
c  Velocity[Z]                                      0.26352E+01 
c  Pressure     0.11749E-03     173   0.60545E-02   0.17520E+00 0.29792E+03 
c  k            0.62871E-02      20   0.89586E-03   0.38483E+01 0.80195E+03 
c  omega        0.20687E+03      37   0.28531E-03   0.10676E+11 0.23261E+04 
c  TempC        0.33245E+04      53   0.20444E-01   0.12169E+06 0.23799E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6791          54.816          3.9354          4.0217
v  Velocity[Y]            -8.0129          7.2484      0.00096414       0.0009469
v  Velocity[Z]            -17.015          18.732        -0.22699        -0.10576
v  ǁVelocityǁ           0.0091498          54.821          4.2426          4.1267
v  Pressure               -1632.4          58.974          36.985          44.897
v  k                   5.3378e-08          11.336        0.089301        0.078232
v  omega                  0.47603      4.1151e+06          4706.3          1380.4
v  TempC                  -137.39          592.52          44.944          47.736
v  Density                0.40296          2.5423           1.184          1.2014
v  TurbVisc            3.0135e-14       0.0022898      0.00011711       0.0001722
v  CourantNb                    0          29.516         0.72684         0.53068
v  FourierNb            0.0024931          4.6713          0.1139         0.14519
v  total_pressure           99693      1.0138e+05      1.0136e+05      1.0137e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41979           2.238          1.1159          1.1667


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015355           29.64         0.84073         0.67587


 TIME FOR THE TIME STEP              232:        0.65772E+02

===============================================================


 INSTANT    0.212300000E-01   TIME STEP NUMBER             233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.196373666E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870467E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59166E+02 0.89877E+01
   Friction velocity        uet   :  0.39648E-02 0.49719E+01
   Friction velocity        uk    :  0.14185E-01 0.18616E+01
   Dimensionless distance   yplus :  0.19377E+00 0.49986E+02
   Friction thermal sca.    tstar : -0.33029E+03 0.38619E+02
   Rough dim-less th. sca.  tplus :  0.14457E+00 0.13272E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     138360
   Nb of faces within the viscous sub-layer     :       7746
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         72 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20649E+00      29   0.21467E-01   0.29076E+02 0.11798E+03 
c  Velocity[X]                                      0.25544E+02 
c  Velocity[Y]                                      0.82999E+00 
c  Velocity[Z]                                      0.27020E+01 
c  Pressure     0.12201E-03     171   0.62907E-02   0.18163E+00 0.29624E+03 
c  k            0.63043E-02      20   0.91599E-03   0.38523E+01 0.80118E+03 
c  omega        0.35556E+03      35   0.94169E-04   0.31683E+10 0.12903E+04 
c  TempC        0.33318E+04      52   0.20757E-01   0.12180E+06 0.23753E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6545          52.028          3.9372          4.0243
v  Velocity[Y]            -8.1395          7.2816      0.00093195      0.00094213
v  Velocity[Z]            -16.712          18.796        -0.22759        -0.10631
v  ǁVelocityǁ            0.010513          52.095           4.245          4.1298
v  Pressure               -1640.3          57.918           35.59          43.522
v  k                   1.7228e-08          11.404         0.08953        0.078521
v  omega                  0.73543       2.081e+06          4707.4          1380.1
v  TempC                  -140.47          608.26          45.126          47.961
v  Density                0.40799          2.6016          1.1836          1.2009
v  TurbVisc            2.4129e-13       0.0022897      0.00011772      0.00017305
v  CourantNb                    0          29.187         0.72716         0.53105
v  FourierNb            0.0024934          4.6713         0.11443         0.14589
v  total_pressure           99685      1.0138e+05      1.0136e+05      1.0137e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40799          2.3577          1.1156          1.1663


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014388          29.317         0.84159         0.67695


 TIME FOR THE TIME STEP              233:        0.65519E+02

===============================================================


 INSTANT    0.213300000E-01   TIME STEP NUMBER             234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.261401307E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871283E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57513E+02 0.90110E+01
   Friction velocity        uet   :  0.25160E-02 0.48778E+01
   Friction velocity        uk    :  0.96607E-02 0.18641E+01
   Dimensionless distance   yplus :  0.18533E+00 0.49777E+02
   Friction thermal sca.    tstar : -0.43132E+03 0.39545E+02
   Rough dim-less th. sca.  tplus :  0.13828E+00 0.13262E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     138209
   Nb of faces within the viscous sub-layer     :       7829
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         74 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20655E+00      29   0.22618E-01   0.28906E+02 0.11751E+03 
c  Velocity[X]                                      0.25392E+02 
c  Velocity[Y]                                      0.84427E+00 
c  Velocity[Z]                                      0.26694E+01 
c  Pressure     0.12033E-03     173   0.61727E-02   0.17884E+00 0.31071E+03 
c  k            0.63166E-02      21   0.92240E-03   0.38462E+01 0.79928E+03 
c  omega        0.16828E+03      37   0.13523E-03   0.17727E+10 0.96761E+03 
c  TempC        0.33391E+04      54   0.20660E-01   0.12264E+06 0.23778E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6578          52.338           3.939           4.027
v  Velocity[Y]             -8.691          7.1852       0.0009148      0.00093803
v  Velocity[Z]            -16.795          19.039        -0.22819        -0.10686
v  ǁVelocityǁ            0.008749          52.403          4.2475          4.1329
v  Pressure                 -1654          56.735          34.169          42.119
v  k                   4.5003e-08          11.575        0.089767        0.078813
v  omega                  0.63316      1.0796e+06          4710.9          1380.1
v  TempC                  -142.91          604.65          45.309          48.186
v  Density                 0.4007          2.6619          1.1832          1.2005
v  TurbVisc            1.3346e-13       0.0022897       0.0001183      0.00017387
v  CourantNb                    0          27.659         0.72748         0.53143
v  FourierNb            0.0024936          4.6713         0.11495         0.14658
v  total_pressure           99671      1.0138e+05      1.0136e+05      1.0137e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41592          2.3381          1.1153           1.166


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012458          27.784         0.84242         0.67801


 TIME FOR THE TIME STEP              234:        0.65871E+02

===============================================================


 INSTANT    0.214300000E-01   TIME STEP NUMBER             235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.137539300E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870987E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57927E+02 0.90482E+01
   Friction velocity        uet   :  0.32317E-02 0.47959E+01
   Friction velocity        uk    :  0.13483E-01 0.18790E+01
   Dimensionless distance   yplus :  0.19631E+00 0.50188E+02
   Friction thermal sca.    tstar : -0.42433E+03 0.41426E+02
   Rough dim-less th. sca.  tplus :  0.14647E+00 0.13281E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     138024
   Nb of faces within the viscous sub-layer     :       7880
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         75 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20660E+00      29   0.21085E-01   0.29156E+02 0.11790E+03 
c  Velocity[X]                                      0.25656E+02 
c  Velocity[Y]                                      0.83703E+00 
c  Velocity[Z]                                      0.26629E+01 
c  Pressure     0.12042E-03     159   0.61122E-02   0.17894E+00 0.29218E+03 
c  k            0.63239E-02      20   0.90479E-03   0.38160E+01 0.79478E+03 
c  omega        0.14819E+03      38   0.13141E-03   0.80562E+09 0.65330E+03 
c  TempC        0.33462E+04      51   0.21001E-01   0.12332E+06 0.23788E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6868          51.465          3.9408          4.0296
v  Velocity[Y]            -8.6782          7.1401      0.00091921      0.00093528
v  Velocity[Z]            -16.565           18.64        -0.22883        -0.10741
v  ǁVelocityǁ           0.0056449          51.551          4.2499           4.136
v  Pressure               -1658.3          55.102          32.884          40.835
v  k                    8.216e-09          11.442         0.09002        0.079107
v  omega                  0.19884      5.8297e+05          4712.3          1379.9
v  TempC                  -144.57          584.17          45.492           48.41
v  Density                0.40235          2.7118          1.1829          1.2001
v  TurbVisc            3.3745e-13       0.0022897       0.0001189      0.00017469
v  CourantNb                    0          29.659         0.72781          0.5318
v  FourierNb            0.0024939          4.6713         0.11547         0.14728
v  total_pressure           99667      1.0138e+05      1.0136e+05      1.0137e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40425          2.3911           1.115          1.1657


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011226          29.784         0.84329         0.67909


 TIME FOR THE TIME STEP              235:        0.65100E+02

===============================================================


 INSTANT    0.215300000E-01   TIME STEP NUMBER             236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.501465075E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872610E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56477E+02 0.90171E+01
   Friction velocity        uet   :  0.16150E-02 0.49180E+01
   Friction velocity        uk    :  0.12374E-01 0.18674E+01
   Dimensionless distance   yplus :  0.13993E+00 0.50118E+02
   Friction thermal sca.    tstar : -0.54571E+03 0.43617E+02
   Rough dim-less th. sca.  tplus :  0.10440E+00 0.13278E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     137844
   Nb of faces within the viscous sub-layer     :       7940
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         74 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20666E+00      30   0.21154E-01   0.28791E+02 0.11704E+03 
c  Velocity[X]                                      0.25295E+02 
c  Velocity[Y]                                      0.83704E+00 
c  Velocity[Z]                                      0.26588E+01 
c  Pressure     0.11880E-03     176   0.59820E-02   0.17596E+00 0.39730E+03 
c  k            0.63256E-02      21   0.89208E-03   0.37960E+01 0.79146E+03 
c  omega        0.14569E+03      37   0.22152E-03   0.55541E+10 0.16926E+04 
c  TempC        0.33534E+04      54   0.20695E-01   0.12352E+06 0.23751E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7027          54.427          3.9425          4.0323
v  Velocity[Y]            -8.7669          7.2054      0.00094684      0.00094329
v  Velocity[Z]            -16.426          19.048        -0.22943        -0.10798
v  ǁVelocityǁ           0.0088633          54.438          4.2523          4.1392
v  Pressure                 -1669          53.519          31.188          39.146
v  k                   4.8011e-08          11.495         0.09028        0.079399
v  omega                 0.059706       3.767e+06          4716.3          1379.9
v  TempC                  -143.88          598.02          45.677          48.636
v  Density                0.41196          2.7468          1.1825          1.1997
v  TurbVisc            4.5875e-13       0.0022901      0.00011951      0.00017553
v  CourantNb           3.4017e-08          29.109         0.72815         0.53218
v  FourierNb            0.0024941          4.6713         0.11601         0.14799
v  total_pressure           99656      1.0138e+05      1.0136e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41209           2.442          1.1147          1.1653


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011295          29.239         0.84416         0.68017


 TIME FOR THE TIME STEP              236:        0.66287E+02

===============================================================


 INSTANT    0.216300000E-01   TIME STEP NUMBER             237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.260064062E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872982E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57014E+02 0.91016E+01
   Friction velocity        uet   :  0.12954E-02 0.48935E+01
   Friction velocity        uk    :  0.11049E-01 0.18728E+01
   Dimensionless distance   yplus :  0.18155E+00 0.50379E+02
   Friction thermal sca.    tstar : -0.42998E+03 0.47673E+02
   Rough dim-less th. sca.  tplus :  0.13546E+00 0.13290E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     137706
   Nb of faces within the viscous sub-layer     :       7981
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         77 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20673E+00      29   0.21498E-01   0.28937E+02 0.11722E+03 
c  Velocity[X]                                      0.25424E+02 
c  Velocity[Y]                                      0.82496E+00 
c  Velocity[Z]                                      0.26885E+01 
c  Pressure     0.12015E-03     155   0.60243E-02   0.17745E+00 0.30509E+03 
c  k            0.63259E-02      20   0.88413E-03   0.38029E+01 0.79105E+03 
c  omega        0.21739E+03      37   0.11092E-03   0.17373E+10 0.95497E+03 
c  TempC        0.33605E+04      51   0.20556E-01   0.12195E+06 0.23543E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7021          53.549          3.9443          4.0349
v  Velocity[Y]            -8.8842          7.2937      0.00096341      0.00094757
v  Velocity[Z]            -16.321           18.87        -0.23007        -0.10855
v  ǁVelocityǁ            0.007941          53.638          4.2548          4.1423
v  Pressure               -1679.9          52.083          29.965          37.887
v  k                   7.5905e-08          11.697        0.090556        0.079689
v  omega                 0.060592      1.9087e+06          4717.2          1379.7
v  TempC                  -113.27          601.51          45.863          48.861
v  Density                0.40541          2.7321          1.1821          1.1993
v  TurbVisc            4.2549e-13       0.0022903       0.0001201      0.00017636
v  CourantNb                    0          27.535         0.72849         0.53256
v  FourierNb            0.0024944          4.6713         0.11654          0.1487
v  total_pressure           99645      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41428          2.4792          1.1145           1.165


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010227           27.66         0.84504         0.68126


 TIME FOR THE TIME STEP              237:        0.64491E+02

===============================================================


 INSTANT    0.217300000E-01   TIME STEP NUMBER             238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.671351003E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871914E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55158E+02 0.90598E+01
   Friction velocity        uet   :  0.20886E-02 0.49038E+01
   Friction velocity        uk    :  0.11963E-01 0.18847E+01
   Dimensionless distance   yplus :  0.15180E+00 0.50577E+02
   Friction thermal sca.    tstar : -0.43604E+03 0.52015E+02
   Rough dim-less th. sca.  tplus :  0.11326E+00 0.13300E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     137521
   Nb of faces within the viscous sub-layer     :       8045
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         83 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20679E+00      29   0.21723E-01   0.28728E+02 0.11667E+03 
c  Velocity[X]                                      0.25128E+02 
c  Velocity[Y]                                      0.85215E+00 
c  Velocity[Z]                                      0.27474E+01 
c  Pressure     0.11953E-03     158   0.59548E-02   0.17615E+00 0.28745E+03 
c  k            0.63255E-02      21   0.88698E-03   0.38336E+01 0.79317E+03 
c  omega        0.15193E+03      38   0.13794E-03   0.83575E+09 0.66323E+03 
c  TempC        0.33674E+04      54   0.20389E-01   0.12188E+06 0.23481E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6876          52.668          3.9461          4.0376
v  Velocity[Y]            -8.9547          7.4658      0.00097853      0.00095487
v  Velocity[Z]            -16.143          19.138        -0.23071        -0.10912
v  ǁVelocityǁ           0.0079971          52.765          4.2573          4.1454
v  Pressure               -1686.7          51.206          28.792          36.733
v  k                   3.3278e-08           11.48        0.090835        0.079977
v  omega                 0.059414      9.7725e+05          4719.7          1379.6
v  TempC                  -123.63          600.28          46.051          49.086
v  Density                 0.4038          2.2091          1.1817          1.1988
v  TurbVisc            3.6673e-13       0.0022901       0.0001207      0.00017719
v  CourantNb                    0          30.087         0.72885         0.53294
v  FourierNb            0.0024946          4.6713         0.11708          0.1494
v  total_pressure           99638      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41204          2.1912          1.1142          1.1646


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0083661          30.213         0.84593         0.68235


 TIME FOR THE TIME STEP              238:        0.64647E+02

===============================================================


 INSTANT    0.218300000E-01   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.353977800E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870298E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55747E+02 0.90955E+01
   Friction velocity        uet   :  0.47522E-02 0.49913E+01
   Friction velocity        uk    :  0.13258E-01 0.18720E+01
   Dimensionless distance   yplus :  0.16194E+00 0.50729E+02
   Friction thermal sca.    tstar : -0.44998E+03 0.58780E+02
   Rough dim-less th. sca.  tplus :  0.12082E+00 0.13307E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     137355
   Nb of faces within the viscous sub-layer     :       8110
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         78 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20685E+00      30   0.22373E-01   0.28908E+02 0.11692E+03 
c  Velocity[X]                                      0.25334E+02 
c  Velocity[Y]                                      0.85713E+00 
c  Velocity[Z]                                      0.27162E+01 
c  Pressure     0.12117E-03     158   0.61332E-02   0.17853E+00 0.29515E+03 
c  k            0.63272E-02      21   0.89197E-03   0.38360E+01 0.79230E+03 
c  omega        0.14805E+03      38   0.77302E-03   0.52452E+11 0.46540E+04 
c  TempC        0.33742E+04      52   0.20487E-01   0.12270E+06 0.23505E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7965           52.43          3.9479          4.0402
v  Velocity[Y]            -7.9547          7.4742      0.00099177      0.00095976
v  Velocity[Z]            -15.944          18.813         -0.2314         -0.1097
v  ǁVelocityǁ           0.0033971          52.542          4.2599          4.1486
v  Pressure               -1695.4          49.929          27.615          35.577
v  k                   3.8498e-08          11.674        0.091116        0.080266
v  omega                 0.094898       1.176e+07          4730.9          1380.1
v  TempC                  -118.96           600.6          46.239          49.311
v  Density                0.40436          2.3621          1.1813          1.1984
v  TurbVisc            1.8795e-13       0.0022901      0.00012129      0.00017802
v  CourantNb                    0          29.591         0.72921         0.53333
v  FourierNb            0.0024948          4.6713         0.11761          0.1501
v  total_pressure           99630      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40798          2.3621          1.1139          1.1643


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0091031          29.721         0.84681         0.68342


 TIME FOR THE TIME STEP              239:        0.65294E+02

===============================================================


 INSTANT    0.219300000E-01   TIME STEP NUMBER             240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.510739136E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871587E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54360E+02 0.92245E+01
   Friction velocity        uet   :  0.27378E-02 0.49091E+01
   Friction velocity        uk    :  0.10742E-01 0.18830E+01
   Dimensionless distance   yplus :  0.13391E+00 0.50494E+02
   Friction thermal sca.    tstar : -0.57462E+03 0.64436E+02
   Rough dim-less th. sca.  tplus :  0.99914E-01 0.13296E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     137213
   Nb of faces within the viscous sub-layer     :       8146
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         90 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20691E+00      30   0.22211E-01   0.29156E+02 0.11730E+03 
c  Velocity[X]                                      0.25570E+02 
c  Velocity[Y]                                      0.86380E+00 
c  Velocity[Z]                                      0.27220E+01 
c  Pressure     0.11951E-03     155   0.60446E-02   0.17572E+00 0.28356E+03 
c  k            0.63305E-02      21   0.90104E-03   0.38310E+01 0.79064E+03 
c  omega        0.16280E+04      32   0.42804E-04   0.16498E+11 0.28239E+04 
c  TempC        0.33810E+04      53   0.20258E-01   0.12310E+06 0.23489E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7083          56.415          3.9498          4.0429
v  Velocity[Y]            -7.8347          7.5813       0.0010208      0.00096552
v  Velocity[Z]            -16.047          19.051        -0.23203        -0.11027
v  ǁVelocityǁ           0.0047417          56.423          4.2624          4.1517
v  Pressure                 -1707          48.941          26.535          34.494
v  k                   2.3109e-08          11.461        0.091389        0.080555
v  omega               0.00099199      5.9033e+06          4731.1          1379.9
v  TempC                  -138.82          616.72          46.429          49.536
v  Density                0.40422          2.2906          1.1809           1.198
v  TurbVisc            1.8655e-13         0.00229      0.00012188      0.00017885
v  CourantNb                    0          27.949         0.72956         0.53371
v  FourierNb            0.0024951          4.6713         0.11814          0.1508
v  total_pressure           99618      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41764          2.2837          1.1136          1.1639


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011454          28.075          0.8477         0.68451


 TIME FOR THE TIME STEP              240:        0.64255E+02

===============================================================


 INSTANT    0.220300000E-01   TIME STEP NUMBER             241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.300271783E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870049E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54891E+02 0.91549E+01
   Friction velocity        uet   :  0.18987E-02 0.49284E+01
   Friction velocity        uk    :  0.14429E-01 0.18712E+01
   Dimensionless distance   yplus :  0.23148E+00 0.50903E+02
   Friction thermal sca.    tstar : -0.56157E+03 0.74754E+02
   Rough dim-less th. sca.  tplus :  0.17271E+00 0.13315E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     137016
   Nb of faces within the viscous sub-layer     :       8209
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         97 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20698E+00      30   0.23058E-01   0.29397E+02 0.11766E+03 
c  Velocity[X]                                      0.25769E+02 
c  Velocity[Y]                                      0.86167E+00 
c  Velocity[Z]                                      0.27662E+01 
c  Pressure     0.11972E-03     157   0.62024E-02   0.17556E+00 0.29829E+03 
c  k            0.63374E-02      21   0.90330E-03   0.38345E+01 0.78983E+03 
c  omega        0.45293E+03      36   0.96706E-04   0.56212E+10 0.16919E+04 
c  TempC        0.33878E+04      52   0.20563E-01   0.12255E+06 0.23382E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6842          53.511          3.9517          4.0456
v  Velocity[Y]            -7.4316          7.6629       0.0010166      0.00096422
v  Velocity[Z]            -15.913          18.724        -0.23273        -0.11086
v  ǁVelocityǁ           0.0081022          53.587          4.2651          4.1548
v  Pressure               -1711.9          47.726          25.407          33.383
v  k                   5.6381e-08          11.698        0.091659        0.080845
v  omega                 0.010149      2.9747e+06          4731.7          1379.7
v  TempC                  -124.45          594.86          46.619          49.761
v  Density                0.39689          2.6293          1.1805          1.1976
v  TurbVisc            8.3631e-14         0.00229      0.00012248      0.00017969
v  CourantNb                    0          30.196         0.72994          0.5341
v  FourierNb            0.0024953          4.6713         0.11867          0.1515
v  total_pressure           99613      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41515          2.3282          1.1133          1.1636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013664          30.322         0.84861          0.6856


 TIME FOR THE TIME STEP              241:        0.64492E+02

===============================================================


 INSTANT    0.221300000E-01   TIME STEP NUMBER             242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.694784609E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871553E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53601E+02 0.92937E+01
   Friction velocity        uet   :  0.28350E-02 0.50547E+01
   Friction velocity        uk    :  0.15072E-01 0.18868E+01
   Dimensionless distance   yplus :  0.20121E+00 0.50798E+02
   Friction thermal sca.    tstar : -0.58551E+03 0.87793E+02
   Rough dim-less th. sca.  tplus :  0.15013E+00 0.13310E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     136913
   Nb of faces within the viscous sub-layer     :       8265
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         94 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20703E+00      29   0.21564E-01   0.29536E+02 0.11782E+03 
c  Velocity[X]                                      0.25924E+02 
c  Velocity[Y]                                      0.85822E+00 
c  Velocity[Z]                                      0.27533E+01 
c  Pressure     0.12058E-03     172   0.59469E-02   0.17651E+00 0.37909E+03 
c  k            0.63464E-02      21   0.90343E-03   0.38459E+01 0.78981E+03 
c  omega        0.18625E+03      37   0.14781E-03   0.19278E+10 0.99950E+03 
c  TempC        0.33946E+04      53   0.20768E-01   0.12297E+06 0.23369E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8142          52.755          3.9535          4.0482
v  Velocity[Y]            -7.7093          7.5114       0.0010086      0.00096531
v  Velocity[Z]            -16.038          19.537        -0.23341        -0.11146
v  ǁVelocityǁ           0.0078042          52.847          4.2677           4.158
v  Pressure               -1721.6           46.48          24.009          32.011
v  k                     8.16e-08          11.619        0.091919        0.081135
v  omega                0.0074195      1.5097e+06          4732.8          1379.5
v  TempC                  -126.63          598.46          46.808          49.986
v  Density                0.40689          2.3752          1.1801          1.1971
v  TurbVisc            2.7312e-13       0.0022898      0.00012307      0.00018051
v  CourantNb                    0          29.919         0.73032         0.53449
v  FourierNb            0.0024955          4.6713         0.11919          0.1522
v  total_pressure           99603      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41301          2.3752          1.1131          1.1632


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013164          30.051         0.84951         0.68668


 TIME FOR THE TIME STEP              242:        0.65584E+02

===============================================================


 INSTANT    0.222300000E-01   TIME STEP NUMBER             243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.685581027E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869280E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53763E+02 0.93162E+01
   Friction velocity        uet   :  0.21105E-02 0.49287E+01
   Friction velocity        uk    :  0.14330E-01 0.18836E+01
   Dimensionless distance   yplus :  0.18805E+00 0.51238E+02
   Friction thermal sca.    tstar : -0.44144E+03 0.89680E+02
   Rough dim-less th. sca.  tplus :  0.14031E+00 0.13331E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     136726
   Nb of faces within the viscous sub-layer     :       8298
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for         93 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20710E+00      29   0.22537E-01   0.29008E+02 0.11664E+03 
c  Velocity[X]                                      0.25376E+02 
c  Velocity[Y]                                      0.84877E+00 
c  Velocity[Z]                                      0.27823E+01 
c  Pressure     0.11909E-03     136   0.59192E-02   0.17364E+00 0.24474E+03 
c  k            0.63575E-02      21   0.90332E-03   0.38386E+01 0.78780E+03 
c  omega        0.15020E+03      38   0.14976E-03   0.10284E+10 0.73110E+03 
c  TempC        0.34013E+04      52   0.20226E-01   0.12312E+06 0.23330E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7603          53.138          3.9554          4.0509
v  Velocity[Y]            -7.8765          7.4531       0.0010102      0.00096556
v  Velocity[Z]            -15.554          18.664        -0.23409        -0.11205
v  ǁVelocityǁ           0.0042803          53.238          4.2703          4.1612
v  Pressure                 -1733          45.676            23.2          31.154
v  k                    3.774e-08          11.766         0.09217        0.081428
v  omega                 0.074737      8.1999e+05          4733.8          1379.3
v  TempC                  -128.52          595.93          46.996          50.211
v  Density                0.40521          2.4104          1.1797          1.1967
v  TurbVisc            3.9519e-13       0.0022902      0.00012365      0.00018133
v  CourantNb                    0          28.005         0.73069         0.53487
v  FourierNb            0.0024958          4.6713         0.11972         0.15289
v  total_pressure           99592      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42338          2.4104          1.1128          1.1629


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0082208          28.131         0.85041         0.68776


 TIME FOR THE TIME STEP              243:        0.63485E+02

===============================================================


 INSTANT    0.223300000E-01   TIME STEP NUMBER             244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.105191902E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869048E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52144E+02 0.92951E+01
   Friction velocity        uet   :  0.92637E-03 0.48633E+01
   Friction velocity        uk    :  0.20276E-01 0.18912E+01
   Dimensionless distance   yplus :  0.21091E+00 0.51109E+02
   Friction thermal sca.    tstar : -0.40038E+03 0.81906E+02
   Rough dim-less th. sca.  tplus :  0.15736E+00 0.13325E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     136517
   Nb of faces within the viscous sub-layer     :       8334
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        100 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20716E+00      30   0.22869E-01   0.29283E+02 0.11707E+03 
c  Velocity[X]                                      0.25622E+02 
c  Velocity[Y]                                      0.85835E+00 
c  Velocity[Z]                                      0.28034E+01 
c  Pressure     0.12013E-03     153   0.59945E-02   0.17491E+00 0.26166E+03 
c  k            0.63690E-02      21   0.90849E-03   0.38222E+01 0.78490E+03 
c  omega        0.14750E+03      38   0.15224E-03   0.79044E+09 0.64087E+03 
c  TempC        0.34081E+04      54   0.19754E-01   0.12354E+06 0.23317E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.742          55.537          3.9573          4.0535
v  Velocity[Y]            -7.9934          7.4495       0.0010295      0.00096937
v  Velocity[Z]            -16.126          19.103        -0.23479        -0.11265
v  ǁVelocityǁ           0.0057555          55.545           4.273          4.1643
v  Pressure               -1737.3          44.602          22.264          30.255
v  k                   9.5456e-09          11.951        0.092413        0.081719
v  omega                  0.67869      5.8427e+05          4735.4          1379.2
v  TempC                  -126.53           597.6          47.184          50.436
v  Density                0.40639          2.4419          1.1793          1.1963
v  TurbVisc            3.7409e-13       0.0022905      0.00012424      0.00018216
v  CourantNb                    0           30.33         0.73108         0.53526
v  FourierNb             0.002496          4.6713         0.12024         0.15359
v  total_pressure           99588      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41725          2.4419          1.1125          1.1626


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0096889          30.458         0.85132         0.68885


 TIME FOR THE TIME STEP              244:        0.64767E+02

===============================================================


 INSTANT    0.224300000E-01   TIME STEP NUMBER             245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.233541264E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868458E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52775E+02 0.93250E+01
   Friction velocity        uet   :  0.37229E-02 0.49612E+01
   Friction velocity        uk    :  0.15303E-01 0.19061E+01
   Dimensionless distance   yplus :  0.16001E+00 0.51552E+02
   Friction thermal sca.    tstar : -0.41520E+03 0.93293E+02
   Rough dim-less th. sca.  tplus :  0.11939E+00 0.13345E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     136346
   Nb of faces within the viscous sub-layer     :       8382
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        111 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20721E+00      30   0.22215E-01   0.30048E+02 0.11847E+03 
c  Velocity[X]                                      0.26307E+02 
c  Velocity[Y]                                      0.88754E+00 
c  Velocity[Z]                                      0.28537E+01 
c  Pressure     0.12325E-03     157   0.60351E-02   0.17972E+00 0.33339E+03 
c  k            0.63837E-02      21   0.90578E-03   0.38133E+01 0.78283E+03 
c  omega        0.14740E+03      38   0.14055E-03   0.65296E+09 0.58210E+03 
c  TempC        0.34150E+04      53   0.19964E-01   0.12202E+06 0.23120E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7904          52.629          3.9592          4.0562
v  Velocity[Y]            -8.0402          7.3639       0.0010152      0.00097221
v  Velocity[Z]            -16.057           18.95        -0.23552        -0.11326
v  ǁVelocityǁ           0.0055808          52.746          4.2756          4.1675
v  Pressure               -1749.3          43.443          21.127          29.137
v  k                    3.851e-08          11.804        0.092652        0.082009
v  omega                  0.20642      5.8509e+05          4737.5          1379.1
v  TempC                   -115.4          591.87           47.37          50.661
v  Density                0.40561          2.4089          1.1789          1.1959
v  TurbVisc            1.1695e-13       0.0022903      0.00012483      0.00018297
v  CourantNb                    0          29.791         0.73144         0.53565
v  FourierNb            0.0024962          4.6713         0.12077         0.15428
v  total_pressure           99576      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41308          2.4089          1.1122          1.1622


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010975          29.923         0.85221         0.68993


 TIME FOR THE TIME STEP              245:        0.64991E+02

===============================================================


 INSTANT    0.225300000E-01   TIME STEP NUMBER             246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.275138456E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870861E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51494E+02 0.92851E+01
   Friction velocity        uet   :  0.27849E-02 0.48597E+01
   Friction velocity        uk    :  0.12607E-01 0.18940E+01
   Dimensionless distance   yplus :  0.14505E+00 0.51510E+02
   Friction thermal sca.    tstar : -0.33931E+03 0.76407E+02
   Rough dim-less th. sca.  tplus :  0.10822E+00 0.13343E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     136183
   Nb of faces within the viscous sub-layer     :       8403
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        116 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20728E+00      30   0.21840E-01   0.29138E+02 0.11654E+03 
c  Velocity[X]                                      0.25446E+02 
c  Velocity[Y]                                      0.85719E+00 
c  Velocity[Z]                                      0.28350E+01 
c  Pressure     0.12010E-03     154   0.60064E-02   0.17428E+00 0.34826E+03 
c  k            0.64000E-02      21   0.89342E-03   0.38321E+01 0.78372E+03 
c  omega        0.14752E+03      38   0.12504E-03   0.83316E+09 0.65663E+03 
c  TempC        0.34219E+04      55   0.20434E-01   0.12169E+06 0.23036E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7969          56.336           3.961          4.0589
v  Velocity[Y]            -8.2484          7.3248        0.001029      0.00097168
v  Velocity[Z]            -15.986          19.301        -0.23625        -0.11387
v  ǁVelocityǁ           0.0083141          56.348          4.2783          4.1707
v  Pressure               -1763.6          42.335          19.982          27.995
v  k                   9.9714e-09          11.949        0.092885        0.082298
v  omega                  0.11121      9.6135e+05          4739.1            1379
v  TempC                  -121.98          604.73          47.556          50.886
v  Density                0.40829          2.2388          1.1786          1.1954
v  TurbVisc            1.8032e-13       0.0022901      0.00012543      0.00018381
v  CourantNb                    0          28.041         0.73184         0.53604
v  FourierNb            0.0024964          4.6713          0.1213         0.15498
v  total_pressure           99561      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41532          2.2388          1.1119          1.1619


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0098458          28.168         0.85314         0.69102


 TIME FOR THE TIME STEP              246:        0.64856E+02

===============================================================


 INSTANT    0.226300000E-01   TIME STEP NUMBER             247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.822904253E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870230E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51531E+02 0.92686E+01
   Friction velocity        uet   :  0.22531E-02 0.48555E+01
   Friction velocity        uk    :  0.51945E-02 0.19074E+01
   Dimensionless distance   yplus :  0.59761E-01 0.51543E+02
   Friction thermal sca.    tstar : -0.38221E+03 0.52479E+02
   Rough dim-less th. sca.  tplus :  0.44588E-01 0.13345E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     136067
   Nb of faces within the viscous sub-layer     :       8423
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        122 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20735E+00      30   0.21721E-01   0.29313E+02 0.11677E+03 
c  Velocity[X]                                      0.25544E+02 
c  Velocity[Y]                                      0.89709E+00 
c  Velocity[Z]                                      0.28720E+01 
c  Pressure     0.12035E-03     151   0.60518E-02   0.17422E+00 0.31704E+03 
c  k            0.64190E-02      21   0.87768E-03   0.38450E+01 0.78398E+03 
c  omega        0.14876E+03      39   0.29679E-03   0.22218E+11 0.32148E+04 
c  TempC        0.34287E+04      52   0.20267E-01   0.12270E+06 0.23080E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8868          53.902          3.9629          4.0615
v  Velocity[Y]            -8.7477           7.394       0.0010527      0.00097464
v  Velocity[Z]             -16.04           19.13        -0.23701         -0.1145
v  ǁVelocityǁ           0.0075173          54.008           4.281          4.1739
v  Pressure               -1767.2           41.42          19.007          26.986
v  k                   3.9372e-09          11.952        0.093118        0.082587
v  omega                 0.080777      7.7408e+06          4745.1          1379.2
v  TempC                  -116.42          599.73           47.74          51.111
v  Density                0.40231          2.3363          1.1782           1.195
v  TurbVisc            4.6677e-14       0.0022899      0.00012602      0.00018463
v  CourantNb                    0          30.349         0.73223         0.53643
v  FourierNb            0.0024966          4.6713         0.12182         0.15568
v  total_pressure           99558      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41178          2.3363          1.1116          1.1615


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0097102          30.477         0.85405         0.69211


 TIME FOR THE TIME STEP              247:        0.64892E+02

===============================================================


 INSTANT    0.227300000E-01   TIME STEP NUMBER             248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.434145062E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868771E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50302E+02 0.94093E+01
   Friction velocity        uet   :  0.30650E-02 0.50731E+01
   Friction velocity        uk    :  0.13460E-01 0.19054E+01
   Dimensionless distance   yplus :  0.13461E+00 0.51419E+02
   Friction thermal sca.    tstar : -0.53665E+03 0.47665E+02
   Rough dim-less th. sca.  tplus :  0.10044E+00 0.13339E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135935
   Nb of faces within the viscous sub-layer     :       8454
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        129 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20742E+00      30   0.23018E-01   0.29378E+02 0.11678E+03 
c  Velocity[X]                                      0.25651E+02 
c  Velocity[Y]                                      0.86433E+00 
c  Velocity[Z]                                      0.28629E+01 
c  Pressure     0.11930E-03     153   0.58704E-02   0.17219E+00 0.28986E+03 
c  k            0.64382E-02      21   0.87580E-03   0.38530E+01 0.78375E+03 
c  omega        0.70340E+03      34   0.38346E-04   0.59459E+10 0.17275E+04 
c  TempC        0.34357E+04      54   0.20033E-01   0.12235E+06 0.22996E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8594          53.195          3.9647          4.0642
v  Velocity[Y]            -8.7425          7.3587       0.0010775      0.00098147
v  Velocity[Z]            -15.898          19.348        -0.23775        -0.11512
v  ǁVelocityǁ           0.0070367          53.321          4.2836          4.1771
v  Pressure               -1780.2          40.562          18.088          26.086
v  k                    3.382e-08          12.095        0.093345        0.082875
v  omega                  0.21914      3.8941e+06          4744.9            1379
v  TempC                  -124.39          599.73          47.923          51.335
v  Density                0.40462          2.2535          1.1778          1.1946
v  TurbVisc            1.8425e-14       0.0022898      0.00012662      0.00018546
v  CourantNb                    0          30.038         0.73262         0.53683
v  FourierNb            0.0024969          4.6713         0.12235         0.15638
v  total_pressure           99545      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41863          2.2535          1.1113          1.1612


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013373          30.171         0.85497         0.69321


 TIME FOR THE TIME STEP              248:        0.64677E+02

===============================================================


 INSTANT    0.228300000E-01   TIME STEP NUMBER             249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.470234792E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867625E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50821E+02 0.94279E+01
   Friction velocity        uet   :  0.16733E-02 0.49316E+01
   Friction velocity        uk    :  0.73288E-02 0.19180E+01
   Dimensionless distance   yplus :  0.12468E+00 0.51772E+02
   Friction thermal sca.    tstar : -0.76394E+03 0.42072E+02
   Rough dim-less th. sca.  tplus :  0.93025E-01 0.13355E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135818
   Nb of faces within the viscous sub-layer     :       8490
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        130 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20748E+00      30   0.22912E-01   0.29813E+02 0.11752E+03 
c  Velocity[X]                                      0.26090E+02 
c  Velocity[Y]                                      0.87413E+00 
c  Velocity[Z]                                      0.28483E+01 
c  Pressure     0.11927E-03     146   0.58938E-02   0.17184E+00 0.26524E+03 
c  k            0.64585E-02      21   0.88527E-03   0.38581E+01 0.78319E+03 
c  omega        0.23053E+03      37   0.11648E-03   0.39505E+10 0.14144E+04 
c  TempC        0.34428E+04      53   0.20406E-01   0.12197E+06 0.22909E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8224          54.169          3.9665          4.0668
v  Velocity[Y]            -8.8286          7.4483       0.0010812      0.00098806
v  Velocity[Z]            -16.492          18.982        -0.23858        -0.11576
v  ǁVelocityǁ           0.0090542          54.291          4.2864          4.1803
v  Pressure               -1795.3          39.801          17.295          25.283
v  k                   2.0772e-08          12.036        0.093576        0.083163
v  omega                  0.41925      1.9704e+06          4747.3          1378.9
v  TempC                  -116.46          587.72          48.106           51.56
v  Density                0.40462          2.3741          1.1774          1.1942
v  TurbVisc            1.5312e-13       0.0022897      0.00012723       0.0001863
v  CourantNb                    0           28.19         0.73301         0.53722
v  FourierNb            0.0024971          4.6713         0.12289         0.15709
v  total_pressure           99530      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41532          2.3741           1.111          1.1608


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011351          28.318          0.8559         0.69431


 TIME FOR THE TIME STEP              249:        0.64338E+02

===============================================================


 INSTANT    0.229300000E-01   TIME STEP NUMBER             250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.405439412E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867155E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50366E+02 0.95053E+01
   Friction velocity        uet   :  0.76079E-03 0.48836E+01
   Friction velocity        uk    :  0.11664E-01 0.19111E+01
   Dimensionless distance   yplus :  0.16330E+00 0.51636E+02
   Friction thermal sca.    tstar : -0.63485E+03 0.38772E+02
   Rough dim-less th. sca.  tplus :  0.12184E+00 0.13349E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135648
   Nb of faces within the viscous sub-layer     :       8498
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        137 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20754E+00      30   0.22549E-01   0.29573E+02 0.11692E+03 
c  Velocity[X]                                      0.25788E+02 
c  Velocity[Y]                                      0.89138E+00 
c  Velocity[Z]                                      0.28938E+01 
c  Pressure     0.12126E-03     154   0.60039E-02   0.17444E+00 0.31910E+03 
c  k            0.64755E-02      21   0.89003E-03   0.38594E+01 0.78222E+03 
c  omega        0.17115E+03      38   0.15296E-03   0.44076E+10 0.14912E+04 
c  TempC        0.34498E+04      55   0.20363E-01   0.12233E+06 0.22893E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8897          57.237          3.9684          4.0695
v  Velocity[Y]            -8.9163          7.4831       0.0010956      0.00098907
v  Velocity[Z]            -15.845          19.751        -0.23939        -0.11641
v  ǁVelocityǁ           0.0084776           57.24          4.2891          4.1835
v  Pressure               -1798.5          38.696          16.304           24.34
v  k                   1.4883e-08          12.057         0.09381        0.083451
v  omega                 0.066191      2.5574e+06          4749.3          1378.9
v  TempC                  -126.94          600.83          48.288          51.785
v  Density                0.41026           2.254           1.177          1.1938
v  TurbVisc            9.4402e-14       0.0022896      0.00012784      0.00018713
v  CourantNb                    0          30.701         0.73343         0.53761
v  FourierNb            0.0024973          4.6713         0.12342         0.15779
v  total_pressure           99526      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41367           2.254          1.1107          1.1605


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0092646           30.83         0.85685          0.6954


 TIME FOR THE TIME STEP              250:        0.64924E+02

===============================================================


 INSTANT    0.230300000E-01   TIME STEP NUMBER             251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.198510391E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868370E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49859E+02 0.95165E+01
   Friction velocity        uet   :  0.15905E-02 0.50903E+01
   Friction velocity        uk    :  0.11013E-01 0.19167E+01
   Dimensionless distance   yplus :  0.17550E+00 0.52058E+02
   Friction thermal sca.    tstar : -0.61618E+03 0.43211E+02
   Rough dim-less th. sca.  tplus :  0.13094E+00 0.13369E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135577
   Nb of faces within the viscous sub-layer     :       8499
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        144 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20761E+00      30   0.22790E-01   0.29468E+02 0.11660E+03 
c  Velocity[X]                                      0.25634E+02 
c  Velocity[Y]                                      0.89005E+00 
c  Velocity[Z]                                      0.29443E+01 
c  Pressure     0.12106E-03     141   0.59130E-02   0.17376E+00 0.30377E+03 
c  k            0.64897E-02      21   0.88535E-03   0.38395E+01 0.77901E+03 
c  omega        0.18117E+03      38   0.28589E-03   0.86848E+10 0.20693E+04 
c  TempC        0.34569E+04      53   0.20371E-01   0.12301E+06 0.22906E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9133          54.415          3.9702          4.0722
v  Velocity[Y]            -8.0523          7.4531       0.0010881      0.00098923
v  Velocity[Z]            -16.189          19.441        -0.24023        -0.11706
v  ǁVelocityǁ           0.0065784          54.539          4.2918          4.1867
v  Pressure               -1811.1          37.628          15.416          23.456
v  k                    1.255e-08          12.095        0.094057        0.083743
v  omega                0.0027004      4.6859e+06          4751.6          1378.8
v  TempC                  -121.96          593.68          48.468          52.009
v  Density                0.40411          2.4156          1.1766          1.1933
v  TurbVisc            6.6054e-14       0.0022896      0.00012844      0.00018795
v  CourantNb                    0          30.223         0.73384         0.53801
v  FourierNb            0.0024975          4.6713         0.12395         0.15849
v  total_pressure           99514      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4194          2.4156          1.1104          1.1601


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0071741          30.357          0.8578          0.6965


 TIME FOR THE TIME STEP              251:        0.63838E+02

===============================================================


 INSTANT    0.231300000E-01   TIME STEP NUMBER             252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.147407550E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870217E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50619E+02 0.94360E+01
   Friction velocity        uet   :  0.20973E-02 0.50147E+01
   Friction velocity        uk    :  0.83687E-02 0.19172E+01
   Dimensionless distance   yplus :  0.14673E+00 0.51826E+02
   Friction thermal sca.    tstar : -0.44683E+03 0.50779E+02
   Rough dim-less th. sca.  tplus :  0.10948E+00 0.13358E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135391
   Nb of faces within the viscous sub-layer     :       8525
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        155 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20768E+00      31   0.24236E-01   0.29832E+02 0.11719E+03 
c  Velocity[X]                                      0.25992E+02 
c  Velocity[Y]                                      0.87148E+00 
c  Velocity[Z]                                      0.29691E+01 
c  Pressure     0.12118E-03     153   0.58303E-02   0.17354E+00 0.35766E+03 
c  k            0.64984E-02      21   0.88299E-03   0.38124E+01 0.77506E+03 
c  omega        0.27718E+03      36   0.21032E-03   0.75354E+10 0.19321E+04 
c  TempC        0.34641E+04      54   0.19968E-01   0.12321E+06 0.22875E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9422          54.768          3.9721          4.0748
v  Velocity[Y]            -7.4475          7.4004       0.0011035      0.00098941
v  Velocity[Z]            -16.181          19.462         -0.2411        -0.11772
v  ǁVelocityǁ           0.0065342          54.891          4.2946            4.19
v  Pressure               -1828.5          36.697          14.403           22.44
v  k                   2.4081e-08          12.114        0.094316        0.084036
v  omega                0.0015057      2.9313e+06            4752          1378.7
v  TempC                  -125.81          607.67           48.65          52.234
v  Density                0.40744          2.3361          1.1762          1.1929
v  TurbVisc            5.5669e-14       0.0022901      0.00012904      0.00018877
v  CourantNb                    0          28.576         0.73425         0.53841
v  FourierNb            0.0024977          4.6713         0.12449         0.15919
v  total_pressure           99497      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41318          2.3361          1.1101          1.1598


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.007185          28.705         0.85873          0.6976


 TIME FOR THE TIME STEP              252:        0.64503E+02

===============================================================


 INSTANT    0.232300000E-01   TIME STEP NUMBER             253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.488041168E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869011E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49067E+02 0.94952E+01
   Friction velocity        uet   :  0.35710E-02 0.49229E+01
   Friction velocity        uk    :  0.13132E-01 0.19210E+01
   Dimensionless distance   yplus :  0.17045E+00 0.52328E+02
   Friction thermal sca.    tstar : -0.31984E+03 0.65239E+02
   Rough dim-less th. sca.  tplus :  0.12717E+00 0.13381E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135297
   Nb of faces within the viscous sub-layer     :       8522
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        171 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20774E+00      31   0.22398E-01   0.30696E+02 0.11875E+03 
c  Velocity[X]                                      0.26734E+02 
c  Velocity[Y]                                      0.93277E+00 
c  Velocity[Z]                                      0.30289E+01 
c  Pressure     0.12491E-03     131   0.61771E-02   0.17909E+00 0.25353E+03 
c  k            0.65028E-02      21   0.88451E-03   0.38066E+01 0.77339E+03 
c  omega        0.23552E+03      38   0.13994E-03   0.30265E+10 0.12377E+04 
c  TempC        0.34712E+04      54   0.20027E-01   0.12162E+06 0.22677E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9539          54.303          3.9739          4.0775
v  Velocity[Y]            -7.4215          7.5091       0.0011118      0.00098999
v  Velocity[Z]            -16.173          19.418          -0.242        -0.11838
v  ǁVelocityǁ           0.0086119          54.423          4.2974          4.1932
v  Pressure               -1833.7          36.169          13.746          21.744
v  k                   1.5507e-08          12.364        0.094589        0.084326
v  omega               0.00016204      1.4889e+06          4751.1          1378.5
v  TempC                  -131.48          599.68          48.833          52.459
v  Density                0.40097          2.3971          1.1758          1.1925
v  TurbVisc            1.0943e-13       0.0022905      0.00012964      0.00018961
v  CourantNb                    0          30.855         0.73469         0.53881
v  FourierNb            0.0024979          4.6713         0.12503          0.1599
v  total_pressure           99491      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40979          2.3453          1.1098          1.1594


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0095091          30.985         0.85972         0.69871


 TIME FOR THE TIME STEP              253:        0.63511E+02

===============================================================


 INSTANT    0.233300000E-01   TIME STEP NUMBER             254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.260921502E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867097E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50419E+02 0.95330E+01
   Friction velocity        uet   :  0.43000E-02 0.50904E+01
   Friction velocity        uk    :  0.12862E-01 0.19368E+01
   Dimensionless distance   yplus :  0.13533E+00 0.52087E+02
   Friction thermal sca.    tstar : -0.31019E+03 0.11529E+03
   Rough dim-less th. sca.  tplus :  0.10097E+00 0.13370E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135205
   Nb of faces within the viscous sub-layer     :       8569
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        184 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20781E+00      31   0.21844E-01   0.29925E+02 0.11713E+03 
c  Velocity[X]                                      0.25972E+02 
c  Velocity[Y]                                      0.91051E+00 
c  Velocity[Z]                                      0.30421E+01 
c  Pressure     0.12108E-03     152   0.58619E-02   0.17310E+00 0.31820E+03 
c  k            0.65047E-02      22   0.87615E-03   0.38165E+01 0.77341E+03 
c  omega        0.15840E+03      39   0.14157E-03   0.11349E+10 0.76109E+03 
c  TempC        0.34783E+04      55   0.20261E-01   0.12133E+06 0.22600E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9512          57.467          3.9758          4.0802
v  Velocity[Y]            -7.0445          7.4453       0.0011229      0.00099008
v  Velocity[Z]            -16.004          19.835        -0.24291        -0.11906
v  ǁVelocityǁ           0.0053137          57.475          4.3002          4.1965
v  Pressure               -1842.3          35.515          12.874          20.884
v  k                   2.7091e-08          12.269        0.094868        0.084613
v  omega                1.919e-05       7.673e+05          4751.1          1378.3
v  TempC                  -134.78          620.43          49.018          52.684
v  Density                0.40464          2.4931          1.1755          1.1921
v  TurbVisc            1.2666e-13       0.0022903      0.00013025      0.00019045
v  CourantNb                    0          30.572         0.73512         0.53921
v  FourierNb            0.0024981          4.6713         0.12557         0.16061
v  total_pressure           99483      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40746          2.2622          1.1095           1.159


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011854          30.707         0.86069         0.69982


 TIME FOR THE TIME STEP              254:        0.65023E+02

===============================================================


 INSTANT    0.234300000E-01   TIME STEP NUMBER             255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.251229064E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867109E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48454E+02 0.96523E+01
   Friction velocity        uet   :  0.27172E-02 0.50831E+01
   Friction velocity        uk    :  0.11063E-01 0.19326E+01
   Dimensionless distance   yplus :  0.20258E+00 0.52707E+02
   Friction thermal sca.    tstar : -0.38444E+03 0.49869E+02
   Rough dim-less th. sca.  tplus :  0.15115E+00 0.13398E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     135066
   Nb of faces within the viscous sub-layer     :       8584
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        196 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20789E+00      30   0.23363E-01   0.29192E+02 0.11557E+03 
c  Velocity[X]                                      0.25300E+02 
c  Velocity[Y]                                      0.89680E+00 
c  Velocity[Z]                                      0.29950E+01 
c  Pressure     0.11949E-03     136   0.59123E-02   0.17015E+00 0.26598E+03 
c  k            0.65068E-02      21   0.86924E-03   0.38161E+01 0.77235E+03 
c  omega        0.15001E+03      40   0.14463E-03   0.84143E+09 0.65545E+03 
c  TempC        0.34851E+04      53   0.20131E-01   0.12208E+06 0.22621E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9023          56.107          3.9777          4.0828
v  Velocity[Y]            -7.4106          7.3336       0.0011305      0.00099186
v  Velocity[Z]            -16.334           19.41        -0.24387        -0.11974
v  ǁVelocityǁ           0.0068072          56.225          4.3031          4.1997
v  Pressure               -1856.8          34.819          12.166          20.179
v  k                    2.607e-08          12.502        0.095158        0.084902
v  omega               3.7397e-06      5.8352e+05          4751.9          1378.2
v  TempC                  -137.35          636.21          49.203          52.909
v  Density                0.39524          2.5525          1.1751          1.1916
v  TurbVisc            1.2302e-13       0.0022903      0.00013085      0.00019127
v  CourantNb                    0          28.686         0.73555         0.53961
v  FourierNb            0.0024982          4.6713          0.1261         0.16131
v  total_pressure           99468      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41378          2.3772          1.1092          1.1587


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014219          28.816         0.86164         0.70092


 TIME FOR THE TIME STEP              255:        0.63970E+02

===============================================================


 INSTANT    0.235300000E-01   TIME STEP NUMBER             256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.293320025E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867958E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50255E+02 0.96456E+01
   Friction velocity        uet   :  0.27761E-02 0.50420E+01
   Friction velocity        uk    :  0.15995E-01 0.19468E+01
   Dimensionless distance   yplus :  0.17706E+00 0.52738E+02
   Friction thermal sca.    tstar : -0.30834E+03 0.36985E+02
   Rough dim-less th. sca.  tplus :  0.13211E+00 0.13399E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134914
   Nb of faces within the viscous sub-layer     :       8598
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        194 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20795E+00      30   0.23158E-01   0.29832E+02 0.11670E+03 
c  Velocity[X]                                      0.25868E+02 
c  Velocity[Y]                                      0.91634E+00 
c  Velocity[Z]                                      0.30474E+01 
c  Pressure     0.12112E-03     150   0.58918E-02   0.17201E+00 0.31819E+03 
c  k            0.65090E-02      22   0.86816E-03   0.38019E+01 0.76985E+03 
c  omega        0.14959E+03      39   0.14736E-03   0.14907E+10 0.87035E+03 
c  TempC        0.34919E+04      54   0.20305E-01   0.12292E+06 0.22650E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9703          55.145          3.9796          4.0855
v  Velocity[Y]            -7.8425          7.4513       0.0011585       0.0009951
v  Velocity[Z]            -16.492          19.854        -0.24483        -0.12043
v  ǁVelocityǁ            0.002103          55.273          4.3059           4.203
v  Pressure               -1863.7           33.98          11.312          19.348
v  k                   1.0989e-08          12.343        0.095448        0.085193
v  omega                2.999e-07      1.2702e+06          4753.7          1378.1
v  TempC                  -139.36          610.81           49.39          53.134
v  Density                0.38839          2.6008          1.1747          1.1912
v  TurbVisc            1.7587e-13       0.0022902      0.00013143      0.00019209
v  CourantNb                    0          31.287         0.73597         0.54001
v  FourierNb            0.0024984          4.6713         0.12662           0.162
v  total_pressure           99461      1.0136e+05      1.0134e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41915          2.2689          1.1089          1.1583


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01665          31.417         0.86259         0.70201


 TIME FOR THE TIME STEP              256:        0.64383E+02

===============================================================


 INSTANT    0.236300000E-01   TIME STEP NUMBER             257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.877354810E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866760E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48649E+02 0.97988E+01
   Friction velocity        uet   :  0.23963E-02 0.51307E+01
   Friction velocity        uk    :  0.11850E-01 0.19385E+01
   Dimensionless distance   yplus :  0.16997E+00 0.52955E+02
   Friction thermal sca.    tstar : -0.34967E+03 0.31472E+02
   Rough dim-less th. sca.  tplus :  0.12681E+00 0.13409E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134810
   Nb of faces within the viscous sub-layer     :       8639
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        207 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20802E+00      31   0.24583E-01   0.30205E+02 0.11731E+03 
c  Velocity[X]                                      0.26226E+02 
c  Velocity[Y]                                      0.91102E+00 
c  Velocity[Z]                                      0.30684E+01 
c  Pressure     0.12185E-03     133   0.59556E-02   0.17270E+00 0.22991E+03 
c  k            0.65123E-02      22   0.87765E-03   0.37941E+01 0.76803E+03 
c  omega        0.15103E+03      40   0.14125E-03   0.12229E+10 0.78808E+03 
c  TempC        0.34986E+04      55   0.20172E-01   0.12229E+06 0.22543E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0207          54.744          3.9815          4.0882
v  Velocity[Y]            -8.1484          7.5126       0.0011492      0.00099207
v  Velocity[Z]            -16.319          19.419        -0.24581        -0.12111
v  ǁVelocityǁ           0.0039734          54.873          4.3089          4.2063
v  Pressure               -1874.8          33.386          10.738          18.769
v  k                   1.8634e-08          12.583        0.095735        0.085481
v  omega               2.1408e-05      8.3851e+05          4755.4          1378.1
v  TempC                  -138.61          586.28          49.578          53.359
v  Density                0.39954          2.6397          1.1743          1.1908
v  TurbVisc            4.8096e-14         0.00229      0.00013203      0.00019293
v  CourantNb                    0          30.914         0.73642         0.54042
v  FourierNb            0.0024986          4.6713         0.12715         0.16271
v  total_pressure           99450      1.0136e+05      1.0134e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41916          2.4138          1.1086           1.158


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.019137           31.05         0.86358         0.70312


 TIME FOR THE TIME STEP              257:        0.63441E+02

===============================================================


 INSTANT    0.237300000E-01   TIME STEP NUMBER             258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.114564793E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866160E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50773E+02 0.98358E+01
   Friction velocity        uet   :  0.28652E-02 0.50248E+01
   Friction velocity        uk    :  0.75385E-02 0.19538E+01
   Dimensionless distance   yplus :  0.13024E+00 0.52549E+02
   Friction thermal sca.    tstar : -0.40395E+03 0.31798E+02
   Rough dim-less th. sca.  tplus :  0.97172E-01 0.13391E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134696
   Nb of faces within the viscous sub-layer     :       8664
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        221 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20809E+00      31   0.23185E-01   0.30291E+02 0.11735E+03 
c  Velocity[X]                                      0.26256E+02 
c  Velocity[Y]                                      0.93488E+00 
c  Velocity[Z]                                      0.31002E+01 
c  Pressure     0.12379E-03     151   0.61045E-02   0.17530E+00 0.31590E+03 
c  k            0.65173E-02      22   0.88135E-03   0.37973E+01 0.76734E+03 
c  omega        0.15040E+03      40   0.13003E-03   0.67114E+09 0.58406E+03 
c  TempC        0.35053E+04      55   0.19993E-01   0.12185E+06 0.22454E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0586          57.845          3.9835          4.0909
v  Velocity[Y]            -8.3806          7.5078       0.0011466      0.00098926
v  Velocity[Z]            -16.318          19.834        -0.24681        -0.12181
v  ǁVelocityǁ           0.0030013          57.853          4.3119          4.2096
v  Pressure               -1891.4          32.645          9.9139          17.979
v  k                   1.3332e-08          12.488        0.096015        0.085769
v  omega                0.0014936      5.8351e+05          4756.1            1378
v  TempC                  -122.85           584.8          49.766          53.584
v  Density                0.41095           2.625          1.1739          1.1904
v  TurbVisc            8.0763e-14       0.0022898      0.00013261      0.00019375
v  CourantNb                    0          29.135         0.73687         0.54082
v  FourierNb            0.0024988          4.6713         0.12767         0.16339
v  total_pressure           99434      1.0136e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41513          2.2396          1.1083          1.1576


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018658          29.265         0.86453         0.70421


 TIME FOR THE TIME STEP              258:        0.64991E+02

===============================================================


 INSTANT    0.238300000E-01   TIME STEP NUMBER             259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.263713724E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866859E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49064E+02 0.98723E+01
   Friction velocity        uet   :  0.59448E-03 0.49367E+01
   Friction velocity        uk    :  0.59024E-02 0.19491E+01
   Dimensionless distance   yplus :  0.10193E+00 0.52891E+02
   Friction thermal sca.    tstar : -0.35648E+03 0.34061E+02
   Rough dim-less th. sca.  tplus :  0.76051E-01 0.13406E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134632
   Nb of faces within the viscous sub-layer     :       8687
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        230 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20816E+00      31   0.23952E-01   0.30025E+02 0.11671E+03 
c  Velocity[X]                                      0.25947E+02 
c  Velocity[Y]                                      0.94748E+00 
c  Velocity[Z]                                      0.31304E+01 
c  Pressure     0.12304E-03     146   0.59363E-02   0.17358E+00 0.31424E+03 
c  k            0.65262E-02      22   0.88032E-03   0.37964E+01 0.76617E+03 
c  omega        0.15014E+03      40   0.12699E-03   0.64917E+09 0.57401E+03 
c  TempC        0.35119E+04      54   0.20088E-01   0.12130E+06 0.22356E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1267          55.788          3.9855          4.0935
v  Velocity[Y]            -8.8812          7.5608       0.0011724      0.00099204
v  Velocity[Z]            -16.327          19.594        -0.24789        -0.12252
v  ǁVelocityǁ            0.002762          55.923          4.3149          4.2129
v  Pressure               -1896.1           31.94          9.1385          17.205
v  k                   3.0907e-08          12.613        0.096297         0.08606
v  omega                 0.012733      5.8464e+05          4757.3            1378
v  TempC                  -117.54          592.49          49.954          53.808
v  Density                0.41166          2.3499          1.1735            1.19
v  TurbVisc            1.1757e-13       0.0022901       0.0001332      0.00019457
v  CourantNb                    0          31.199         0.73735         0.54123
v  FourierNb             0.002499          4.6713         0.12819         0.16409
v  total_pressure           99429      1.0136e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41351          2.3499           1.108          1.1572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015353          31.331         0.86554         0.70532


 TIME FOR THE TIME STEP              259:        0.64498E+02

===============================================================


 INSTANT    0.239300000E-01   TIME STEP NUMBER             260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.101933295E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867022E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50967E+02 0.98482E+01
   Friction velocity        uet   :  0.17435E-02 0.51767E+01
   Friction velocity        uk    :  0.10225E-01 0.19551E+01
   Dimensionless distance   yplus :  0.96600E-01 0.52811E+02
   Friction thermal sca.    tstar : -0.48546E+03 0.36748E+02
   Rough dim-less th. sca.  tplus :  0.72075E-01 0.13403E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134550
   Nb of faces within the viscous sub-layer     :       8722
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        244 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20824E+00      30   0.25525E-01   0.30178E+02 0.11689E+03 
c  Velocity[X]                                      0.26115E+02 
c  Velocity[Y]                                      0.95008E+00 
c  Velocity[Z]                                      0.31132E+01 
c  Pressure     0.12344E-03     131   0.58973E-02   0.17367E+00 0.27919E+03 
c  k            0.65355E-02      22   0.87719E-03   0.37820E+01 0.76357E+03 
c  omega        0.15033E+03      40   0.15807E-03   0.12633E+10 0.79866E+03 
c  TempC        0.35185E+04      56   0.20180E-01   0.12253E+06 0.22421E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1168          56.073          3.9874          4.0962
v  Velocity[Y]            -8.9282          7.5654       0.0011998       0.0009955
v  Velocity[Z]            -16.245          19.726        -0.24893        -0.12324
v  ǁVelocityǁ           0.0078078           56.21          4.3179          4.2162
v  Pressure               -1907.9           31.07          8.4978          16.535
v  k                   6.3688e-09          12.632        0.096571        0.086352
v  omega                0.0047934      1.0402e+06            4761          1378.1
v  TempC                  -127.31          587.71          50.142          54.033
v  Density                  0.408          2.2697          1.1731          1.1895
v  TurbVisc            1.6078e-13       0.0022904      0.00013378      0.00019539
v  CourantNb                    0          31.021         0.73782         0.54164
v  FourierNb            0.0024991          4.6713          0.1287         0.16478
v  total_pressure           99417      1.0136e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41216          2.2697          1.1077          1.1569


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020897          31.158         0.86652         0.70642


 TIME FOR THE TIME STEP              260:        0.63475E+02

===============================================================


 INSTANT    0.240300000E-01   TIME STEP NUMBER             261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.485157156E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866312E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49220E+02 0.98394E+01
   Friction velocity        uet   :  0.88084E-03 0.51462E+01
   Friction velocity        uk    :  0.77167E-02 0.19590E+01
   Dimensionless distance   yplus :  0.69878E-01 0.53270E+02
   Friction thermal sca.    tstar : -0.66429E+03 0.39787E+02
   Rough dim-less th. sca.  tplus :  0.52137E-01 0.13423E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134454
   Nb of faces within the viscous sub-layer     :       8758
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        255 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20830E+00      31   0.24941E-01   0.31071E+02 0.11848E+03 
c  Velocity[X]                                      0.26924E+02 
c  Velocity[Y]                                      0.95263E+00 
c  Velocity[Z]                                      0.31936E+01 
c  Pressure     0.12495E-03     148   0.58983E-02   0.17578E+00 0.27392E+03 
c  k            0.65472E-02      22   0.87429E-03   0.37637E+01 0.76061E+03 
c  omega        0.15127E+03      40   0.12383E-03   0.63250E+09 0.56534E+03 
c  TempC        0.35251E+04      55   0.19425E-01   0.12244E+06 0.22366E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1065          56.529          3.9894          4.0989
v  Velocity[Y]            -8.8394          7.5224       0.0011896      0.00098987
v  Velocity[Z]             -16.82          19.681        -0.25007        -0.12396
v  ǁVelocityǁ           0.0037272          56.656          4.3209          4.2196
v  Pressure               -1924.5          30.702          7.8503          15.897
v  k                   2.4082e-08          12.562        0.096842        0.086644
v  omega               8.4305e-05      5.8501e+05          4761.6            1378
v  TempC                  -107.77          595.85          50.329          54.258
v  Density                0.41027          2.4217          1.1727          1.1891
v  TurbVisc            2.0635e-14       0.0022901      0.00013435      0.00019619
v  CourantNb                    0          29.339         0.73827         0.54205
v  FourierNb            0.0024993          4.6713         0.12922         0.16545
v  total_pressure           99401      1.0136e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41865          2.4217          1.1074          1.1565


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014137          29.471         0.86749         0.70751


 TIME FOR THE TIME STEP              261:        0.64663E+02

===============================================================


 INSTANT    0.241300000E-01   TIME STEP NUMBER             262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.152779097E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155865308E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50972E+02 0.99358E+01
   Friction velocity        uet   :  0.17053E-02 0.50663E+01
   Friction velocity        uk    :  0.13259E-01 0.19528E+01
   Dimensionless distance   yplus :  0.11997E+00 0.53154E+02
   Friction thermal sca.    tstar : -0.38302E+03 0.43277E+02
   Rough dim-less th. sca.  tplus :  0.89513E-01 0.13418E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134397
   Nb of faces within the viscous sub-layer     :       8802
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        275 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20837E+00      31   0.23524E-01   0.30452E+02 0.11717E+03 
c  Velocity[X]                                      0.26318E+02 
c  Velocity[Y]                                      0.92770E+00 
c  Velocity[Z]                                      0.32066E+01 
c  Pressure     0.12181E-03     149   0.58742E-02   0.17071E+00 0.31321E+03 
c  k            0.65598E-02      22   0.86909E-03   0.37629E+01 0.75949E+03 
c  omega        0.15107E+03      40   0.26305E-03   0.53533E+10 0.16236E+04 
c  TempC        0.35318E+04      55   0.20102E-01   0.12106E+06 0.22192E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0965          56.051          3.9914          4.1016
v  Velocity[Y]            -8.8546          7.5709       0.0011955      0.00098792
v  Velocity[Z]            -15.963          20.088        -0.25118        -0.12469
v  ǁVelocityǁ           0.0086852           56.19           4.324          4.2229
v  Pressure               -1934.5          29.951          7.0975          15.166
v  k                   1.8458e-08          12.833        0.097104        0.086934
v  omega               2.6617e-06      3.3513e+06          4766.9          1378.2
v  TempC                  -109.81          608.28          50.516          54.483
v  Density                0.40643          2.1356          1.1723          1.1887
v  TurbVisc            1.2509e-13       0.0022899      0.00013493      0.00019701
v  CourantNb                    0          31.776         0.73874         0.54246
v  FourierNb            0.0024994          4.6713         0.12973         0.16614
v  total_pressure           99391      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41036          2.0642           1.107          1.1562


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018855          31.909         0.86847          0.7086


 TIME FOR THE TIME STEP              262:        0.64713E+02

===============================================================


 INSTANT    0.242300000E-01   TIME STEP NUMBER             263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.384657747E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155865985E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49467E+02 0.98825E+01
   Friction velocity        uet   :  0.37564E-02 0.51780E+01
   Friction velocity        uk    :  0.11843E-01 0.19744E+01
   Dimensionless distance   yplus :  0.12641E+00 0.53284E+02
   Friction thermal sca.    tstar : -0.30015E+03 0.47384E+02
   Rough dim-less th. sca.  tplus :  0.94314E-01 0.13424E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134332
   Nb of faces within the viscous sub-layer     :       8842
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        282 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20845E+00      31   0.23359E-01   0.30206E+02 0.11657E+03 
c  Velocity[X]                                      0.26049E+02 
c  Velocity[Y]                                      0.94402E+00 
c  Velocity[Z]                                      0.32133E+01 
c  Pressure     0.12347E-03     135   0.58395E-02   0.17251E+00 0.29363E+03 
c  k            0.65766E-02      22   0.86017E-03   0.37701E+01 0.75917E+03 
c  omega        0.20213E+03      39   0.12641E-03   0.19404E+10 0.98443E+03 
c  TempC        0.35384E+04      56   0.20115E-01   0.12195E+06 0.22227E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1045          56.373          3.9934          4.1043
v  Velocity[Y]            -8.8613          7.4621        0.001205      0.00099168
v  Velocity[Z]            -16.151          19.726        -0.25235        -0.12543
v  ǁVelocityǁ           0.0077956          56.508          4.3271          4.2262
v  Pressure               -1947.4          29.174          6.4254          14.495
v  k                   1.1954e-08          12.778        0.097366        0.087226
v  omega               4.7703e-07      1.6986e+06          4768.1          1378.2
v  TempC                  -116.35          590.82          50.701          54.707
v  Density                0.40069          2.1622          1.1719          1.1883
v  TurbVisc            9.5816e-14       0.0022897      0.00013551      0.00019782
v  CourantNb                    0          31.264         0.73922         0.54288
v  FourierNb            0.0024996          4.6712         0.13025         0.16682
v  total_pressure           99378      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41085          2.1496          1.1067          1.1558


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021142          31.402         0.86947          0.7097


 TIME FOR THE TIME STEP              263:        0.64034E+02

===============================================================


 INSTANT    0.243300000E-01   TIME STEP NUMBER             264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.112279629E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867785E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51377E+02 0.10051E+02
   Friction velocity        uet   :  0.27666E-02 0.51435E+01
   Friction velocity        uk    :  0.12912E-01 0.19680E+01
   Dimensionless distance   yplus :  0.13599E+00 0.53171E+02
   Friction thermal sca.    tstar : -0.37215E+03 0.50584E+02
   Rough dim-less th. sca.  tplus :  0.10147E+00 0.13419E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134272
   Nb of faces within the viscous sub-layer     :       8859
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        307 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20853E+00      31   0.24654E-01   0.30363E+02 0.11675E+03 
c  Velocity[X]                                      0.26253E+02 
c  Velocity[Y]                                      0.93151E+00 
c  Velocity[Z]                                      0.31790E+01 
c  Pressure     0.12201E-03     150   0.56285E-02   0.16967E+00 0.36580E+03 
c  k            0.65944E-02      22   0.84797E-03   0.37630E+01 0.75735E+03 
c  omega        0.15585E+03      40   0.18762E-03   0.67705E+10 0.18152E+04 
c  TempC        0.35451E+04      54   0.19463E-01   0.12224E+06 0.22208E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0844          60.773          3.9954           4.107
v  Velocity[Y]            -8.8777          7.4998       0.0012037        0.000992
v  Velocity[Z]            -16.323          19.943        -0.25355        -0.12618
v  ǁVelocityǁ            0.010258          60.777          4.3302          4.2296
v  Pressure               -1958.7          28.378          5.5743          13.661
v  k                   5.3619e-09          12.712        0.097624         0.08752
v  omega               9.7923e-08      4.4558e+06          4772.7          1378.3
v  TempC                   -113.4          590.74          50.888          54.932
v  Density                0.40879          2.2524          1.1715          1.1879
v  TurbVisc            6.1985e-14       0.0022897      0.00013608      0.00019862
v  CourantNb                    0          29.641         0.73971         0.54329
v  FourierNb            0.0024998          4.6712         0.13075          0.1675
v  total_pressure           99366      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41209          2.2524          1.1064          1.1554


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018642          29.774         0.87046         0.71079


 TIME FOR THE TIME STEP              264:        0.64370E+02

===============================================================


 INSTANT    0.244300000E-01   TIME STEP NUMBER             265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.969816198E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867155E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49421E+02 0.99944E+01
   Friction velocity        uet   :  0.14944E-02 0.51694E+01
   Friction velocity        uk    :  0.12008E-01 0.19652E+01
   Dimensionless distance   yplus :  0.13430E+00 0.53580E+02
   Friction thermal sca.    tstar : -0.40355E+03 0.56015E+02
   Rough dim-less th. sca.  tplus :  0.10020E+00 0.13437E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     134117
   Nb of faces within the viscous sub-layer     :       8870
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        325 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20859E+00      31   0.24460E-01   0.30627E+02 0.11713E+03 
c  Velocity[X]                                      0.26432E+02 
c  Velocity[Y]                                      0.97068E+00 
c  Velocity[Z]                                      0.32237E+01 
c  Pressure     0.12457E-03     130   0.58107E-02   0.17309E+00 0.28615E+03 
c  k            0.66162E-02      23   0.84607E-03   0.37612E+01 0.75608E+03 
c  omega        0.23968E+03      39   0.10188E-03   0.20479E+10 0.10089E+04 
c  TempC        0.35519E+04      55   0.19591E-01   0.12228E+06 0.22166E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0788          57.431          3.9973          4.1096
v  Velocity[Y]            -8.0372          7.6311       0.0012382      0.00099458
v  Velocity[Z]            -16.303          19.883        -0.25478        -0.12693
v  ǁVelocityǁ           0.0065477          57.567          4.3333           4.233
v  Pressure               -1965.2          27.738           4.968          13.028
v  k                   3.1675e-09           12.97        0.097884        0.087813
v  omega               2.7593e-08      2.2486e+06            4773          1378.2
v  TempC                  -108.52          582.37          51.073          55.156
v  Density                0.40883          2.2109          1.1711          1.1874
v  TurbVisc            2.7777e-14       0.0022896      0.00013668      0.00019946
v  CourantNb                    0          32.001         0.74021         0.54371
v  FourierNb            0.0024999          4.6712         0.13128          0.1682
v  total_pressure           99360      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41458          2.1734          1.1061          1.1551


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016154          32.135         0.87148         0.71191


 TIME FOR THE TIME STEP              265:        0.63820E+02

===============================================================


 INSTANT    0.245300000E-01   TIME STEP NUMBER             266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.347313406E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866502E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51433E+02 0.10007E+02
   Friction velocity        uet   :  0.10580E-02 0.53196E+01
   Friction velocity        uk    :  0.13048E-01 0.19813E+01
   Dimensionless distance   yplus :  0.14584E+00 0.53450E+02
   Friction thermal sca.    tstar : -0.40602E+03 0.62335E+02
   Rough dim-less th. sca.  tplus :  0.10881E+00 0.13431E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133976
   Nb of faces within the viscous sub-layer     :       8909
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        347 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20868E+00      32   0.24468E-01   0.30917E+02 0.11756E+03 
c  Velocity[X]                                      0.26633E+02 
c  Velocity[Y]                                      0.96883E+00 
c  Velocity[Z]                                      0.33149E+01 
c  Pressure     0.12351E-03     146   0.56406E-02   0.17084E+00 0.35665E+03 
c  k            0.66360E-02      22   0.85029E-03   0.37665E+01 0.75557E+03 
c  omega        0.16018E+03      40   0.15275E-03   0.62611E+10 0.17442E+04 
c  TempC        0.35588E+04      55   0.19831E-01   0.12057E+06 0.21964E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0711          57.392          3.9993          4.1123
v  Velocity[Y]            -7.9546          7.7048       0.0012593       0.0010003
v  Velocity[Z]            -16.735          20.496        -0.25606         -0.1277
v  ǁVelocityǁ            0.011609          57.552          4.3364          4.2363
v  Pressure               -1976.9          26.888          4.1835          12.247
v  k                    1.533e-08          12.817        0.098139        0.088105
v  omega               9.5712e-09      3.3803e+06          4778.3          1378.5
v  TempC                  -116.68          587.49          51.258          55.381
v  Density                0.41283          2.1453          1.1707           1.187
v  TurbVisc            1.6397e-14       0.0022896      0.00013727      0.00020029
v  CourantNb                    0          31.897          0.7407         0.54413
v  FourierNb            0.0025001          4.6712          0.1318         0.16889
v  total_pressure           99348      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41676          2.0992          1.1057          1.1547


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013576          32.036          0.8725         0.71303


 TIME FOR THE TIME STEP              266:        0.64679E+02

===============================================================


 INSTANT    0.246300000E-01   TIME STEP NUMBER             267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.223501113E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155865439E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49653E+02 0.10077E+02
   Friction velocity        uet   :  0.16867E-02 0.52164E+01
   Friction velocity        uk    :  0.12385E-01 0.19732E+01
   Dimensionless distance   yplus :  0.16456E+00 0.54133E+02
   Friction thermal sca.    tstar : -0.37586E+03 0.69703E+02
   Rough dim-less th. sca.  tplus :  0.12278E+00 0.13462E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133922
   Nb of faces within the viscous sub-layer     :       8971
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        371 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20875E+00      32   0.24518E-01   0.30291E+02 0.11624E+03 
c  Velocity[X]                                      0.26061E+02 
c  Velocity[Y]                                      0.95843E+00 
c  Velocity[Z]                                      0.32718E+01 
c  Pressure     0.12278E-03     127   0.56603E-02   0.16909E+00 0.20949E+03 
c  k            0.66557E-02      23   0.85181E-03   0.37758E+01 0.75543E+03 
c  omega        0.22269E+03      40   0.93068E-04   0.32158E+10 0.12575E+04 
c  TempC        0.35657E+04      56   0.19647E-01   0.12127E+06 0.21983E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0625          58.005          4.0013           4.115
v  Velocity[Y]            -7.6643          7.5901       0.0012549       0.0009988
v  Velocity[Z]            -16.423          20.066        -0.25738        -0.12847
v  ǁVelocityǁ            0.010986          58.155          4.3395          4.2397
v  Pressure               -1994.8          26.729          3.7878          11.817
v  k                   2.1641e-08          13.016        0.098404        0.088397
v  omega               4.1465e-09      2.0343e+06          4780.6          1378.5
v  TempC                  -103.19           593.5          51.442          55.606
v  Density                0.41037          2.2572          1.1703          1.1866
v  TurbVisc            7.9299e-14       0.0022895      0.00013786      0.00020112
v  CourantNb                    0          29.778         0.74121         0.54455
v  FourierNb            0.0025002          4.6712         0.13232         0.16959
v  total_pressure           99330      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41443          2.2572          1.1054          1.1543


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010912          29.912         0.87353         0.71414


 TIME FOR THE TIME STEP              267:        0.63551E+02

===============================================================


 INSTANT    0.247300000E-01   TIME STEP NUMBER             268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.609837638E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155863082E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51470E+02 0.10009E+02
   Friction velocity        uet   :  0.15095E-02 0.51268E+01
   Friction velocity        uk    :  0.11933E-01 0.19852E+01
   Dimensionless distance   yplus :  0.14232E+00 0.54246E+02
   Friction thermal sca.    tstar : -0.42038E+03 0.76447E+02
   Rough dim-less th. sca.  tplus :  0.10619E+00 0.13467E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133831
   Nb of faces within the viscous sub-layer     :       9026
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        383 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20883E+00      31   0.25600E-01   0.30749E+02 0.11699E+03 
c  Velocity[X]                                      0.26425E+02 
c  Velocity[Y]                                      0.96370E+00 
c  Velocity[Z]                                      0.33606E+01 
c  Pressure     0.12368E-03     126   0.56938E-02   0.16970E+00 0.18898E+03 
c  k            0.66720E-02      23   0.84409E-03   0.37612E+01 0.75279E+03 
c  omega        0.16422E+03      40   0.16608E-03   0.14890E+10 0.85817E+03 
c  TempC        0.35727E+04      55   0.19576E-01   0.12216E+06 0.22018E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0661          60.421          4.0032          4.1177
v  Velocity[Y]            -8.0251          7.5595       0.0012968       0.0010045
v  Velocity[Z]            -16.464           20.29        -0.25869        -0.12924
v  ǁVelocityǁ           0.0096081          60.426          4.3427          4.2431
v  Pressure               -2003.6          26.035           3.391          11.429
v  k                   4.3678e-08          12.873        0.098681        0.088692
v  omega               2.0847e-09      1.0334e+06          4783.6          1378.6
v  TempC                  -111.55          596.94          51.626          55.831
v  Density                0.40753          2.0781          1.1699          1.1862
v  TurbVisc            1.5349e-13       0.0022899      0.00013844      0.00020193
v  CourantNb                    0          31.712         0.74171         0.54497
v  FourierNb            0.0025004          4.6712         0.13283         0.17027
v  total_pressure           99321      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.42003          2.0781          1.1051           1.154


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0082214          31.846         0.87455         0.71524


 TIME FOR THE TIME STEP              268:        0.63664E+02

===============================================================


 INSTANT    0.248300000E-01   TIME STEP NUMBER             269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.198659301E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155862971E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49734E+02 0.10187E+02
   Friction velocity        uet   :  0.24375E-02 0.51920E+01
   Friction velocity        uk    :  0.11755E-01 0.19775E+01
   Dimensionless distance   yplus :  0.13453E+00 0.54670E+02
   Friction thermal sca.    tstar : -0.63240E+03 0.85403E+02
   Rough dim-less th. sca.  tplus :  0.10037E+00 0.13485E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133727
   Nb of faces within the viscous sub-layer     :       9052
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        406 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20889E+00      31   0.24595E-01   0.31633E+02 0.11853E+03 
c  Velocity[X]                                      0.27262E+02 
c  Velocity[Y]                                      0.99386E+00 
c  Velocity[Z]                                      0.33777E+01 
c  Pressure     0.12569E-03     127   0.57986E-02   0.17224E+00 0.13502E+03 
c  k            0.66845E-02      23   0.84213E-03   0.37359E+01 0.74908E+03 
c  omega        0.15429E+03      41   0.21837E-03   0.89724E+10 0.20661E+04 
c  TempC        0.35796E+04      57   0.19381E-01   0.12237E+06 0.21992E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0885          57.062          4.0052          4.1204
v  Velocity[Y]            -8.2962          7.6381       0.0012733       0.0010025
v  Velocity[Z]            -16.531          20.191        -0.26005        -0.13002
v  ǁVelocityǁ           0.0093182           57.23          4.3459          4.2464
v  Pressure               -2021.9          26.011          3.1418          11.196
v  k                   2.7743e-08          12.925        0.098969        0.088987
v  omega               1.0643e-09      4.5728e+06          4787.2          1378.8
v  TempC                  -118.51          592.72          51.811          56.055
v  Density                0.40592          2.1855          1.1696          1.1858
v  TurbVisc             1.992e-13       0.0022902      0.00013901      0.00020276
v  CourantNb                    0          31.379         0.74223          0.5454
v  FourierNb            0.0025005          4.6712         0.13335         0.17096
v  total_pressure           99303      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41424          2.1855          1.1047          1.1536


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010483          31.518         0.87558         0.71635


 TIME FOR THE TIME STEP              269:        0.63246E+02

===============================================================


 INSTANT    0.249300000E-01   TIME STEP NUMBER             270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.316948592E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155862153E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51791E+02 0.10238E+02
   Friction velocity        uet   :  0.13515E-02 0.51401E+01
   Friction velocity        uk    :  0.12787E-01 0.19791E+01
   Dimensionless distance   yplus :  0.13882E+00 0.54418E+02
   Friction thermal sca.    tstar : -0.37338E+03 0.85985E+02
   Rough dim-less th. sca.  tplus :  0.10358E+00 0.13474E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133667
   Nb of faces within the viscous sub-layer     :       9100
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        424 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20897E+00      32   0.25445E-01   0.30947E+02 0.11712E+03 
c  Velocity[X]                                      0.26562E+02 
c  Velocity[Y]                                      0.98983E+00 
c  Velocity[Z]                                      0.33955E+01 
c  Pressure     0.12519E-03     129   0.57133E-02   0.17114E+00 0.16186E+03 
c  k            0.66931E-02      23   0.84284E-03   0.37317E+01 0.74758E+03 
c  omega        0.31115E+03      39   0.84637E-04   0.27921E+10 0.11683E+04 
c  TempC        0.35866E+04      56   0.19709E-01   0.12108E+06 0.21831E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0754           61.04          4.0072          4.1231
v  Velocity[Y]            -8.4496          7.6703       0.0012643      0.00099655
v  Velocity[Z]            -16.395          20.411        -0.26145        -0.13081
v  ǁVelocityǁ           0.0026095          61.051          4.3491          4.2498
v  Pressure               -2039.3          25.743          2.8074          10.902
v  k                   1.2444e-08           13.13        0.099262         0.08928
v  omega               7.0823e-10      2.3094e+06            4790            1379
v  TempC                  -116.64          619.29          51.997          56.281
v  Density                0.40789          2.2838          1.1692          1.1853
v  TurbVisc            1.7174e-13       0.0022899       0.0001396      0.00020358
v  CourantNb                    0          30.226         0.74275         0.54582
v  FourierNb            0.0025006          4.6712         0.13387         0.17165
v  total_pressure           99286      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41744          2.2838          1.1044          1.1532


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010391          30.361         0.87662         0.71747


 TIME FOR THE TIME STEP              270:        0.63601E+02

===============================================================


 INSTANT    0.250300000E-01   TIME STEP NUMBER             271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.303620830E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155862062E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49785E+02 0.10250E+02
   Friction velocity        uet   :  0.18914E-02 0.51798E+01
   Friction velocity        uk    :  0.12229E-01 0.19957E+01
   Dimensionless distance   yplus :  0.20515E+00 0.54664E+02
   Friction thermal sca.    tstar : -0.41354E+03 0.83839E+02
   Rough dim-less th. sca.  tplus :  0.15307E+00 0.13485E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133584
   Nb of faces within the viscous sub-layer     :       9128
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        439 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20906E+00      32   0.26078E-01   0.30865E+02 0.11683E+03 
c  Velocity[X]                                      0.26399E+02 
c  Velocity[Y]                                      0.98881E+00 
c  Velocity[Z]                                      0.34773E+01 
c  Pressure     0.12463E-03     133   0.57267E-02   0.16977E+00 0.17543E+03 
c  k            0.67022E-02      23   0.83851E-03   0.37424E+01 0.74766E+03 
c  omega        0.16894E+03      41   0.12635E-03   0.10898E+10 0.73207E+03 
c  TempC        0.35934E+04      56   0.19863E-01   0.12145E+06 0.21820E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0787          58.323          4.0092          4.1258
v  Velocity[Y]             -8.528          7.5871       0.0012728      0.00099454
v  Velocity[Z]             -16.84          20.431        -0.26292        -0.13162
v  ǁVelocityǁ           0.0097048            58.5          4.3524          4.2533
v  Pressure               -2048.7          25.307          2.4515          10.582
v  k                   2.1714e-09          13.142        0.099556         0.08957
v  omega               4.9729e-10      1.1774e+06          4791.6            1379
v  TempC                  -110.32           611.4          52.185          56.506
v  Density                0.39575          2.2566          1.1688          1.1849
v  TurbVisc            7.7016e-14       0.0022899      0.00014017      0.00020441
v  CourantNb                    0          32.412         0.74327         0.54624
v  FourierNb            0.0025008          4.6712         0.13439         0.17234
v  total_pressure           99276      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41841          2.2566          1.1041          1.1529


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0077727          32.549         0.87766         0.71858


 TIME FOR THE TIME STEP              271:        0.63870E+02

===============================================================


 INSTANT    0.251300000E-01   TIME STEP NUMBER             272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.286739222E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155863230E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51809E+02 0.10177E+02
   Friction velocity        uet   :  0.26424E-02 0.53088E+01
   Friction velocity        uk    :  0.10383E-01 0.19950E+01
   Dimensionless distance   yplus :  0.18561E+00 0.54673E+02
   Friction thermal sca.    tstar : -0.37197E+03 0.79930E+02
   Rough dim-less th. sca.  tplus :  0.13849E+00 0.13485E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133597
   Nb of faces within the viscous sub-layer     :       9182
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        457 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20913E+00      31   0.24503E-01   0.31494E+02 0.11789E+03 
c  Velocity[X]                                      0.26970E+02 
c  Velocity[Y]                                      0.99994E+00 
c  Velocity[Z]                                      0.35246E+01 
c  Pressure     0.12595E-03     120   0.57577E-02   0.17120E+00 0.16387E+03 
c  k            0.67131E-02      23   0.83082E-03   0.37444E+01 0.74683E+03 
c  omega        0.15486E+03      41   0.14549E-03   0.95448E+09 0.68442E+03 
c  TempC        0.36001E+04      58   0.19451E-01   0.12186E+06 0.21812E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.078          59.992          4.0112          4.1285
v  Velocity[Y]            -8.6623          7.6604       0.0012577      0.00098363
v  Velocity[Z]            -16.908           20.58        -0.26442        -0.13244
v  ǁVelocityǁ           0.0077036          60.165          4.3557          4.2567
v  Pressure               -2062.1          24.925          2.1774          10.274
v  k                   8.4876e-09          13.261         0.09985        0.089861
v  omega               3.7804e-10      1.0741e+06          4795.1          1379.2
v  TempC                  -120.49          625.23          52.375           56.73
v  Density                0.39928           2.169          1.1684          1.1845
v  TurbVisc            1.3435e-14       0.0022899      0.00014074      0.00020522
v  CourantNb                    0          32.095         0.74383         0.54668
v  FourierNb            0.0025009          4.6712         0.13489         0.17302
v  total_pressure           99263      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41588          2.1127          1.1037          1.1525


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0068695          32.237         0.87872         0.71969


 TIME FOR THE TIME STEP              272:        0.62926E+02

===============================================================


 INSTANT    0.252300000E-01   TIME STEP NUMBER             273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.152864973E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155860225E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49756E+02 0.10128E+02
   Friction velocity        uet   :  0.34642E-02 0.53128E+01
   Friction velocity        uk    :  0.10744E-01 0.20057E+01
   Dimensionless distance   yplus :  0.13460E+00 0.55266E+02
   Friction thermal sca.    tstar : -0.34789E+03 0.75311E+02
   Rough dim-less th. sca.  tplus :  0.10042E+00 0.13511E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133567
   Nb of faces within the viscous sub-layer     :       9251
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        482 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20921E+00      32   0.24878E-01   0.31123E+02 0.11707E+03 
c  Velocity[X]                                      0.26658E+02 
c  Velocity[Y]                                      0.98991E+00 
c  Velocity[Z]                                      0.34743E+01 
c  Pressure     0.12369E-03     123   0.55842E-02   0.16760E+00 0.94485E+02 
c  k            0.67287E-02      23   0.83024E-03   0.37534E+01 0.74671E+03 
c  omega        0.15460E+03      42   0.18257E-03   0.12145E+10 0.77039E+03 
c  TempC        0.36068E+04      57   0.19447E-01   0.12187E+06 0.21769E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0518           59.68          4.0133          4.1312
v  Velocity[Y]            -8.6084          7.6026       0.0012343      0.00097906
v  Velocity[Z]            -17.113          20.299        -0.26594        -0.13325
v  ǁVelocityǁ           0.0082137          59.851          4.3591          4.2601
v  Pressure               -2082.4           25.39          2.1231          10.193
v  k                   9.3502e-09          13.284         0.10014        0.090152
v  omega               3.1503e-10      1.0796e+06          4800.4          1379.5
v  TempC                  -127.18          603.14          52.564          56.955
v  Density                0.39313          2.3135           1.168          1.1841
v  TurbVisc            5.2498e-14       0.0022899      0.00014132      0.00020605
v  CourantNb                    0          30.048         0.74437          0.5471
v  FourierNb             0.002501          4.6712         0.13541         0.17371
v  total_pressure           99243      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41951          2.3135          1.1034          1.1521


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0097403          30.185         0.87978         0.72082


 TIME FOR THE TIME STEP              273:        0.63522E+02

===============================================================


 INSTANT    0.253300000E-01   TIME STEP NUMBER             274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.293073308E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155858200E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51407E+02 0.10254E+02
   Friction velocity        uet   :  0.39289E-02 0.53056E+01
   Friction velocity        uk    :  0.11421E-01 0.20049E+01
   Dimensionless distance   yplus :  0.16175E+00 0.54913E+02
   Friction thermal sca.    tstar : -0.31540E+03 0.68589E+02
   Rough dim-less th. sca.  tplus :  0.12068E+00 0.13496E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133527
   Nb of faces within the viscous sub-layer     :       9279
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        503 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20929E+00      31   0.25972E-01   0.31342E+02 0.11735E+03 
c  Velocity[X]                                      0.26822E+02 
c  Velocity[Y]                                      0.99127E+00 
c  Velocity[Z]                                      0.35286E+01 
c  Pressure     0.12425E-03     124   0.56671E-02   0.16767E+00 0.89608E+02 
c  k            0.67469E-02      23   0.83334E-03   0.37554E+01 0.74586E+03 
c  omega        0.15493E+03      41   0.15584E-03   0.65745E+09 0.56666E+03 
c  TempC        0.36135E+04      56   0.19504E-01   0.12191E+06 0.21730E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.05          59.865          4.0153          4.1338
v  Velocity[Y]            -9.1175          7.5353       0.0012664      0.00098537
v  Velocity[Z]            -17.633          20.749        -0.26749        -0.13408
v  ǁVelocityǁ           0.0053969          60.041          4.3624          4.2635
v  Pressure               -2090.6          25.307          2.1205          10.188
v  k                   3.3602e-10          13.462         0.10041        0.090443
v  omega               2.8272e-10      5.8401e+05            4803          1379.7
v  TempC                  -133.02          628.89          52.754           57.18
v  Density                0.40304          2.4196          1.1676          1.1837
v  TurbVisc            5.7836e-14       0.0022897      0.00014189      0.00020688
v  CourantNb                    0          33.042         0.74492         0.54753
v  FourierNb            0.0025012          4.6712         0.13593          0.1744
v  total_pressure           99234      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41868          2.1284           1.103          1.1517


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012636           33.18         0.88085         0.72194


 TIME FOR THE TIME STEP              274:        0.63595E+02

===============================================================


 INSTANT    0.254300000E-01   TIME STEP NUMBER             275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.142368087E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855599E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50039E+02 0.10294E+02
   Friction velocity        uet   :  0.35765E-02 0.54711E+01
   Friction velocity        uk    :  0.11605E-01 0.20195E+01
   Dimensionless distance   yplus :  0.11830E+00 0.55336E+02
   Friction thermal sca.    tstar : -0.32866E+03 0.59523E+02
   Rough dim-less th. sca.  tplus :  0.88268E-01 0.13514E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133512
   Nb of faces within the viscous sub-layer     :       9304
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        522 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20936E+00      33   0.25453E-01   0.31895E+02 0.11825E+03 
c  Velocity[X]                                      0.27297E+02 
c  Velocity[Y]                                      0.10430E+01 
c  Velocity[Z]                                      0.35543E+01 
c  Pressure     0.12529E-03     126   0.59441E-02   0.16862E+00 0.13862E+03 
c  k            0.67697E-02      24   0.84112E-03   0.37558E+01 0.74483E+03 
c  omega        0.15467E+03      41   0.14877E-03   0.69591E+09 0.58226E+03 
c  TempC        0.36202E+04      58   0.19686E-01   0.12155E+06 0.21654E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0338          59.173          4.0173          4.1365
v  Velocity[Y]            -9.1239          7.5117        0.001284      0.00098605
v  Velocity[Z]            -17.702          20.468        -0.26914        -0.13493
v  ǁVelocityǁ           0.0051812          59.348          4.3658           4.267
v  Pressure               -2104.9          26.761           2.357           10.41
v  k                   1.4796e-08          13.386         0.10067        0.090736
v  omega               2.8801e-10      5.8408e+05          4806.4          1379.9
v  TempC                  -136.72          617.93          52.941          57.404
v  Density                0.39154          2.5204          1.1672          1.1832
v  TurbVisc            1.5389e-15         0.00229      0.00014246      0.00020769
v  CourantNb                    0          32.725         0.74549         0.54797
v  FourierNb            0.0025013          4.6712         0.13643         0.17508
v  total_pressure           99220      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39154          2.1967          1.1027          1.1514


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015591          32.868         0.88192         0.72304


 TIME FOR THE TIME STEP              275:        0.63663E+02

===============================================================


 INSTANT    0.255300000E-01   TIME STEP NUMBER             276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.177643088E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155851830E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52211E+02 0.10442E+02
   Friction velocity        uet   :  0.99047E-03 0.53343E+01
   Friction velocity        uk    :  0.98845E-02 0.20129E+01
   Dimensionless distance   yplus :  0.10377E+00 0.55229E+02
   Friction thermal sca.    tstar : -0.44712E+03 0.60541E+02
   Rough dim-less th. sca.  tplus :  0.77421E-01 0.13509E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133477
   Nb of faces within the viscous sub-layer     :       9307
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        529 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20945E+00      32   0.26322E-01   0.31846E+02 0.11803E+03 
c  Velocity[X]                                      0.27165E+02 
c  Velocity[Y]                                      0.10160E+01 
c  Velocity[Z]                                      0.36645E+01 
c  Pressure     0.12526E-03     147   0.57645E-02   0.16775E+00 0.33594E+03 
c  k            0.67940E-02      24   0.85654E-03   0.37460E+01 0.74271E+03 
c  omega        0.15496E+03      41   0.16627E-03   0.30493E+10 0.12106E+04 
c  TempC        0.36271E+04      57   0.19624E-01   0.12229E+06 0.21677E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0091          63.254          4.0193          4.1392
v  Velocity[Y]            -9.2924          7.5152       0.0012813      0.00098142
v  Velocity[Z]            -16.989          20.819        -0.27088        -0.13581
v  ǁVelocityǁ           0.0043955          63.266          4.3693          4.2704
v  Pressure                 -2123          27.377          3.1424          11.136
v  k                   1.6792e-08           13.55         0.10093        0.091032
v  omega               2.8995e-10       2.927e+06          4810.2          1380.1
v  TempC                  -139.51          605.72          53.128          57.628
v  Density                0.39636          2.5887          1.1668          1.1828
v  TurbVisc            8.9565e-14       0.0022903      0.00014302      0.00020851
v  CourantNb                    0          30.825         0.74607          0.5484
v  FourierNb            0.0025014          4.6712         0.13693         0.17575
v  total_pressure           99202      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39636          2.3102          1.1023           1.151


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017441          30.962           0.883         0.72415


 TIME FOR THE TIME STEP              276:        0.64161E+02

===============================================================


 INSTANT    0.256300000E-01   TIME STEP NUMBER             277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.430317242E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155844696E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50380E+02 0.10435E+02
   Friction velocity        uet   :  0.29427E-02 0.52662E+01
   Friction velocity        uk    :  0.12710E-01 0.20278E+01
   Dimensionless distance   yplus :  0.14455E+00 0.55597E+02
   Friction thermal sca.    tstar : -0.34851E+03 0.49398E+02
   Rough dim-less th. sca.  tplus :  0.10785E+00 0.13525E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133357
   Nb of faces within the viscous sub-layer     :       9332
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        545 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20952E+00      32   0.25599E-01   0.32282E+02 0.11871E+03 
c  Velocity[X]                                      0.27557E+02 
c  Velocity[Y]                                      0.10167E+01 
c  Velocity[Z]                                      0.37090E+01 
c  Pressure     0.12882E-03     156   0.58226E-02   0.17222E+00 0.57357E+03 
c  k            0.68213E-02      24   0.86820E-03   0.37232E+01 0.73929E+03 
c  omega        0.17568E+03      42   0.18153E-03   0.25347E+10 0.11041E+04 
c  TempC        0.36340E+04      57   0.19268E-01   0.12242E+06 0.21646E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0037          60.058          4.0212          4.1418
v  Velocity[Y]            -9.3169          7.5247       0.0012688      0.00097881
v  Velocity[Z]            -17.567          20.516        -0.27269         -0.1367
v  ǁVelocityǁ            0.005176          60.263          4.3728          4.2738
v  Pressure               -2132.7          29.358           4.469          12.453
v  k                   1.8027e-08           13.63         0.10118        0.091328
v  omega               3.2075e-10      1.4851e+06          4813.1          1380.3
v  TempC                  -139.23          601.36          53.312          57.852
v  Density                0.40186          2.6429          1.1664          1.1824
v  TurbVisc            8.9665e-14       0.0022902      0.00014358      0.00020931
v  CourantNb                    0          32.948         0.74666         0.54883
v  FourierNb            0.0025016          4.6712         0.13743         0.17642
v  total_pressure           99192      1.0135e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40433          2.2515           1.102          1.1506


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01923          33.088         0.88409         0.72525


 TIME FOR THE TIME STEP              277:        0.65033E+02

===============================================================


 INSTANT    0.257300000E-01   TIME STEP NUMBER             278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.233320992E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155839823E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52595E+02 0.10559E+02
   Friction velocity        uet   :  0.34850E-02 0.53628E+01
   Friction velocity        uk    :  0.11710E-01 0.20305E+01
   Dimensionless distance   yplus :  0.18707E+00 0.55252E+02
   Friction thermal sca.    tstar : -0.38320E+03 0.44108E+02
   Rough dim-less th. sca.  tplus :  0.13957E+00 0.13510E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133301
   Nb of faces within the viscous sub-layer     :       9367
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        562 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20961E+00      32   0.25617E-01   0.31989E+02 0.11804E+03 
c  Velocity[X]                                      0.27288E+02 
c  Velocity[Y]                                      0.10058E+01 
c  Velocity[Z]                                      0.36958E+01 
c  Pressure     0.12580E-03     176   0.57629E-02   0.16744E+00 0.81130E+03 
c  k            0.68476E-02      24   0.86855E-03   0.37159E+01 0.73748E+03 
c  omega        0.16301E+03      42   0.18795E-03   0.25534E+10 0.11065E+04 
c  TempC        0.36411E+04      57   0.19643E-01   0.12125E+06 0.21500E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9879          63.543          4.0232          4.1445
v  Velocity[Y]            -9.1791          7.5664       0.0012963      0.00097897
v  Velocity[Z]            -16.939          20.578        -0.27451         -0.1376
v  ǁVelocityǁ           0.0035404          63.551          4.3763          4.2773
v  Pressure               -2150.5          31.209          6.4056          14.426
v  k                   1.9109e-08          13.761         0.10143        0.091623
v  omega               3.7859e-10      1.5495e+06          4818.1          1380.7
v  TempC                  -108.98          608.28          53.496          58.077
v  Density                0.40387          2.6373           1.166           1.182
v  TurbVisc            1.1142e-13         0.00229      0.00014416      0.00021013
v  CourantNb                    0          33.178         0.74726         0.54927
v  FourierNb            0.0025017          4.6712         0.13794         0.17711
v  total_pressure           99175      1.0136e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41194          2.1708          1.1016          1.1502


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020309          33.322          0.8852         0.72637


 TIME FOR THE TIME STEP              278:        0.66274E+02

===============================================================


 INSTANT    0.258300000E-01   TIME STEP NUMBER             279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.239006039E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155836702E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51162E+02 0.10606E+02
   Friction velocity        uet   :  0.45088E-02 0.53027E+01
   Friction velocity        uk    :  0.11691E-01 0.20426E+01
   Dimensionless distance   yplus :  0.13392E+00 0.55951E+02
   Friction thermal sca.    tstar : -0.41653E+03 0.45672E+02
   Rough dim-less th. sca.  tplus :  0.99921E-01 0.13540E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133276
   Nb of faces within the viscous sub-layer     :       9394
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        586 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20969E+00      33   0.25890E-01   0.31940E+02 0.11782E+03 
c  Velocity[X]                                      0.27126E+02 
c  Velocity[Y]                                      0.10324E+01 
c  Velocity[Z]                                      0.37817E+01 
c  Pressure     0.12693E-03     176   0.58335E-02   0.16851E+00 0.80201E+03 
c  k            0.68765E-02      24   0.85516E-03   0.37174E+01 0.73662E+03 
c  omega        0.16034E+03      42   0.17500E-03   0.25888E+10 0.11126E+04 
c  TempC        0.36482E+04      57   0.19555E-01   0.12073E+06 0.21411E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9712          61.016          4.0252          4.1472
v  Velocity[Y]            -8.9744          7.5383       0.0013158      0.00098034
v  Velocity[Z]            -17.311          20.841        -0.27644        -0.13853
v  ǁVelocityǁ           0.0076926           61.24          4.3799          4.2808
v  Pressure               -2168.4          32.075           8.385          16.485
v  k                   1.5694e-08          14.045         0.10168        0.091916
v  omega               4.6499e-10      1.1627e+06          4820.7          1380.9
v  TempC                  -103.35          607.87          53.678          58.302
v  Density                0.40069          2.1514          1.1656          1.1816
v  TurbVisc            1.1808e-13       0.0022898      0.00014474      0.00021095
v  CourantNb                    0          30.852         0.74787         0.54971
v  FourierNb            0.0025018          4.6712         0.13846         0.17779
v  total_pressure           99157      1.0136e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41381          2.0788          1.1013          1.1498


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016587          30.992         0.88633          0.7275


 TIME FOR THE TIME STEP              279:        0.66423E+02

===============================================================


 INSTANT    0.259300000E-01   TIME STEP NUMBER             280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.154174173E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155837021E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52822E+02 0.10748E+02
   Friction velocity        uet   :  0.35140E-02 0.53334E+01
   Friction velocity        uk    :  0.14443E-01 0.20605E+01
   Dimensionless distance   yplus :  0.15155E+00 0.56104E+02
   Friction thermal sca.    tstar : -0.55753E+03 0.46900E+02
   Rough dim-less th. sca.  tplus :  0.11307E+00 0.13547E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133306
   Nb of faces within the viscous sub-layer     :       9418
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        600 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20979E+00      32   0.26270E-01   0.31932E+02 0.11767E+03 
c  Velocity[X]                                      0.27234E+02 
c  Velocity[Y]                                      0.10276E+01 
c  Velocity[Z]                                      0.36702E+01 
c  Pressure     0.12608E-03     158   0.57674E-02   0.16657E+00 0.59828E+03 
c  k            0.69082E-02      24   0.83309E-03   0.37133E+01 0.73520E+03 
c  omega        0.16502E+03      42   0.13826E-03   0.11142E+10 0.73148E+03 
c  TempC        0.36554E+04      57   0.19573E-01   0.12134E+06 0.21423E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9501          65.842          4.0272          4.1499
v  Velocity[Y]            -9.0634          7.5811        0.001343      0.00097534
v  Velocity[Z]            -17.433          20.789         -0.2784        -0.13947
v  ǁVelocityǁ           0.0084103          65.853          4.3835          4.2843
v  Pressure               -2181.8          32.996          9.9306          18.088
v  k                   4.7926e-09          13.978         0.10193        0.092209
v  omega                5.785e-10      6.0503e+05          4823.2            1381
v  TempC                  -115.74          605.58           53.86          58.526
v  Density                0.40088            2.08          1.1652          1.1811
v  TurbVisc            9.6966e-14       0.0022897      0.00014532      0.00021177
v  CourantNb                    0          33.267         0.74851         0.55015
v  FourierNb            0.0025019          4.6712         0.13896         0.17847
v  total_pressure           99143      1.0136e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4122            2.08          1.1009          1.1495


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012551          33.409         0.88747         0.72862


 TIME FOR THE TIME STEP              280:        0.65132E+02

===============================================================


 INSTANT    0.260300000E-01   TIME STEP NUMBER             281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.325624457E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155837721E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51036E+02 0.10780E+02
   Friction velocity        uet   :  0.25002E-02 0.55224E+01
   Friction velocity        uk    :  0.97144E-02 0.20584E+01
   Dimensionless distance   yplus :  0.92619E-01 0.56521E+02
   Friction thermal sca.    tstar : -0.43890E+03 0.46163E+02
   Rough dim-less th. sca.  tplus :  0.69104E-01 0.13564E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133218
   Nb of faces within the viscous sub-layer     :       9429
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        615 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20988E+00      33   0.27904E-01   0.32344E+02 0.11829E+03 
c  Velocity[X]                                      0.27531E+02 
c  Velocity[Y]                                      0.10350E+01 
c  Velocity[Z]                                      0.37787E+01 
c  Pressure     0.12776E-03     155   0.56905E-02   0.16807E+00 0.50962E+03 
c  k            0.69407E-02      24   0.81966E-03   0.37017E+01 0.73302E+03 
c  omega        0.15751E+03      42   0.30327E-03   0.40224E+10 0.13789E+04 
c  TempC        0.36627E+04      58   0.19356E-01   0.12091E+06 0.21345E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9149          62.867          4.0291          4.1526
v  Velocity[Y]             -9.336          7.5279       0.0013231      0.00096656
v  Velocity[Z]            -17.235          20.997        -0.28043        -0.14044
v  ǁVelocityǁ           0.0084109          63.084          4.3871          4.2879
v  Pressure               -2201.6          34.549          11.328          19.505
v  k                   6.9884e-09           14.32         0.10219        0.092504
v  omega                7.688e-10      3.0928e+06            4827          1381.3
v  TempC                  -98.336          603.98          54.041           58.75
v  Density                0.40193          2.2437          1.1648          1.1807
v  TurbVisc            2.0958e-14       0.0022896      0.00014591       0.0002126
v  CourantNb                    0          33.355         0.74915          0.5506
v  FourierNb             0.002502          4.6712         0.13947         0.17916
v  total_pressure           99123      1.0136e+05      1.0134e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41972          2.2437          1.1005          1.1491


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015114          33.501         0.88862         0.72976


 TIME FOR THE TIME STEP              281:        0.64879E+02

===============================================================


 INSTANT    0.261300000E-01   TIME STEP NUMBER             282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.130390722E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155839164E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52894E+02 0.10814E+02
   Friction velocity        uet   :  0.14861E-02 0.55078E+01
   Friction velocity        uk    :  0.55139E-02 0.20790E+01
   Dimensionless distance   yplus :  0.66304E-01 0.56445E+02
   Friction thermal sca.    tstar : -0.45634E+03 0.47813E+02
   Rough dim-less th. sca.  tplus :  0.49470E-01 0.13561E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133191
   Nb of faces within the viscous sub-layer     :       9446
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        635 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20996E+00      32   0.26246E-01   0.32516E+02 0.11847E+03 
c  Velocity[X]                                      0.27680E+02 
c  Velocity[Y]                                      0.10679E+01 
c  Velocity[Z]                                      0.37676E+01 
c  Pressure     0.12878E-03     154   0.57933E-02   0.16887E+00 0.47307E+03 
c  k            0.69711E-02      25   0.83600E-03   0.37077E+01 0.73259E+03 
c  omega        0.19052E+03      41   0.15405E-03   0.14430E+10 0.83009E+03 
c  TempC        0.36701E+04      58   0.19383E-01   0.12019E+06 0.21240E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8964          62.295          4.0311          4.1553
v  Velocity[Y]            -9.3315          7.6508       0.0013252      0.00095782
v  Velocity[Z]            -17.652          20.819        -0.28249        -0.14141
v  ǁVelocityǁ           0.0069987           62.46          4.3908          4.2914
v  Pressure               -2218.8          35.705          12.677          20.871
v  k                   6.3686e-09          14.165         0.10245        0.092798
v  omega               1.1126e-09      1.5692e+06          4828.2          1381.4
v  TempC                  -107.18          623.95          54.221          58.975
v  Density                0.40266          2.0203          1.1644          1.1803
v  TurbVisc            4.3579e-14       0.0022895      0.00014651      0.00021344
v  CourantNb                    0          32.165         0.74979         0.55105
v  FourierNb            0.0025022          4.6712         0.13999         0.17986
v  total_pressure           99106      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41856          2.0203          1.1002          1.1487


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010398          32.308         0.88978          0.7309


 TIME FOR THE TIME STEP              282:        0.65225E+02

===============================================================


 INSTANT    0.262300000E-01   TIME STEP NUMBER             283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.481485832E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155839518E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50915E+02 0.10790E+02
   Friction velocity        uet   :  0.26317E-02 0.55201E+01
   Friction velocity        uk    :  0.12408E-01 0.20709E+01
   Dimensionless distance   yplus :  0.12862E+00 0.57223E+02
   Friction thermal sca.    tstar : -0.44292E+03 0.49342E+02
   Rough dim-less th. sca.  tplus :  0.95966E-01 0.13594E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133083
   Nb of faces within the viscous sub-layer     :       9458
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        661 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21005E+00      34   0.26285E-01   0.32221E+02 0.11780E+03 
c  Velocity[X]                                      0.27269E+02 
c  Velocity[Y]                                      0.10464E+01 
c  Velocity[Z]                                      0.39053E+01 
c  Pressure     0.12540E-03     154   0.56117E-02   0.16361E+00 0.39882E+03 
c  k            0.69999E-02      25   0.85969E-03   0.37048E+01 0.73126E+03 
c  omega        0.15991E+03      42   0.14990E-03   0.90052E+09 0.65588E+03 
c  TempC        0.36776E+04      58   0.19860E-01   0.11946E+06 0.21135E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8782          65.151           4.033           4.158
v  Velocity[Y]            -9.4555          7.5529       0.0013271      0.00095624
v  Velocity[Z]            -17.683          21.058        -0.28461         -0.1424
v  ǁVelocityǁ           0.0074948          65.163          4.3944           4.295
v  Pressure               -2231.8          36.829           13.85          22.054
v  k                   5.4444e-09          14.292         0.10272        0.093092
v  omega               1.6024e-09      8.0684e+05          4830.5          1381.6
v  TempC                  -120.64          628.24            54.4            59.2
v  Density                 0.3937           2.128           1.164          1.1799
v  TurbVisc            3.9344e-14       0.0022896       0.0001471      0.00021426
v  CourantNb                    0          33.799         0.75044          0.5515
v  FourierNb            0.0025023          4.6712         0.14051         0.18054
v  total_pressure           99093      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4137           2.128          1.0998          1.1483


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0057464          33.942         0.89094         0.73204


 TIME FOR THE TIME STEP              283:        0.65237E+02

===============================================================


 INSTANT    0.263300000E-01   TIME STEP NUMBER             284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.282137387E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155842759E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53000E+02 0.11041E+02
   Friction velocity        uet   :  0.40101E-02 0.55376E+01
   Friction velocity        uk    :  0.10813E-01 0.20792E+01
   Dimensionless distance   yplus :  0.11192E+00 0.57159E+02
   Friction thermal sca.    tstar : -0.52262E+03 0.47725E+02
   Rough dim-less th. sca.  tplus :  0.83503E-01 0.13591E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133030
   Nb of faces within the viscous sub-layer     :       9486
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        681 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21016E+00      33   0.26645E-01   0.32155E+02 0.11755E+03 
c  Velocity[X]                                      0.27216E+02 
c  Velocity[Y]                                      0.10397E+01 
c  Velocity[Z]                                      0.38990E+01 
c  Pressure     0.12506E-03     135   0.54456E-02   0.16216E+00 0.27486E+03 
c  k            0.70249E-02      25   0.87596E-03   0.36821E+01 0.72786E+03 
c  omega        0.15821E+03      42   0.19130E-03   0.23444E+10 0.10534E+04 
c  TempC        0.36851E+04      59   0.19454E-01   0.12065E+06 0.21199E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9138          62.209           4.035          4.1607
v  Velocity[Y]            -9.1156          7.4835       0.0013531      0.00095417
v  Velocity[Z]             -18.06          20.829        -0.28679         -0.1434
v  ǁVelocityǁ            0.006335          62.414          4.3981          4.2986
v  Pressure               -2245.8          37.577          14.673          22.879
v  k                   3.9697e-10          14.381           0.103         0.09339
v  omega               2.3799e-09      2.2902e+06          4835.4            1382
v  TempC                  -103.33          647.05           54.58          59.424
v  Density                0.39182          2.3158          1.1637          1.1795
v  TurbVisc            3.3632e-14       0.0022902      0.00014768      0.00021507
v  CourantNb                    0          33.654         0.75109         0.55195
v  FourierNb            0.0025024          4.6712         0.14102         0.18122
v  total_pressure           99079      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41576          2.3158          1.0995          1.1479


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0068951          33.802          0.8921         0.73317


 TIME FOR THE TIME STEP              284:        0.63945E+02

===============================================================


 INSTANT    0.264300000E-01   TIME STEP NUMBER             285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.214387858E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155843568E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51218E+02 0.10930E+02
   Friction velocity        uet   :  0.29924E-02 0.54842E+01
   Friction velocity        uk    :  0.16930E-01 0.20872E+01
   Dimensionless distance   yplus :  0.16677E+00 0.57861E+02
   Friction thermal sca.    tstar : -0.39614E+03 0.44902E+02
   Rough dim-less th. sca.  tplus :  0.12443E+00 0.13620E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     133013
   Nb of faces within the viscous sub-layer     :       9519
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        703 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21025E+00      33   0.26742E-01   0.32403E+02 0.11787E+03 
c  Velocity[X]                                      0.27409E+02 
c  Velocity[Y]                                      0.10791E+01 
c  Velocity[Z]                                      0.39142E+01 
c  Pressure     0.12680E-03     134   0.55332E-02   0.16387E+00 0.23896E+03 
c  k            0.70440E-02      25   0.86427E-03   0.36371E+01 0.72215E+03 
c  omega        0.16724E+03      42   0.16205E-03   0.20843E+10 0.99254E+03 
c  TempC        0.36927E+04      59   0.19474E-01   0.12135E+06 0.21219E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9051           65.71          4.0369          4.1634
v  Velocity[Y]            -9.0229          7.4507       0.0013666      0.00095001
v  Velocity[Z]            -18.307            20.9        -0.28899        -0.14441
v  ǁVelocityǁ           0.0069964          65.718          4.4018          4.3021
v  Pressure               -2264.2          38.512          15.425          23.601
v  k                    8.789e-09           14.64          0.1033        0.093692
v  omega               3.6959e-09      1.3436e+06          4839.7          1382.4
v  TempC                   -108.7          651.95          54.759          59.649
v  Density                0.38381          2.0798          1.1633           1.179
v  TurbVisc            2.4522e-15       0.0022905      0.00014826      0.00021587
v  CourantNb                    0          32.692         0.75175          0.5524
v  FourierNb            0.0025025          4.6712         0.14151         0.18188
v  total_pressure           99061      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41142          2.0798          1.0991          1.1475


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.005312          32.836         0.89327         0.73429


 TIME FOR THE TIME STEP              285:        0.64172E+02

===============================================================


 INSTANT    0.265300000E-01   TIME STEP NUMBER             286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.345139169E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845337E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53071E+02 0.11156E+02
   Friction velocity        uet   :  0.30419E-02 0.54465E+01
   Friction velocity        uk    :  0.11080E-01 0.21033E+01
   Dimensionless distance   yplus :  0.16119E+00 0.57722E+02
   Friction thermal sca.    tstar : -0.48726E+03 0.40199E+02
   Rough dim-less th. sca.  tplus :  0.12026E+00 0.13614E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132923
   Nb of faces within the viscous sub-layer     :       9559
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        729 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21036E+00      33   0.28140E-01   0.32876E+02 0.11859E+03 
c  Velocity[X]                                      0.27688E+02 
c  Velocity[Y]                                      0.10700E+01 
c  Velocity[Z]                                      0.41176E+01 
c  Pressure     0.12695E-03     129   0.56118E-02   0.16307E+00 0.23071E+03 
c  k            0.70575E-02      25   0.84509E-03   0.36094E+01 0.71822E+03 
c  omega        0.16097E+03      42   0.24110E-03   0.22541E+10 0.10303E+04 
c  TempC        0.37003E+04      58   0.19126E-01   0.12058E+06 0.21111E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8999          63.692          4.0388          4.1661
v  Velocity[Y]            -8.7746           7.458       0.0013972      0.00094328
v  Velocity[Z]            -18.705          21.013        -0.29122        -0.14543
v  ǁVelocityǁ            0.006806          63.943          4.4054          4.3057
v  Pressure               -2275.5          39.134          16.099          24.311
v  k                   4.0226e-09          14.646         0.10362        0.093992
v  omega               5.6989e-09      1.4144e+06          4844.7          1382.8
v  TempC                  -120.86          616.61          54.942          59.875
v  Density                0.38178          2.1477          1.1629          1.1786
v  TurbVisc            5.4303e-14       0.0022903      0.00014884      0.00021669
v  CourantNb                    0          34.599          0.7524         0.55285
v  FourierNb            0.0025026          4.6712         0.14202         0.18256
v  total_pressure           99050      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41263          2.1477          1.0987          1.1471


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0075067          34.746         0.89442         0.73542


 TIME FOR THE TIME STEP              286:        0.63568E+02

===============================================================


 INSTANT    0.266300000E-01   TIME STEP NUMBER             287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.132791323E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155845752E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51452E+02 0.11034E+02
   Friction velocity        uet   :  0.68012E-03 0.55618E+01
   Friction velocity        uk    :  0.11353E-01 0.21046E+01
   Dimensionless distance   yplus :  0.20761E+00 0.58142E+02
   Friction thermal sca.    tstar : -0.36145E+03 0.40809E+02
   Rough dim-less th. sca.  tplus :  0.15490E+00 0.13632E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132833
   Nb of faces within the viscous sub-layer     :       9566
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        744 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21044E+00      34   0.27377E-01   0.32860E+02 0.11843E+03 
c  Velocity[X]                                      0.27695E+02 
c  Velocity[Y]                                      0.10941E+01 
c  Velocity[Z]                                      0.40709E+01 
c  Pressure     0.12957E-03     128   0.57571E-02   0.16583E+00 0.20391E+03 
c  k            0.70663E-02      25   0.82948E-03   0.36111E+01 0.71732E+03 
c  omega        0.16150E+03      42   0.16339E-03   0.11509E+10 0.73703E+03 
c  TempC        0.37077E+04      59   0.19759E-01   0.11926E+06 0.20955E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.914          64.516          4.0407          4.1689
v  Velocity[Y]            -9.2074          7.5489       0.0014256      0.00093939
v  Velocity[Z]            -18.804          20.894        -0.29345        -0.14645
v  ǁVelocityǁ           0.0065914          64.772          4.4091          4.3093
v  Pressure               -2293.1          39.871          16.728          24.943
v  k                   8.4889e-10          14.768         0.10395         0.09429
v  omega               9.4093e-09      7.2774e+05          4847.4            1383
v  TempC                  -93.635          595.66          55.124            60.1
v  Density                0.39694          2.3191          1.1625          1.1782
v  TurbVisc            1.8711e-14       0.0022902      0.00014943      0.00021752
v  CourantNb                    0          34.114         0.75307         0.55331
v  FourierNb            0.0025027          4.6712         0.14253         0.18325
v  total_pressure           99032      1.0136e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41758          2.3191          1.0983          1.1467


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0065924          34.266         0.89561         0.73656


 TIME FOR THE TIME STEP              287:        0.64030E+02

===============================================================


 INSTANT    0.267300000E-01   TIME STEP NUMBER             288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.157991369E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155846857E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53626E+02 0.11253E+02
   Friction velocity        uet   :  0.27273E-02 0.56304E+01
   Friction velocity        uk    :  0.11513E-01 0.21121E+01
   Dimensionless distance   yplus :  0.16674E+00 0.57881E+02
   Friction thermal sca.    tstar : -0.33135E+03 0.39844E+02
   Rough dim-less th. sca.  tplus :  0.12441E+00 0.13621E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132811
   Nb of faces within the viscous sub-layer     :       9612
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        767 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21054E+00      34   0.27909E-01   0.32816E+02 0.11821E+03 
c  Velocity[X]                                      0.27505E+02 
c  Velocity[Y]                                      0.11276E+01 
c  Velocity[Z]                                      0.41842E+01 
c  Pressure     0.13010E-03     124   0.57373E-02   0.16572E+00 0.15616E+03 
c  k            0.70749E-02      25   0.81203E-03   0.36245E+01 0.71758E+03 
c  omega        0.15954E+03      42   0.14818E-03   0.94133E+09 0.66596E+03 
c  TempC        0.37150E+04      59   0.19668E-01   0.11958E+06 0.20943E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8984          68.815          4.0426          4.1716
v  Velocity[Y]            -9.2244          7.5576       0.0014428      0.00093036
v  Velocity[Z]            -18.753          20.793         -0.2957        -0.14749
v  ǁVelocityǁ           0.0054883          68.821          4.4127          4.3128
v  Pressure               -2313.4           40.44          17.173          25.418
v  k                   3.3796e-09          14.818          0.1043        0.094586
v  omega               1.5219e-08      6.7027e+05          4851.6          1383.4
v  TempC                  -109.98          608.27          55.309          60.326
v  Density                0.40651          1.9674          1.1621          1.1778
v  TurbVisc            3.5568e-15       0.0022901      0.00015001      0.00021834
v  CourantNb                    0           32.67         0.75371         0.55376
v  FourierNb            0.0025028          4.6712         0.14304         0.18393
v  total_pressure           99012      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41566          1.9674           1.098          1.1464


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.007118          32.816         0.89675         0.73768


 TIME FOR THE TIME STEP              288:        0.63790E+02

===============================================================


 INSTANT    0.268300000E-01   TIME STEP NUMBER             289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.828190573E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155848827E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51584E+02 0.11237E+02
   Friction velocity        uet   :  0.26375E-02 0.56410E+01
   Friction velocity        uk    :  0.12868E-01 0.21165E+01
   Dimensionless distance   yplus :  0.16798E+00 0.58141E+02
   Friction thermal sca.    tstar : -0.32066E+03 0.42276E+02
   Rough dim-less th. sca.  tplus :  0.12533E+00 0.13632E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132731
   Nb of faces within the viscous sub-layer     :       9608
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        781 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21062E+00      34   0.27073E-01   0.32919E+02 0.11826E+03 
c  Velocity[X]                                      0.27709E+02 
c  Velocity[Y]                                      0.11041E+01 
c  Velocity[Z]                                      0.41057E+01 
c  Pressure     0.12802E-03     127   0.55367E-02   0.16251E+00 0.14018E+03 
c  k            0.70827E-02      25   0.80854E-03   0.36228E+01 0.71636E+03 
c  omega        0.15976E+03      42   0.12842E-03   0.77361E+09 0.60327E+03 
c  TempC        0.37221E+04      57   0.19372E-01   0.11993E+06 0.20934E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9141           65.61          4.0445          4.1743
v  Velocity[Y]            -9.4335          7.5323       0.0014217      0.00091593
v  Velocity[Z]            -18.916          21.006        -0.29801        -0.14853
v  ǁVelocityǁ           0.0057746          65.863          4.4164          4.3164
v  Pressure               -2328.1          40.904          17.603          25.846
v  k                    1.438e-08          14.962         0.10465        0.094882
v  omega               2.6864e-08      5.8577e+05          4854.9          1383.7
v  TempC                  -123.73          605.21          55.496          60.551
v  Density                 0.4007          2.1644          1.1617          1.1774
v  TurbVisc             3.594e-14         0.00229      0.00015057      0.00021915
v  CourantNb                    0          34.561         0.75438         0.55421
v  FourierNb             0.002503          4.6712         0.14353          0.1846
v  total_pressure           98997      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41552          2.1644          1.0976           1.146


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0056753           34.71         0.89791         0.73881


 TIME FOR THE TIME STEP              289:        0.63807E+02

===============================================================


 INSTANT    0.269300000E-01   TIME STEP NUMBER             290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.566757786E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155850545E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53648E+02 0.11458E+02
   Friction velocity        uet   :  0.34527E-02 0.57607E+01
   Friction velocity        uk    :  0.14936E-01 0.21257E+01
   Dimensionless distance   yplus :  0.16694E+00 0.57808E+02
   Friction thermal sca.    tstar : -0.50062E+03 0.44391E+02
   Rough dim-less th. sca.  tplus :  0.12456E+00 0.13618E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132721
   Nb of faces within the viscous sub-layer     :       9639
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        800 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21073E+00      34   0.27364E-01   0.32659E+02 0.11766E+03 
c  Velocity[X]                                      0.27381E+02 
c  Velocity[Y]                                      0.10933E+01 
c  Velocity[Z]                                      0.41849E+01 
c  Pressure     0.12678E-03     123   0.53936E-02   0.16010E+00 0.91669E+02 
c  k            0.70892E-02      25   0.82354E-03   0.36150E+01 0.71450E+03 
c  omega        0.16005E+03      42   0.20616E-03   0.35536E+10 0.12830E+04 
c  TempC        0.37292E+04      58   0.18961E-01   0.12051E+06 0.20945E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0094          64.449          4.0464           4.177
v  Velocity[Y]             -9.428          7.5825       0.0014283      0.00090562
v  Velocity[Z]            -18.139          21.073        -0.30027        -0.14957
v  ǁVelocityǁ           0.0078348          64.689          4.4201            4.32
v  Pressure               -2346.2           41.45          17.818          26.091
v  k                   1.6592e-08          14.919           0.105        0.095179
v  omega               4.9552e-08      1.4359e+06          4860.8          1384.3
v  TempC                  -103.23          602.92          55.684          60.777
v  Density                0.40209          2.3637          1.1613          1.1769
v  TurbVisc            6.0246e-14       0.0022898      0.00015114      0.00021997
v  CourantNb                    0          35.173         0.75503         0.55467
v  FourierNb            0.0025031          4.6712         0.14402         0.18527
v  total_pressure           98979      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41862          2.3637          1.0972          1.1456


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0059023          35.327         0.89905         0.73994


 TIME FOR THE TIME STEP              290:        0.63469E+02

===============================================================


 INSTANT    0.270300000E-01   TIME STEP NUMBER             291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.159882929E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852709E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51995E+02 0.11387E+02
   Friction velocity        uet   :  0.38334E-02 0.56594E+01
   Friction velocity        uk    :  0.10126E-01 0.21242E+01
   Dimensionless distance   yplus :  0.11228E+00 0.58554E+02
   Friction thermal sca.    tstar : -0.36204E+03 0.44866E+02
   Rough dim-less th. sca.  tplus :  0.83776E-01 0.13648E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132660
   Nb of faces within the viscous sub-layer     :       9671
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        821 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21083E+00      34   0.28488E-01   0.33375E+02 0.11881E+03 
c  Velocity[X]                                      0.28061E+02 
c  Velocity[Y]                                      0.11154E+01 
c  Velocity[Z]                                      0.41982E+01 
c  Pressure     0.12853E-03     125   0.54638E-02   0.16130E+00 0.83617E+02 
c  k            0.70972E-02      25   0.83506E-03   0.36109E+01 0.71294E+03 
c  omega        0.17859E+03      42   0.13179E-03   0.13116E+10 0.78232E+03 
c  TempC        0.37362E+04      58   0.19332E-01   0.11992E+06 0.20853E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1012          68.442          4.0483          4.1797
v  Velocity[Y]            -9.3748          7.6504       0.0013969      0.00088597
v  Velocity[Z]            -18.607          21.036        -0.30262        -0.15062
v  ǁVelocityǁ           0.0065801          68.458          4.4238          4.3235
v  Pressure                 -2366          41.406          18.014          26.277
v  k                   1.3765e-08          15.171         0.10537        0.095478
v  omega               9.3769e-08      7.4238e+05          4863.7          1384.6
v  TempC                  -109.67          598.32          55.874          61.002
v  Density                0.40315          2.0785          1.1609          1.1765
v  TurbVisc            1.0313e-13       0.0022902       0.0001517      0.00022077
v  CourantNb                    0          33.307         0.75569         0.55513
v  FourierNb            0.0025032          4.6712          0.1445         0.18592
v  total_pressure           98959      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41689          2.0785          1.0968          1.1452


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.008283          33.456         0.90018         0.74105


 TIME FOR THE TIME STEP              291:        0.63467E+02

===============================================================


 INSTANT    0.271300000E-01   TIME STEP NUMBER             292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.829755040E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155853736E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54017E+02 0.11572E+02
   Friction velocity        uet   :  0.25946E-02 0.56419E+01
   Friction velocity        uk    :  0.11640E-01 0.21398E+01
   Dimensionless distance   yplus :  0.16745E+00 0.58533E+02
   Friction thermal sca.    tstar : -0.29135E+03 0.43724E+02
   Rough dim-less th. sca.  tplus :  0.12494E+00 0.13648E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132578
   Nb of faces within the viscous sub-layer     :       9724
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        837 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21092E+00      34   0.27805E-01   0.33624E+02 0.11912E+03 
c  Velocity[X]                                      0.28212E+02 
c  Velocity[Y]                                      0.11177E+01 
c  Velocity[Z]                                      0.42944E+01 
c  Pressure     0.12873E-03     124   0.55026E-02   0.16074E+00 0.87289E+02 
c  k            0.71048E-02      25   0.83706E-03   0.36195E+01 0.71260E+03 
c  omega        0.16215E+03      42   0.13063E-03   0.12800E+10 0.77178E+03 
c  TempC        0.37431E+04      59   0.19326E-01   0.12000E+06 0.20822E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1894          66.749          4.0502          4.1824
v  Velocity[Y]            -9.0872          7.6279       0.0014065      0.00087446
v  Velocity[Z]            -18.811          21.286        -0.30494        -0.15167
v  ǁVelocityǁ           0.0055218          67.021          4.4276          4.3271
v  Pressure               -2378.4          42.173          18.253           26.51
v  k                   1.8078e-08          15.161         0.10573        0.095778
v  omega               1.9094e-07      1.1792e+06          4868.2            1385
v  TempC                  -122.34          605.18          56.065          61.228
v  Density                0.40527          2.1604          1.1605          1.1761
v  TurbVisc            5.8085e-14       0.0022904      0.00015225      0.00022157
v  CourantNb                    0          35.403         0.75636         0.55559
v  FourierNb            0.0025033          4.6712         0.14497         0.18657
v  total_pressure           98947      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41845          2.1604          1.0964          1.1448


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010077          35.554         0.90133         0.74216


 TIME FOR THE TIME STEP              292:        0.63758E+02

===============================================================


 INSTANT    0.272300000E-01   TIME STEP NUMBER             293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.224210639E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852468E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52315E+02 0.11548E+02
   Friction velocity        uet   :  0.15826E-02 0.58667E+01
   Friction velocity        uk    :  0.13439E-01 0.21407E+01
   Dimensionless distance   yplus :  0.15050E+00 0.59053E+02
   Friction thermal sca.    tstar : -0.38659E+03 0.44178E+02
   Rough dim-less th. sca.  tplus :  0.11229E+00 0.13669E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132522
   Nb of faces within the viscous sub-layer     :       9754
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        861 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21101E+00      34   0.27840E-01   0.33169E+02 0.11818E+03 
c  Velocity[X]                                      0.27663E+02 
c  Velocity[Y]                                      0.11243E+01 
c  Velocity[Z]                                      0.43813E+01 
c  Pressure     0.12926E-03     125   0.55556E-02   0.16059E+00 0.73585E+02 
c  k            0.71137E-02      25   0.83198E-03   0.36155E+01 0.71098E+03 
c  omega        0.16448E+03      42   0.20844E-03   0.16122E+11 0.26455E+04 
c  TempC        0.37500E+04      59   0.18741E-01   0.12142E+06 0.20906E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3128          67.502          4.0521          4.1851
v  Velocity[Y]            -9.1293          7.6275       0.0013901      0.00086513
v  Velocity[Z]             -18.41          21.319        -0.30731        -0.15273
v  ǁVelocityǁ           0.0047012          67.778          4.4313          4.3307
v  Pressure               -2392.5          42.698          18.389          26.651
v  k                   3.8655e-11          15.338          0.1061        0.096079
v  omega               3.7156e-07      6.6763e+06          4876.4          1385.6
v  TempC                  -106.47          609.74          56.257          61.453
v  Density                0.40211           2.342          1.1601          1.1757
v  TurbVisc            8.7316e-14       0.0022902       0.0001528      0.00022238
v  CourantNb                    0           35.44         0.75702         0.55604
v  FourierNb            0.0025034          4.6712         0.14544         0.18722
v  total_pressure           98932      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41311           2.342           1.096          1.1444


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010843          35.597         0.90246         0.74327


 TIME FOR THE TIME STEP              293:        0.63567E+02

===============================================================


 INSTANT    0.273300000E-01   TIME STEP NUMBER             294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.163009354E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855313E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54471E+02 0.11696E+02
   Friction velocity        uet   :  0.28153E-02 0.58352E+01
   Friction velocity        uk    :  0.11216E-01 0.21525E+01
   Dimensionless distance   yplus :  0.13991E+00 0.59013E+02
   Friction thermal sca.    tstar : -0.50912E+03 0.45207E+02
   Rough dim-less th. sca.  tplus :  0.10439E+00 0.13667E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132425
   Nb of faces within the viscous sub-layer     :       9815
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        882 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21112E+00      34   0.29011E-01   0.33797E+02 0.11916E+03 
c  Velocity[X]                                      0.28231E+02 
c  Velocity[Y]                                      0.11389E+01 
c  Velocity[Z]                                      0.44273E+01 
c  Pressure     0.13178E-03     121   0.54836E-02   0.16281E+00 0.80737E+02 
c  k            0.71204E-02      25   0.82017E-03   0.36085E+01 0.70909E+03 
c  omega        0.53288E+03      38   0.42608E-04   0.43836E+10 0.14134E+04 
c  TempC        0.37568E+04      59   0.19027E-01   0.12035E+06 0.20774E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.428          70.509           4.054          4.1878
v  Velocity[Y]            -9.7376           7.777        0.001406      0.00086692
v  Velocity[Z]            -18.899          21.293        -0.30966        -0.15379
v  ǁVelocityǁ           0.0047315          70.518           4.435          4.3342
v  Pressure               -2410.7          43.984          18.576          26.859
v  k                   1.1663e-08          15.483         0.10647         0.09638
v  omega               7.7148e-07      3.3615e+06          4879.7            1386
v  TempC                  -115.37          597.47           56.45          61.679
v  Density                0.40003          2.1189          1.1596          1.1753
v  TurbVisc            1.8672e-16         0.00229      0.00015333      0.00022317
v  CourantNb                    0          33.814         0.75768          0.5565
v  FourierNb            0.0025035          4.6712          0.1459         0.18786
v  total_pressure           98914      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4153           1.989          1.0956           1.144


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010814          33.966         0.90358         0.74437


 TIME FOR THE TIME STEP              294:        0.63262E+02

===============================================================


 INSTANT    0.274300000E-01   TIME STEP NUMBER             295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.449679195E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155853138E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52361E+02 0.11715E+02
   Friction velocity        uet   :  0.18071E-02 0.57403E+01
   Friction velocity        uk    :  0.14057E-01 0.21669E+01
   Dimensionless distance   yplus :  0.15242E+00 0.59730E+02
   Friction thermal sca.    tstar : -0.48404E+03 0.45172E+02
   Rough dim-less th. sca.  tplus :  0.11372E+00 0.13696E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132362
   Nb of faces within the viscous sub-layer     :       9826
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        894 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21120E+00      35   0.28917E-01   0.33646E+02 0.11876E+03 
c  Velocity[X]                                      0.28084E+02 
c  Velocity[Y]                                      0.11860E+01 
c  Velocity[Z]                                      0.43761E+01 
c  Pressure     0.13202E-03     124   0.54519E-02   0.16236E+00 0.74177E+02 
c  k            0.71280E-02      25   0.81093E-03   0.36223E+01 0.70927E+03 
c  omega        0.20805E+03      41   0.12692E-03   0.21330E+10 0.99013E+03 
c  TempC        0.37636E+04      58   0.19164E-01   0.12002E+06 0.20707E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5555          67.246          4.0559          4.1906
v  Velocity[Y]            -9.3914          7.7685        0.001423      0.00086224
v  Velocity[Z]             -19.13          21.304        -0.31205        -0.15485
v  ǁVelocityǁ            0.004811          67.558          4.4388          4.3377
v  Pressure               -2425.9          44.565          18.691          26.995
v  k                   2.5692e-09           15.67         0.10685        0.096679
v  omega               7.1235e-07      1.7037e+06            4884          1386.5
v  TempC                  -124.53          598.15          56.645          61.906
v  Density                0.40567          2.2385          1.1592          1.1748
v  TurbVisc            7.2357e-14       0.0022899      0.00015389        0.000224
v  CourantNb                    0          36.099         0.75835         0.55696
v  FourierNb            0.0025036          4.6712         0.14637         0.18853
v  total_pressure           98899      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41372          2.1769          1.0953          1.1436


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0092873          36.252         0.90473         0.74549


 TIME FOR THE TIME STEP              295:        0.63801E+02

===============================================================


 INSTANT    0.275300000E-01   TIME STEP NUMBER             296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.200148297E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855071E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54683E+02 0.11853E+02
   Friction velocity        uet   :  0.16607E-02 0.59203E+01
   Friction velocity        uk    :  0.14575E-01 0.21737E+01
   Dimensionless distance   yplus :  0.15219E+00 0.59188E+02
   Friction thermal sca.    tstar : -0.35287E+03 0.45658E+02
   Rough dim-less th. sca.  tplus :  0.11355E+00 0.13674E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132341
   Nb of faces within the viscous sub-layer     :       9874
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        910 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21131E+00      35   0.29642E-01   0.33631E+02 0.11860E+03 
c  Velocity[X]                                      0.27999E+02 
c  Velocity[Y]                                      0.11640E+01 
c  Velocity[Z]                                      0.44676E+01 
c  Pressure     0.12955E-03     124   0.54163E-02   0.15855E+00 0.81040E+02 
c  k            0.71367E-02      25   0.79539E-03   0.36297E+01 0.70889E+03 
c  omega        0.16685E+03      42   0.18151E-03   0.17374E+10 0.89316E+03 
c  TempC        0.37701E+04      60   0.19127E-01   0.12092E+06 0.20745E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6659          68.569          4.0578          4.1933
v  Velocity[Y]             -9.425          7.7474       0.0014274      0.00085215
v  Velocity[Z]            -18.864           21.28        -0.31447        -0.15592
v  ǁVelocityǁ           0.0057638           68.88          4.4426          4.3413
v  Pressure               -2439.9          44.996          18.922          27.218
v  k                   2.5719e-09          15.825         0.10722        0.096976
v  omega               2.4589e-07      1.0273e+06          4890.1          1387.1
v  TempC                  -128.13          590.85          56.841          62.131
v  Density                0.40535          2.3765          1.1588          1.1744
v  TurbVisc            1.2413e-14       0.0022899      0.00015443       0.0002248
v  CourantNb                    0          36.092         0.75903         0.55742
v  FourierNb            0.0025037          4.6712         0.14683         0.18918
v  total_pressure           98885      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41171          2.3765          1.0949          1.1432


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0064188          36.252         0.90586          0.7466


 TIME FOR THE TIME STEP              296:        0.63682E+02

===============================================================


 INSTANT    0.276300000E-01   TIME STEP NUMBER             297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.253103136E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852584E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52925E+02 0.11764E+02
   Friction velocity        uet   :  0.48583E-03 0.59470E+01
   Friction velocity        uk    :  0.14747E-01 0.21852E+01
   Dimensionless distance   yplus :  0.15464E+00 0.59457E+02
   Friction thermal sca.    tstar : -0.32314E+03 0.44717E+02
   Rough dim-less th. sca.  tplus :  0.11538E+00 0.13685E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132256
   Nb of faces within the viscous sub-layer     :       9909
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        925 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21139E+00      35   0.27870E-01   0.33881E+02 0.11890E+03 
c  Velocity[X]                                      0.28255E+02 
c  Velocity[Y]                                      0.11320E+01 
c  Velocity[Z]                                      0.44942E+01 
c  Pressure     0.12834E-03     122   0.52958E-02   0.15616E+00 0.10108E+03 
c  k            0.71485E-02      25   0.78526E-03   0.36378E+01 0.70860E+03 
c  omega        0.16382E+03      42   0.19499E-03   0.32950E+10 0.12239E+04 
c  TempC        0.37766E+04      60   0.18948E-01   0.12059E+06 0.20679E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7813          72.338          4.0597           4.196
v  Velocity[Y]            -9.4391          7.7604       0.0014044      0.00084321
v  Velocity[Z]            -19.176          21.292         -0.3169        -0.15698
v  ǁVelocityǁ           0.0063209          72.346          4.4464          4.3448
v  Pressure               -2461.3           44.95           19.19          27.506
v  k                   1.1847e-08          15.966         0.10759        0.097274
v  omega               8.8807e-08      2.1912e+06          4895.4          1387.7
v  TempC                  -131.61          592.81          57.039          62.357
v  Density                0.40878          2.4355          1.1584           1.174
v  TurbVisc            1.2549e-14       0.0022899      0.00015497       0.0002256
v  CourantNb                    0          34.704          0.7597         0.55788
v  FourierNb            0.0025038          4.6712         0.14729         0.18982
v  total_pressure           98864      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41256          2.0769          1.0945          1.1428


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.008053           34.86         0.90699          0.7477


 TIME FOR THE TIME STEP              297:        0.63874E+02

===============================================================


 INSTANT    0.277300000E-01   TIME STEP NUMBER             298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.452098816E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852593E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54857E+02 0.12020E+02
   Friction velocity        uet   :  0.14671E-02 0.58343E+01
   Friction velocity        uk    :  0.15688E-01 0.22115E+01
   Dimensionless distance   yplus :  0.18616E+00 0.59612E+02
   Friction thermal sca.    tstar : -0.28932E+03 0.42892E+02
   Rough dim-less th. sca.  tplus :  0.13889E+00 0.13691E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132128
   Nb of faces within the viscous sub-layer     :       9919
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        944 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21148E+00      35   0.28938E-01   0.33812E+02 0.11865E+03 
c  Velocity[X]                                      0.28106E+02 
c  Velocity[Y]                                      0.11278E+01 
c  Velocity[Z]                                      0.45782E+01 
c  Pressure     0.13029E-03     122   0.53590E-02   0.15766E+00 0.80129E+02 
c  k            0.71630E-02      25   0.78952E-03   0.36594E+01 0.70961E+03 
c  omega        0.18895E+03      42   0.13498E-03   0.14673E+10 0.81906E+03 
c  TempC        0.37832E+04      59   0.18634E-01   0.12097E+06 0.20674E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8771          68.464          4.0616          4.1987
v  Velocity[Y]            -9.1354          7.6943       0.0014274      0.00084601
v  Velocity[Z]            -18.982          21.402        -0.31937        -0.15805
v  ǁVelocityǁ           0.0031437          68.769          4.4502          4.3483
v  Pressure               -2476.4          44.353          19.355          27.704
v  k                   1.0603e-08           15.95         0.10796        0.097571
v  omega               3.3751e-08       1.119e+06          4898.8          1388.1
v  TempC                  -135.46          597.33          57.238          62.583
v  Density                0.40785          2.4953           1.158          1.1736
v  TurbVisc            5.7245e-14       0.0022898      0.00015554      0.00022643
v  CourantNb                    0          36.281         0.76037         0.55833
v  FourierNb            0.0025039          4.6712         0.14776         0.19049
v  total_pressure           98849      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41385          2.1941          1.0941          1.1424


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0086287          36.438         0.90813         0.74882


 TIME FOR THE TIME STEP              298:        0.63546E+02

===============================================================


 INSTANT    0.278300000E-01   TIME STEP NUMBER             299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.163991821E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155853902E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53190E+02 0.11937E+02
   Friction velocity        uet   :  0.15697E-02 0.59649E+01
   Friction velocity        uk    :  0.75893E-02 0.22123E+01
   Dimensionless distance   yplus :  0.80178E-01 0.60173E+02
   Friction thermal sca.    tstar : -0.28041E+03 0.42351E+02
   Rough dim-less th. sca.  tplus :  0.59822E-01 0.13713E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132083
   Nb of faces within the viscous sub-layer     :       9949
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        965 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21158E+00      35   0.29434E-01   0.34263E+02 0.11931E+03 
c  Velocity[X]                                      0.28494E+02 
c  Velocity[Y]                                      0.11826E+01 
c  Velocity[Z]                                      0.45869E+01 
c  Pressure     0.13158E-03     123   0.54660E-02   0.15823E+00 0.62435E+02 
c  k            0.71790E-02      25   0.79782E-03   0.36827E+01 0.71077E+03 
c  omega        0.16471E+03      42   0.21564E-03   0.12679E+10 0.76066E+03 
c  TempC        0.37897E+04      60   0.18627E-01   0.12006E+06 0.20558E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9826          68.641          4.0635          4.2014
v  Velocity[Y]             -9.153          7.7196       0.0014284      0.00084781
v  Velocity[Z]            -19.314          21.575        -0.32187        -0.15913
v  ǁVelocityǁ           0.0043719          68.981           4.454          4.3519
v  Pressure               -2493.1           45.16          19.372          27.749
v  k                   2.8273e-09          16.323         0.10832        0.097869
v  omega               1.3674e-08      1.0091e+06          4903.2          1388.7
v  TempC                  -138.99          602.64          57.436          62.808
v  Density                0.40574          2.5651          1.1576          1.1732
v  TurbVisc            5.1724e-14       0.0022898      0.00015609      0.00022725
v  CourantNb                    0          36.532         0.76106         0.55879
v  FourierNb             0.002504          4.6712         0.14823         0.19114
v  total_pressure           98832      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41422          2.3771          1.0937           1.142


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0060618          36.694         0.90928         0.74993


 TIME FOR THE TIME STEP              299:        0.63888E+02

===============================================================


 INSTANT    0.279300000E-01   TIME STEP NUMBER             300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.399112141E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155857106E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55329E+02 0.12145E+02
   Friction velocity        uet   :  0.78194E-03 0.59161E+01
   Friction velocity        uk    :  0.12810E-01 0.22355E+01
   Dimensionless distance   yplus :  0.13974E+00 0.59997E+02
   Friction thermal sca.    tstar : -0.69092E+03 0.41588E+02
   Rough dim-less th. sca.  tplus :  0.10426E+00 0.13706E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     132025
   Nb of faces within the viscous sub-layer     :      10001
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        974 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21167E+00      35   0.29475E-01   0.34552E+02 0.11967E+03 
c  Velocity[X]                                      0.28694E+02 
c  Velocity[Y]                                      0.12002E+01 
c  Velocity[Z]                                      0.46579E+01 
c  Pressure     0.13166E-03     121   0.53833E-02   0.15746E+00 0.55042E+02 
c  k            0.71936E-02      25   0.80413E-03   0.37052E+01 0.71181E+03 
c  omega        0.16416E+03      42   0.27698E-03   0.31949E+10 0.12003E+04 
c  TempC        0.37963E+04      59   0.19048E-01   0.11997E+06 0.20513E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1113          73.406          4.0654          4.2041
v  Velocity[Y]            -9.2431          8.0471       0.0014551      0.00084863
v  Velocity[Z]            -19.437          21.439        -0.32437         -0.1602
v  ǁVelocityǁ           0.0071489          73.418          4.4579          4.3554
v  Pressure               -2511.8          45.102          19.455          27.821
v  k                   6.3636e-09          16.553          0.1087        0.098167
v  omega               5.7437e-09      1.8917e+06          4909.6          1389.4
v  TempC                   -142.4          599.66          57.636          63.034
v  Density                0.40328          2.6325          1.1571          1.1727
v  TurbVisc            1.1947e-14       0.0022902      0.00015664      0.00022807
v  CourantNb                    0          35.272         0.76174         0.55925
v  FourierNb            0.0025042          4.6712          0.1487         0.19179
v  total_pressure           98813      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4152          1.9401          1.0933          1.1416


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.006141           35.43         0.91043         0.75105


 TIME FOR THE TIME STEP              300:        0.63477E+02

===============================================================


 INSTANT    0.280300000E-01   TIME STEP NUMBER             301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.118074843E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855060E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53557E+02 0.12090E+02
   Friction velocity        uet   :  0.14534E-02 0.59521E+01
   Friction velocity        uk    :  0.89930E-02 0.22494E+01
   Dimensionless distance   yplus :  0.10596E+00 0.60330E+02
   Friction thermal sca.    tstar : -0.34342E+03 0.42000E+02
   Rough dim-less th. sca.  tplus :  0.79055E-01 0.13720E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131879
   Nb of faces within the viscous sub-layer     :      10027
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for        985 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21177E+00      35   0.29843E-01   0.34450E+02 0.11936E+03 
c  Velocity[X]                                      0.28579E+02 
c  Velocity[Y]                                      0.11860E+01 
c  Velocity[Z]                                      0.46849E+01 
c  Pressure     0.12940E-03     123   0.53401E-02   0.15393E+00 0.63375E+02 
c  k            0.72070E-02      25   0.80095E-03   0.36946E+01 0.70957E+03 
c  omega        0.18504E+03      42   0.15109E-03   0.15051E+10 0.82592E+03 
c  TempC        0.38027E+04      59   0.18995E-01   0.12169E+06 0.20622E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2385          70.861          4.0673          4.2069
v  Velocity[Y]            -9.3014          8.2632       0.0014646       0.0008509
v  Velocity[Z]            -19.109           21.58         -0.3269        -0.16127
v  ǁVelocityǁ           0.0073577          71.216          4.4617          4.3589
v  Pressure               -2523.4          45.561          19.553          27.935
v  k                   2.3708e-08          16.653         0.10908        0.098469
v  omega               9.8095e-10      1.1215e+06          4913.5          1389.9
v  TempC                  -146.17          598.73          57.836           63.26
v  Density                0.40465          2.7012          1.1567          1.1723
v  TurbVisc            4.2402e-14       0.0022905      0.00015717      0.00022886
v  CourantNb                    0          36.938         0.76244         0.55971
v  FourierNb            0.0025043          4.6712         0.14915         0.19244
v  total_pressure           98802      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41587          2.1701          1.0929          1.1412


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0084235          37.098         0.91159         0.75214


 TIME FOR THE TIME STEP              301:        0.63436E+02

===============================================================


 INSTANT    0.281300000E-01   TIME STEP NUMBER             302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.108677632E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855527E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55992E+02 0.12260E+02
   Friction velocity        uet   :  0.21665E-02 0.60994E+01
   Friction velocity        uk    :  0.12746E-01 0.22580E+01
   Dimensionless distance   yplus :  0.15471E+00 0.59984E+02
   Friction thermal sca.    tstar : -0.28237E+03 0.41790E+02
   Rough dim-less th. sca.  tplus :  0.11543E+00 0.13706E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131840
   Nb of faces within the viscous sub-layer     :      10036
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1000 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21187E+00      35   0.30307E-01   0.34263E+02 0.11891E+03 
c  Velocity[X]                                      0.28413E+02 
c  Velocity[Y]                                      0.11884E+01 
c  Velocity[Z]                                      0.46613E+01 
c  Pressure     0.13094E-03     122   0.51992E-02   0.15495E+00 0.61760E+02 
c  k            0.72137E-02      25   0.79119E-03   0.36721E+01 0.70614E+03 
c  omega        0.16629E+03      42   0.13498E-03   0.83458E+09 0.61532E+03 
c  TempC        0.38092E+04      59   0.18382E-01   0.12209E+06 0.20618E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3589          70.921          4.0692          4.2096
v  Velocity[Y]            -9.5482          8.3462       0.0015023      0.00085903
v  Velocity[Z]            -19.472          21.774        -0.32942        -0.16235
v  ǁVelocityǁ           0.0053701           71.28          4.4655          4.3624
v  Pressure                 -2538          45.793          19.669          28.055
v  k                   4.3601e-09          17.113         0.10948        0.098773
v  omega               2.0076e-10      5.8267e+05          4917.8          1390.5
v  TempC                  -148.78          597.89          58.037          63.485
v  Density                0.40508          2.7814          1.1563          1.1719
v  TurbVisc            1.2242e-13       0.0022903       0.0001577      0.00022966
v  CourantNb                    0          36.939         0.76312         0.56016
v  FourierNb            0.0025044          4.6712         0.14961         0.19308
v  total_pressure           98787      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41754          2.3746          1.0925          1.1408


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0058883          37.104         0.91273         0.75324


 TIME FOR THE TIME STEP              302:        0.63139E+02

===============================================================


 INSTANT    0.282300000E-01   TIME STEP NUMBER             303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.127983458E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155854667E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54409E+02 0.12253E+02
   Friction velocity        uet   :  0.82687E-03 0.60786E+01
   Friction velocity        uk    :  0.11097E-01 0.22869E+01
   Dimensionless distance   yplus :  0.13466E+00 0.60670E+02
   Friction thermal sca.    tstar : -0.27833E+03 0.40002E+02
   Rough dim-less th. sca.  tplus :  0.10047E+00 0.13733E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131748
   Nb of faces within the viscous sub-layer     :      10041
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1008 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21194E+00      35   0.29039E-01   0.34951E+02 0.11996E+03 
c  Velocity[X]                                      0.28943E+02 
c  Velocity[Y]                                      0.11966E+01 
c  Velocity[Z]                                      0.48114E+01 
c  Pressure     0.13302E-03     121   0.53265E-02   0.15651E+00 0.65263E+02 
c  k            0.72167E-02      25   0.78301E-03   0.36680E+01 0.70455E+03 
c  omega        0.98915E+06      16   0.25665E-07   0.12911E+10 0.76376E+03 
c  TempC        0.38157E+04      60   0.18765E-01   0.12115E+06 0.20501E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4834          73.949          4.0712          4.2123
v  Velocity[Y]            -9.4298            8.37       0.0015003      0.00085998
v  Velocity[Z]            -19.674          21.997        -0.33199        -0.16344
v  ǁVelocityǁ           0.0024345          73.957          4.4694          4.3659
v  Pressure               -2561.3           46.22          19.646          28.077
v  k                   2.4212e-08          17.514         0.10989        0.099075
v  omega               4.7532e-11      1.0428e+06          4922.4          1391.1
v  TempC                   -115.8          600.81          58.241          63.712
v  Density                0.40547          2.8397          1.1559          1.1715
v  TurbVisc            1.2444e-14       0.0022902      0.00015825      0.00023048
v  CourantNb                    0          35.746          0.7638         0.56062
v  FourierNb            0.0025045          4.6712         0.15008         0.19373
v  total_pressure           98764      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41041          2.1066          1.0921          1.1404


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0088138          35.907         0.91388         0.75435


 TIME FOR THE TIME STEP              303:        0.61930E+02

===============================================================


 INSTANT    0.283300000E-01   TIME STEP NUMBER             304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.292520211E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856705E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56138E+02 0.12415E+02
   Friction velocity        uet   :  0.92116E-03 0.59536E+01
   Friction velocity        uk    :  0.13937E-01 0.23106E+01
   Dimensionless distance   yplus :  0.16498E+00 0.60457E+02
   Friction thermal sca.    tstar : -0.33159E+03 0.38752E+02
   Rough dim-less th. sca.  tplus :  0.12309E+00 0.13725E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131647
   Nb of faces within the viscous sub-layer     :      10080
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1031 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21203E+00      35   0.29786E-01   0.34265E+02 0.11865E+03 
c  Velocity[X]                                      0.28265E+02 
c  Velocity[Y]                                      0.11682E+01 
c  Velocity[Z]                                      0.48317E+01 
c  Pressure     0.13150E-03     122   0.51148E-02   0.15349E+00 0.53911E+02 
c  k            0.72183E-02      25   0.77606E-03   0.36869E+01 0.70526E+03 
c  omega        0.16564E+03      42   0.27479E-03   0.12949E+10 0.76387E+03 
c  TempC        0.38219E+04      59   0.18926E-01   0.12057E+06 0.20415E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5677          71.073          4.0731           4.215
v  Velocity[Y]            -9.5271          8.4419       0.0015588      0.00087584
v  Velocity[Z]             -19.77          21.825        -0.33463        -0.16453
v  ǁVelocityǁ           0.0028616          71.455          4.4734          4.3694
v  Pressure               -2578.8          45.312          19.721          28.142
v  k                    2.232e-08          17.394         0.11031        0.099375
v  omega               1.2523e-11      9.1124e+05          4927.4          1391.8
v  TempC                  -124.56           589.4          58.449          63.938
v  Density                0.40412          2.2446          1.1554          1.1711
v  TurbVisc            1.0988e-13       0.0022901      0.00015878      0.00023129
v  CourantNb                    0          37.593         0.76451         0.56108
v  FourierNb            0.0025046          4.6712         0.15055         0.19439
v  total_pressure           98746      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41017          2.1858          1.0916            1.14


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011794          37.755         0.91506         0.75547


 TIME FOR THE TIME STEP              304:        0.63376E+02

===============================================================


 INSTANT    0.284300000E-01   TIME STEP NUMBER             305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.152042898E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855273E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54447E+02 0.12296E+02
   Friction velocity        uet   :  0.50595E-03 0.60548E+01
   Friction velocity        uk    :  0.10754E-01 0.23041E+01
   Dimensionless distance   yplus :  0.16705E+00 0.60527E+02
   Friction thermal sca.    tstar : -0.59216E+03 0.39125E+02
   Rough dim-less th. sca.  tplus :  0.12464E+00 0.13727E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131542
   Nb of faces within the viscous sub-layer     :      10080
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1045 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21213E+00      35   0.31135E-01   0.34376E+02 0.11870E+03 
c  Velocity[X]                                      0.28277E+02 
c  Velocity[Y]                                      0.11945E+01 
c  Velocity[Z]                                      0.49045E+01 
c  Pressure     0.13134E-03     123   0.51597E-02   0.15235E+00 0.60153E+02 
c  k            0.72217E-02      25   0.77382E-03   0.37045E+01 0.70592E+03 
c  omega        0.16602E+03      43   0.22718E-03   0.72534E+09 0.57179E+03 
c  TempC        0.38279E+04      60   0.18609E-01   0.12079E+06 0.20396E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6592          71.865          4.0751          4.2178
v  Velocity[Y]            -9.6428          8.5117       0.0015552      0.00087902
v  Velocity[Z]            -19.751          22.222        -0.33729        -0.16562
v  ǁVelocityǁ           0.0026065          72.276          4.4774          4.3729
v  Pressure               -2596.9          45.542           19.75           28.17
v  k                   2.2693e-08          17.697         0.11073        0.099673
v  omega               3.5859e-12      5.8453e+05          4930.2          1392.3
v  TempC                  -91.943          590.45          58.657          64.164
v  Density                0.40947          2.3769           1.155          1.1707
v  TurbVisc            1.0126e-13       0.0022899      0.00015933      0.00023211
v  CourantNb                    0          37.453         0.76523         0.56154
v  FourierNb            0.0025047          4.6712         0.15102         0.19505
v  total_pressure           98728      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41168          2.3769          1.0912          1.1395


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011275          37.621         0.91626         0.75659


 TIME FOR THE TIME STEP              305:        0.63544E+02

===============================================================


 INSTANT    0.285300000E-01   TIME STEP NUMBER             306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.297524051E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856138E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56650E+02 0.12576E+02
   Friction velocity        uet   :  0.14461E-02 0.61662E+01
   Friction velocity        uk    :  0.12203E-01 0.23238E+01
   Dimensionless distance   yplus :  0.15965E+00 0.60034E+02
   Friction thermal sca.    tstar : -0.27375E+03 0.41444E+02
   Rough dim-less th. sca.  tplus :  0.11912E+00 0.13708E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131508
   Nb of faces within the viscous sub-layer     :      10095
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1062 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21221E+00      35   0.30070E-01   0.35268E+02 0.12010E+03 
c  Velocity[X]                                      0.29167E+02 
c  Velocity[Y]                                      0.12111E+01 
c  Velocity[Z]                                      0.48904E+01 
c  Pressure     0.13307E-03     122   0.53622E-02   0.15337E+00 0.59288E+02 
c  k            0.72269E-02      25   0.77862E-03   0.37145E+01 0.70585E+03 
c  omega        0.16546E+03      43   0.32958E-03   0.59030E+09 0.51554E+03 
c  TempC        0.38339E+04      60   0.18218E-01   0.12162E+06 0.20430E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7747          72.736          4.0772          4.2205
v  Velocity[Y]            -9.5322           8.662       0.0015836      0.00088559
v  Velocity[Z]            -19.492           22.33        -0.33998        -0.16671
v  ǁVelocityǁ           0.0022136          73.131          4.4814          4.3764
v  Pressure               -2613.2          45.188          19.813          28.266
v  k                   8.5213e-09          18.117         0.11113        0.099971
v  omega               1.0973e-12      5.8447e+05          4933.3          1392.8
v  TempC                  -110.78          593.55          58.869           64.39
v  Density                0.40896          1.9491          1.1546          1.1702
v  TurbVisc             1.029e-13       0.0022897      0.00015987      0.00023294
v  CourantNb                    0          36.168         0.76594           0.562
v  FourierNb            0.0025048          4.6712          0.1515         0.19571
v  total_pressure           98712      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41322          1.9491          1.0908          1.1391


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0093098          36.332         0.91744         0.75771


 TIME FOR THE TIME STEP              306:        0.63442E+02

===============================================================


 INSTANT    0.286300000E-01   TIME STEP NUMBER             307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.715431726E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855570E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54615E+02 0.12409E+02
   Friction velocity        uet   :  0.15877E-02 0.61596E+01
   Friction velocity        uk    :  0.10655E-01 0.23496E+01
   Dimensionless distance   yplus :  0.11798E+00 0.61640E+02
   Friction thermal sca.    tstar : -0.28399E+03 0.42020E+02
   Rough dim-less th. sca.  tplus :  0.88028E-01 0.13771E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131383
   Nb of faces within the viscous sub-layer     :      10107
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1072 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21230E+00      36   0.30145E-01   0.34952E+02 0.11943E+03 
c  Velocity[X]                                      0.28699E+02 
c  Velocity[Y]                                      0.12216E+01 
c  Velocity[Z]                                      0.50311E+01 
c  Pressure     0.13341E-03     124   0.51401E-02   0.15254E+00 0.60382E+02 
c  k            0.72382E-02      25   0.78919E-03   0.37324E+01 0.70652E+03 
c  omega        0.36932E+11       2   0.36148E-10   0.45753E+10 0.14214E+04 
c  TempC        0.38397E+04      60   0.18477E-01   0.12101E+06 0.20341E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.902          76.207          4.0793          4.2232
v  Velocity[Y]            -9.1982           8.621       0.0015785      0.00088052
v  Velocity[Z]            -19.856          22.393        -0.34274        -0.16782
v  ǁVelocityǁ           0.0029679          76.211          4.4855          4.3799
v  Pressure                 -2628          45.246          19.838          28.319
v  k                    6.624e-09          18.082         0.11153         0.10027
v  omega               1.2286e-10      3.0587e+06          4937.6          1393.4
v  TempC                  -121.85          612.24          59.081          64.615
v  Density                0.40751          2.1751          1.1541          1.1698
v  TurbVisc            4.1013e-14       0.0022901      0.00016041      0.00023375
v  CourantNb                    0           37.93          0.7667         0.56246
v  FourierNb            0.0025049          4.6712         0.15197         0.19637
v  total_pressure           98697      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41702          2.1751          1.0904          1.1387


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0097191          38.095         0.91867         0.75883


 TIME FOR THE TIME STEP              307:        0.61794E+02

===============================================================


 INSTANT    0.287300000E-01   TIME STEP NUMBER             308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.444191878E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155857419E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56669E+02 0.12592E+02
   Friction velocity        uet   :  0.29289E-02 0.61767E+01
   Friction velocity        uk    :  0.17672E-01 0.23476E+01
   Dimensionless distance   yplus :  0.16805E+00 0.60794E+02
   Friction thermal sca.    tstar : -0.24767E+03 0.40178E+02
   Rough dim-less th. sca.  tplus :  0.12538E+00 0.13738E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131353
   Nb of faces within the viscous sub-layer     :      10087
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1079 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21238E+00      35   0.30600E-01   0.34736E+02 0.11893E+03 
c  Velocity[X]                                      0.28471E+02 
c  Velocity[Y]                                      0.12222E+01 
c  Velocity[Z]                                      0.50424E+01 
c  Pressure     0.13356E-03     119   0.51460E-02   0.15184E+00 0.52043E+02 
c  k            0.72521E-02      25   0.79783E-03   0.37618E+01 0.70825E+03 
c  omega        0.21307E+03      43   0.16099E-03   0.15993E+10 0.84488E+03 
c  TempC        0.38456E+04      60   0.18451E-01   0.12138E+06 0.20337E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9915           73.73          4.0814           4.226
v  Velocity[Y]            -9.1748          8.5561       0.0015819      0.00088713
v  Velocity[Z]             -19.92          22.296        -0.34553        -0.16893
v  ǁVelocityǁ           0.0046937          74.193          4.4896          4.3833
v  Pressure               -2649.2          44.852          19.812          28.311
v  k                   5.2028e-09          18.472         0.11191         0.10057
v  omega               4.4191e-11      1.5559e+06          4940.7            1394
v  TempC                  -102.42          620.35          59.293          64.841
v  Density                 0.3989          2.3344          1.1537          1.1694
v  TurbVisc            6.8837e-14       0.0022903      0.00016085      0.00023442
v  CourantNb                    0           38.01         0.76743         0.56292
v  FourierNb             0.002505          4.6712         0.15235         0.19688
v  total_pressure           98676      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41161          2.3344            1.09          1.1383


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.008022           38.18         0.91978         0.75981


 TIME FOR THE TIME STEP              308:        0.63022E+02

===============================================================


 INSTANT    0.288300000E-01   TIME STEP NUMBER             309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.312021479E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155857142E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54897E+02 0.12561E+02
   Friction velocity        uet   :  0.20063E-02 0.61957E+01
   Friction velocity        uk    :  0.83985E-02 0.23713E+01
   Dimensionless distance   yplus :  0.94761E-01 0.62129E+02
   Friction thermal sca.    tstar : -0.49270E+03 0.42261E+02
   Rough dim-less th. sca.  tplus :  0.70702E-01 0.13790E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131281
   Nb of faces within the viscous sub-layer     :      10098
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1090 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21246E+00      35   0.31267E-01   0.35996E+02 0.12093E+03 
c  Velocity[X]                                      0.29687E+02 
c  Velocity[Y]                                      0.12118E+01 
c  Velocity[Z]                                      0.50979E+01 
c  Pressure     0.13548E-03     119   0.53231E-02   0.15312E+00 0.58954E+02 
c  k            0.72727E-02      25   0.79489E-03   0.37472E+01 0.70568E+03 
c  omega        0.17017E+03      45   0.17456E-03   0.28293E+10 0.11196E+04 
c  TempC        0.38515E+04      60   0.18364E-01   0.12218E+06 0.20367E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1093          73.571          4.0835          4.2287
v  Velocity[Y]            -9.1949          8.4809       0.0015764      0.00088946
v  Velocity[Z]            -19.492          22.485        -0.34836        -0.17004
v  ǁVelocityǁ           0.0058383          74.031          4.4937          4.3868
v  Pressure               -2673.8          44.243          19.911          28.393
v  k                   1.1905e-08           19.06         0.11229         0.10087
v  omega               1.0061e-11      2.0602e+06          4945.8          1394.7
v  TempC                  -104.74           603.7          59.505          65.066
v  Density                0.39528          2.0686          1.1532           1.169
v  TurbVisc            2.6212e-14       0.0022903      0.00016138      0.00023523
v  CourantNb                    0          37.105         0.76818         0.56339
v  FourierNb            0.0025051          4.6712         0.15283         0.19754
v  total_pressure           98651      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41463          2.0686          1.0896          1.1379


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.005992          37.272         0.92101         0.76093


 TIME FOR THE TIME STEP              309:        0.63417E+02

===============================================================


 INSTANT    0.289300000E-01   TIME STEP NUMBER             310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.225612255E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155854428E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56792E+02 0.12749E+02
   Friction velocity        uet   :  0.12567E-02 0.61535E+01
   Friction velocity        uk    :  0.81452E-02 0.24060E+01
   Dimensionless distance   yplus :  0.77746E-01 0.61311E+02
   Friction thermal sca.    tstar : -0.25104E+03 0.45392E+02
   Rough dim-less th. sca.  tplus :  0.58007E-01 0.13758E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131172
   Nb of faces within the viscous sub-layer     :      10139
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1098 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21255E+00      35   0.30080E-01   0.35409E+02 0.11981E+03 
c  Velocity[X]                                      0.29129E+02 
c  Velocity[Y]                                      0.12242E+01 
c  Velocity[Z]                                      0.50556E+01 
c  Pressure     0.13237E-03     119   0.51431E-02   0.14859E+00 0.53039E+02 
c  k            0.72950E-02      25   0.78394E-03   0.37157E+01 0.70145E+03 
c  omega        0.17456E+03      43   0.16720E-03   0.10630E+10 0.68811E+03 
c  TempC        0.38574E+04      59   0.18690E-01   0.12288E+06 0.20389E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2315          73.645          4.0857          4.2315
v  Velocity[Y]            -9.7107          8.4927       0.0015741      0.00089004
v  Velocity[Z]            -19.904          22.851        -0.35122        -0.17115
v  ǁVelocityǁ           0.0031719          74.106          4.4977          4.3903
v  Pressure               -2689.5          45.009          19.921          28.412
v  k                    5.583e-09          19.009         0.11266         0.10118
v  omega               2.4363e-12      1.0538e+06          4948.7          1395.3
v  TempC                  -117.44          613.14          59.715          65.292
v  Density                0.40279          2.0972          1.1528          1.1686
v  TurbVisc            5.2885e-14       0.0022901      0.00016192      0.00023602
v  CourantNb                    0          38.537         0.76892         0.56384
v  FourierNb            0.0025052          4.6712         0.15331         0.19819
v  total_pressure           98636      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41677          2.0972          1.0892          1.1375


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0078208          38.705         0.92222         0.76204


 TIME FOR THE TIME STEP              310:        0.63304E+02

===============================================================


 INSTANT    0.290300000E-01   TIME STEP NUMBER             311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.227955102E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855254E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55146E+02 0.12724E+02
   Friction velocity        uet   :  0.15398E-02 0.62741E+01
   Friction velocity        uk    :  0.12522E-01 0.24044E+01
   Dimensionless distance   yplus :  0.13822E+00 0.62364E+02
   Friction thermal sca.    tstar : -0.25108E+03 0.48357E+02
   Rough dim-less th. sca.  tplus :  0.10313E+00 0.13799E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     131069
   Nb of faces within the viscous sub-layer     :      10143
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1107 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21264E+00      35   0.31997E-01   0.35361E+02 0.11959E+03 
c  Velocity[X]                                      0.28933E+02 
c  Velocity[Y]                                      0.12387E+01 
c  Velocity[Z]                                      0.51893E+01 
c  Pressure     0.13136E-03     126   0.50556E-02   0.14628E+00 0.87412E+02 
c  k            0.73199E-02      25   0.76919E-03   0.36973E+01 0.69856E+03 
c  omega        0.16755E+03      43   0.13323E-03   0.76484E+09 0.58343E+03 
c  TempC        0.38634E+04      60   0.18045E-01   0.12259E+06 0.20329E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3534          77.997          4.0878          4.2342
v  Velocity[Y]            -9.2571          8.4622       0.0015624       0.0008935
v  Velocity[Z]            -19.999            22.9        -0.35418        -0.17229
v  ǁVelocityǁ           0.0040886          78.001          4.5018          4.3937
v  Pressure               -2711.2          44.182          19.716          28.244
v  k                   2.8285e-09          19.311         0.11302         0.10148
v  omega               5.5344e-13       5.852e+05          4952.3            1396
v  TempC                  -89.018          606.34          59.922          65.518
v  Density                 0.3985          2.2682          1.1524          1.1682
v  TurbVisc            2.6147e-14       0.0022899      0.00016248      0.00023683
v  CourantNb                    0          38.729         0.76966          0.5643
v  FourierNb            0.0025053          4.6712          0.1538         0.19886
v  total_pressure           98614      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41574          2.2682          1.0888          1.1371


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010356          38.903         0.92346         0.76317


 TIME FOR THE TIME STEP              311:        0.63387E+02

===============================================================


 INSTANT    0.291300000E-01   TIME STEP NUMBER             312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.413217324E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155860418E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57518E+02 0.12800E+02
   Friction velocity        uet   :  0.10590E-02 0.61852E+01
   Friction velocity        uk    :  0.13552E-01 0.24220E+01
   Dimensionless distance   yplus :  0.13730E+00 0.61376E+02
   Friction thermal sca.    tstar : -0.29057E+03 0.51368E+02
   Rough dim-less th. sca.  tplus :  0.10244E+00 0.13761E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130952
   Nb of faces within the viscous sub-layer     :      10147
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1112 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21272E+00      36   0.31495E-01   0.36028E+02 0.12058E+03 
c  Velocity[X]                                      0.29518E+02 
c  Velocity[Y]                                      0.12413E+01 
c  Velocity[Z]                                      0.52691E+01 
c  Pressure     0.13348E-03     119   0.49128E-02   0.14731E+00 0.52816E+02 
c  k            0.73459E-02      26   0.75816E-03   0.37220E+01 0.69986E+03 
c  omega        0.16727E+03      43   0.14330E-03   0.22216E+10 0.98984E+03 
c  TempC        0.38695E+04      58   0.18329E-01   0.12079E+06 0.20144E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4583          75.737          4.0899          4.2369
v  Velocity[Y]            -9.3975          8.4428       0.0015598       0.0008937
v  Velocity[Z]            -19.755          22.784         -0.3572        -0.17343
v  ǁVelocityǁ           0.0041152           76.26          4.5059          4.3972
v  Pressure               -2732.4          44.882          19.654          28.175
v  k                   9.2235e-09           19.67         0.11336         0.10179
v  omega               1.1574e-13      2.0232e+06          4957.6          1396.7
v  TempC                  -105.39           597.7           60.13          65.744
v  Density                0.40158          1.9181          1.1519          1.1677
v  TurbVisc            1.3445e-14       0.0022899      0.00016305      0.00023765
v  CourantNb                    0          37.349         0.77039         0.56477
v  FourierNb            0.0025054          4.6712         0.15431         0.19954
v  total_pressure           98593      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41583          1.8883          1.0884          1.1367


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01085          37.518          0.9247         0.76431


 TIME FOR THE TIME STEP              312:        0.63367E+02

===============================================================


 INSTANT    0.292300000E-01   TIME STEP NUMBER             313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.421294863E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856940E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55738E+02 0.12625E+02
   Friction velocity        uet   :  0.29867E-02 0.62865E+01
   Friction velocity        uk    :  0.12735E-01 0.24439E+01
   Dimensionless distance   yplus :  0.14676E+00 0.62725E+02
   Friction thermal sca.    tstar : -0.46819E+03 0.50743E+02
   Rough dim-less th. sca.  tplus :  0.10950E+00 0.13812E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130825
   Nb of faces within the viscous sub-layer     :      10168
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1119 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21279E+00      35   0.31175E-01   0.35836E+02 0.12013E+03 
c  Velocity[X]                                      0.29274E+02 
c  Velocity[Y]                                      0.12702E+01 
c  Velocity[Z]                                      0.52925E+01 
c  Pressure     0.13521E-03     123   0.50519E-02   0.14826E+00 0.61842E+02 
c  k            0.73774E-02      26   0.75559E-03   0.37594E+01 0.70234E+03 
c  omega        0.17443E+03      44   0.18815E-03   0.12222E+10 0.73474E+03 
c  TempC        0.38756E+04      60   0.18482E-01   0.12075E+06 0.20105E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5842          74.981           4.092          4.2397
v  Velocity[Y]               -9.5          8.3498       0.0015414      0.00089818
v  Velocity[Z]            -20.061          22.684        -0.36026        -0.17458
v  ǁVelocityǁ            0.003528          75.568          4.5099          4.4007
v  Pressure               -2751.3          46.103          19.772          28.275
v  k                   8.0564e-09          19.847         0.11369         0.10209
v  omega               2.2839e-14      1.0381e+06          4962.1          1397.4
v  TempC                  -118.59          588.14          60.335          65.969
v  Density                0.40556          2.1053          1.1515          1.1673
v  TurbVisc            4.0926e-14       0.0022898      0.00016364      0.00023848
v  CourantNb                    0          39.078         0.77114         0.56523
v  FourierNb            0.0025055          4.6712         0.15483         0.20023
v  total_pressure           98574      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41722          2.1053           1.088          1.1363


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010141           39.25         0.92597         0.76546


 TIME FOR THE TIME STEP              313:        0.63637E+02

===============================================================


 INSTANT    0.293300000E-01   TIME STEP NUMBER             314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.939275731E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155854995E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57765E+02 0.12828E+02
   Friction velocity        uet   :  0.17616E-02 0.63780E+01
   Friction velocity        uk    :  0.11776E-01 0.24543E+01
   Dimensionless distance   yplus :  0.12562E+00 0.61224E+02
   Friction thermal sca.    tstar : -0.37055E+03 0.54563E+02
   Rough dim-less th. sca.  tplus :  0.93728E-01 0.13755E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130756
   Nb of faces within the viscous sub-layer     :      10151
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1134 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21287E+00      35   0.32398E-01   0.35892E+02 0.12009E+03 
c  Velocity[X]                                      0.29296E+02 
c  Velocity[Y]                                      0.12803E+01 
c  Velocity[Z]                                      0.53160E+01 
c  Pressure     0.13576E-03     123   0.49711E-02   0.14780E+00 0.77524E+02 
c  k            0.74109E-02      25   0.76030E-03   0.37665E+01 0.70193E+03 
c  omega        0.16855E+03      43   0.23331E-03   0.38742E+10 0.12993E+04 
c  TempC        0.38816E+04      60   0.18076E-01   0.12237E+06 0.20205E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6767          75.085          4.0941          4.2424
v  Velocity[Y]            -9.3177           8.365       0.0015246      0.00089384
v  Velocity[Z]            -20.201          22.972        -0.36326        -0.17571
v  ǁVelocityǁ           0.0038285          75.727          4.5139          4.4041
v  Pressure               -2774.5           47.17          19.973          28.485
v  k                   1.2127e-08          20.316         0.11402         0.10239
v  omega               4.5653e-15      2.7048e+06          4966.7          1398.2
v  TempC                  -107.75          607.61          60.537          66.194
v  Density                0.41006           2.285          1.1511          1.1669
v  TurbVisc            3.8164e-14       0.0022897      0.00016422      0.00023929
v  CourantNb                    0          38.932         0.77187         0.56569
v  FourierNb            0.0025056          4.6712         0.15535         0.20092
v  total_pressure           98550      1.0137e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41553           2.285          1.0876          1.1359


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010077          39.108         0.92722         0.76661


 TIME FOR THE TIME STEP              314:        0.63195E+02

===============================================================


 INSTANT    0.294300000E-01   TIME STEP NUMBER             315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.309307264E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155853429E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55921E+02 0.12775E+02
   Friction velocity        uet   :  0.10796E-02 0.62280E+01
   Friction velocity        uk    :  0.14284E-01 0.24815E+01
   Dimensionless distance   yplus :  0.16850E+00 0.62132E+02
   Friction thermal sca.    tstar : -0.30655E+03 0.75612E+02
   Rough dim-less th. sca.  tplus :  0.12572E+00 0.13790E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130660
   Nb of faces within the viscous sub-layer     :      10163
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1143 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21294E+00      36   0.31143E-01   0.36759E+02 0.12140E+03 
c  Velocity[X]                                      0.30044E+02 
c  Velocity[Y]                                      0.12744E+01 
c  Velocity[Z]                                      0.54409E+01 
c  Pressure     0.13741E-03     122   0.50448E-02   0.14851E+00 0.10290E+03 
c  k            0.74473E-02      26   0.76742E-03   0.37613E+01 0.70024E+03 
c  omega        0.19419E+03      43   0.26960E-03   0.16528E+10 0.85156E+03 
c  TempC        0.38879E+04      60   0.18227E-01   0.12204E+06 0.20142E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7835          79.084          4.0962          4.2451
v  Velocity[Y]            -9.2705           8.381       0.0014809      0.00088716
v  Velocity[Z]            -19.931           23.38        -0.36636        -0.17686
v  ǁVelocityǁ           0.0037443          79.088          4.5179          4.4075
v  Pressure               -2798.5          47.449          20.275          28.793
v  k                   1.4004e-08          20.517         0.11436          0.1027
v  omega               8.5554e-16      1.3758e+06          4970.6          1398.8
v  TempC                  -118.89          603.63          60.738          66.419
v  Density                  0.401          2.1353          1.1507          1.1665
v  TurbVisc            5.3773e-14       0.0022896      0.00016482      0.00024011
v  CourantNb                    0          37.811         0.77261         0.56614
v  FourierNb            0.0025058          4.6712         0.15587         0.20161
v  total_pressure           98526      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4164          2.0589          1.0872          1.1355


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01348          37.982         0.92848         0.76775


 TIME FOR THE TIME STEP              315:        0.63690E+02

===============================================================


 INSTANT    0.295300000E-01   TIME STEP NUMBER             316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.392925799E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155851315E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58078E+02 0.13053E+02
   Friction velocity        uet   :  0.14172E-02 0.62154E+01
   Friction velocity        uk    :  0.11331E-01 0.24930E+01
   Dimensionless distance   yplus :  0.12929E+00 0.61093E+02
   Friction thermal sca.    tstar : -0.25580E+03 0.15427E+03
   Rough dim-less th. sca.  tplus :  0.96468E-01 0.13750E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130530
   Nb of faces within the viscous sub-layer     :      10173
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1153 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21303E+00      36   0.32478E-01   0.36352E+02 0.12059E+03 
c  Velocity[X]                                      0.29489E+02 
c  Velocity[Y]                                      0.12873E+01 
c  Velocity[Z]                                      0.55762E+01 
c  Pressure     0.13430E-03     121   0.49181E-02   0.14393E+00 0.79903E+02 
c  k            0.74827E-02      26   0.77047E-03   0.37605E+01 0.69897E+03 
c  omega        0.17113E+03      44   0.26819E-03   0.18689E+10 0.90365E+03 
c  TempC        0.38943E+04      61   0.18607E-01   0.12202E+06 0.20106E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9228          75.817          4.0983          4.2479
v  Velocity[Y]            -9.2377          8.3016        0.001462      0.00088358
v  Velocity[Z]            -20.307          23.143        -0.36952        -0.17803
v  ǁVelocityǁ           0.0032581          76.501          4.5219           4.411
v  Pressure               -2819.2          46.911          20.362          28.955
v  k                   1.8357e-08          20.482         0.11471         0.10301
v  omega               1.5371e-16      1.4468e+06            4976          1399.6
v  TempC                  -120.53          617.89          60.936          66.644
v  Density                0.40282          2.2895          1.1503          1.1661
v  TurbVisc            6.2077e-14       0.0022896      0.00016544      0.00024095
v  CourantNb                    0          39.256         0.77332          0.5666
v  FourierNb            0.0025059          4.6712         0.15642         0.20232
v  total_pressure           98506      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41508          2.1277          1.0868          1.1351


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01338           39.43         0.92974         0.76892


 TIME FOR THE TIME STEP              316:        0.63369E+02

===============================================================


 INSTANT    0.296300000E-01   TIME STEP NUMBER             317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.564163381E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155854502E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56492E+02 0.12927E+02
   Friction velocity        uet   :  0.10476E-02 0.64187E+01
   Friction velocity        uk    :  0.58515E-02 0.24922E+01
   Dimensionless distance   yplus :  0.66732E-01 0.61751E+02
   Friction thermal sca.    tstar : -0.46846E+03 0.63462E+02
   Rough dim-less th. sca.  tplus :  0.49789E-01 0.13775E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130371
   Nb of faces within the viscous sub-layer     :      10153
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1155 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21309E+00      35   0.31592E-01   0.37333E+02 0.12207E+03 
c  Velocity[X]                                      0.30454E+02 
c  Velocity[Y]                                      0.12985E+01 
c  Velocity[Z]                                      0.55804E+01 
c  Pressure     0.13564E-03     121   0.49187E-02   0.14443E+00 0.58812E+02 
c  k            0.75133E-02      26   0.76408E-03   0.37539E+01 0.69711E+03 
c  omega        0.17232E+03      45   0.18327E-03   0.12360E+10 0.73494E+03 
c  TempC        0.39009E+04      63   0.18424E-01   0.12335E+06 0.20181E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0773          76.906          4.1004          4.2506
v  Velocity[Y]            -9.2561          8.4615       0.0014048      0.00087834
v  Velocity[Z]            -20.382           23.13        -0.37271         -0.1792
v  ǁVelocityǁ           0.0042955          77.651          4.5259          4.4144
v  Pressure               -2843.2          46.425          20.361          28.964
v  k                   1.2906e-08           20.96         0.11508         0.10332
v  omega               2.5748e-17      7.4842e+05          4980.4          1400.3
v  TempC                  -90.813          606.76          61.132          66.869
v  Density                0.39637          2.3141          1.1498          1.1657
v  TurbVisc            8.1355e-14       0.0022895      0.00016605      0.00024178
v  CourantNb                    0          40.002         0.77407         0.56706
v  FourierNb             0.002506          4.6712         0.15696         0.20302
v  total_pressure           98482      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41333          2.3141          1.0864          1.1347


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010636          40.183         0.93103         0.77008


 TIME FOR THE TIME STEP              317:        0.63360E+02

===============================================================


 INSTANT    0.297300000E-01   TIME STEP NUMBER             318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.307395673E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856657E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58305E+02 0.13068E+02
   Friction velocity        uet   :  0.57218E-03 0.64478E+01
   Friction velocity        uk    :  0.66359E-02 0.25194E+01
   Dimensionless distance   yplus :  0.76014E-01 0.60932E+02
   Friction thermal sca.    tstar : -0.26176E+03 0.50983E+02
   Rough dim-less th. sca.  tplus :  0.56715E-01 0.13743E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130299
   Nb of faces within the viscous sub-layer     :      10141
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1157 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21318E+00      36   0.32088E-01   0.36783E+02 0.12104E+03 
c  Velocity[X]                                      0.29948E+02 
c  Velocity[Y]                                      0.12986E+01 
c  Velocity[Z]                                      0.55373E+01 
c  Pressure     0.13764E-03     119   0.48907E-02   0.14562E+00 0.51077E+02 
c  k            0.75374E-02      26   0.75125E-03   0.37522E+01 0.69571E+03 
c  omega        0.16999E+03      44   0.37719E-03   0.37917E+10 0.12780E+04 
c  TempC        0.39075E+04      61   0.18297E-01   0.12257E+06 0.20082E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2199          77.692          4.1024          4.2534
v  Velocity[Y]            -9.4875          8.3685       0.0013973      0.00088601
v  Velocity[Z]            -20.074          23.345        -0.37595        -0.18039
v  ǁVelocityǁ            0.003462          78.447          4.5298          4.4179
v  Pressure               -2870.3          46.191          20.362          28.973
v  k                   8.4395e-09          21.631         0.11547         0.10364
v  omega               1.7192e-18      1.6815e+06          4985.4          1401.2
v  TempC                  -106.78          598.94          61.329          67.094
v  Density                0.40138           1.937          1.1494          1.1653
v  TurbVisc            5.8779e-14       0.0022899      0.00016665      0.00024259
v  CourantNb                    0          38.238          0.7748         0.56752
v  FourierNb            0.0025061          4.6712          0.1575         0.20371
v  total_pressure           98455      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41431          1.9027           1.086          1.1343


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0079075          38.413          0.9323         0.77123


 TIME FOR THE TIME STEP              318:        0.63609E+02

===============================================================


 INSTANT    0.298300000E-01   TIME STEP NUMBER             319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.526173290E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855329E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56246E+02 0.13024E+02
   Friction velocity        uet   :  0.16290E-02 0.63654E+01
   Friction velocity        uk    :  0.41625E-02 0.25577E+01
   Dimensionless distance   yplus :  0.62197E-01 0.62033E+02
   Friction thermal sca.    tstar : -0.35699E+03 0.51422E+02
   Rough dim-less th. sca.  tplus :  0.46406E-01 0.13786E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130153
   Nb of faces within the viscous sub-layer     :      10140
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1162 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21325E+00      36   0.32250E-01   0.36747E+02 0.12085E+03 
c  Velocity[X]                                      0.29832E+02 
c  Velocity[Y]                                      0.12867E+01 
c  Velocity[Z]                                      0.56290E+01 
c  Pressure     0.13410E-03     122   0.47618E-02   0.14074E+00 0.61137E+02 
c  k            0.75540E-02      26   0.75060E-03   0.37700E+01 0.69610E+03 
c  omega        0.20563E+03      44   0.16577E-03   0.36983E+10 0.12602E+04 
c  TempC        0.39139E+04      63   0.18491E-01   0.12130E+06 0.19944E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3751          78.028          4.1044          4.2561
v  Velocity[Y]            -9.6461          8.2655       0.0013486      0.00088096
v  Velocity[Z]             -20.51          23.505        -0.37924        -0.18158
v  ǁVelocityǁ            0.002332          78.769          4.5337          4.4213
v  Pressure               -2890.9          45.844          20.465          29.037
v  k                   2.1984e-09          21.664          0.1159         0.10395
v  omega               2.7148e-19      2.0361e+06          4989.9          1401.8
v  TempC                  -120.58          590.38          61.529           67.32
v  Density                0.40499          2.1229           1.149          1.1648
v  TurbVisc            2.4053e-14       0.0022901      0.00016727      0.00024342
v  CourantNb                    0          40.588         0.77553         0.56798
v  FourierNb            0.0025062          4.6712         0.15806         0.20442
v  total_pressure           98434      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41678          2.1229          1.0856          1.1339


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0099894          40.766         0.93359          0.7724


 TIME FOR THE TIME STEP              319:        0.63502E+02

===============================================================


 INSTANT    0.299300000E-01   TIME STEP NUMBER             320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.370393112E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155853975E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58479E+02 0.13184E+02
   Friction velocity        uet   :  0.73065E-03 0.65545E+01
   Friction velocity        uk    :  0.11659E-01 0.25606E+01
   Dimensionless distance   yplus :  0.13954E+00 0.60847E+02
   Friction thermal sca.    tstar : -0.31949E+03 0.53233E+02
   Rough dim-less th. sca.  tplus :  0.10411E+00 0.13740E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     130061
   Nb of faces within the viscous sub-layer     :      10122
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1166 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21333E+00      36   0.32405E-01   0.36895E+02 0.12096E+03 
c  Velocity[X]                                      0.30020E+02 
c  Velocity[Y]                                      0.13373E+01 
c  Velocity[Z]                                      0.55375E+01 
c  Pressure     0.13642E-03     122   0.48046E-02   0.14207E+00 0.64809E+02 
c  k            0.75645E-02      26   0.75269E-03   0.37722E+01 0.69510E+03 
c  omega        0.19038E+03      44   0.15436E-03   0.16534E+10 0.84506E+03 
c  TempC        0.39203E+04      63   0.18756E-01   0.12184E+06 0.19954E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4559          79.459          4.1065          4.2588
v  Velocity[Y]            -9.9497          8.2951       0.0012816      0.00088061
v  Velocity[Z]            -20.606          23.266         -0.3825        -0.18276
v  ǁVelocityǁ           0.0033072          80.266          4.5377          4.4247
v  Pressure               -2911.6          45.457          20.601          29.169
v  k                   2.6382e-09          22.231         0.11635         0.10426
v  omega               3.8702e-20      1.2725e+06          4993.5          1402.4
v  TempC                  -101.46          589.85           61.73          67.545
v  Density                  0.409          2.3149          1.1486          1.1644
v  TurbVisc            9.0226e-15         0.00229      0.00016788      0.00024426
v  CourantNb                    0          40.089         0.77625         0.56843
v  FourierNb            0.0025063          4.6712         0.15862         0.20514
v  total_pressure           98413      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40998          2.3149          1.0852          1.1335


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0082959          40.273         0.93487         0.77357


 TIME FOR THE TIME STEP              320:        0.63497E+02

===============================================================


 INSTANT    0.300300000E-01   TIME STEP NUMBER             321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.486441088E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155854223E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57128E+02 0.13110E+02
   Friction velocity        uet   :  0.24289E-02 0.66085E+01
   Friction velocity        uk    :  0.11360E-01 0.25927E+01
   Dimensionless distance   yplus :  0.12498E+00 0.61664E+02
   Friction thermal sca.    tstar : -0.50364E+03 0.56046E+02
   Rough dim-less th. sca.  tplus :  0.93246E-01 0.13772E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     129919
   Nb of faces within the viscous sub-layer     :      10107
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1170 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21340E+00      37   0.32633E-01   0.36647E+02 0.12042E+03 
c  Velocity[X]                                      0.29574E+02 
c  Velocity[Y]                                      0.13083E+01 
c  Velocity[Z]                                      0.57653E+01 
c  Pressure     0.13579E-03     121   0.47127E-02   0.14020E+00 0.65518E+02 
c  k            0.75748E-02      26   0.74879E-03   0.37585E+01 0.69260E+03 
c  omega        0.17289E+03      46   0.13023E-03   0.97456E+09 0.64881E+03 
c  TempC        0.39264E+04      64   0.18771E-01   0.12357E+06 0.20061E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5695          78.535          4.1086          4.2615
v  Velocity[Y]            -9.7659          7.9656       0.0012021      0.00087232
v  Velocity[Z]            -20.352           23.45        -0.38585        -0.18396
v  ǁVelocityǁ           0.0030263          79.382          4.5418          4.4281
v  Pressure               -2943.8          45.796          20.604          29.171
v  k                   3.1742e-09          23.235         0.11683         0.10458
v  omega               1.6187e-21      7.7207e+05          4996.4          1402.9
v  TempC                   -107.7          599.21          61.936           67.77
v  Density                0.40925          2.0571          1.1482           1.164
v  TurbVisc            1.1895e-14       0.0022899      0.00016848      0.00024507
v  CourantNb                    0          39.297         0.77699         0.56889
v  FourierNb            0.0025064          4.6712         0.15916         0.20584
v  total_pressure           98381      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41907          2.0571          1.0848          1.1331


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011454          39.477         0.93615         0.77472


 TIME FOR THE TIME STEP              321:        0.63998E+02

===============================================================


 INSTANT    0.301300000E-01   TIME STEP NUMBER             322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.558160269E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855597E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59240E+02 0.13278E+02
   Friction velocity        uet   :  0.22281E-02 0.64572E+01
   Friction velocity        uk    :  0.80480E-02 0.26472E+01
   Dimensionless distance   yplus :  0.13898E+00 0.60512E+02
   Friction thermal sca.    tstar : -0.72283E+03 0.61498E+02
   Rough dim-less th. sca.  tplus :  0.10369E+00 0.13727E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     129803
   Nb of faces within the viscous sub-layer     :      10084
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1177 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21346E+00      36   0.32043E-01   0.37801E+02 0.12217E+03 
c  Velocity[X]                                      0.30610E+02 
c  Velocity[Y]                                      0.13565E+01 
c  Velocity[Z]                                      0.58349E+01 
c  Pressure     0.13884E-03     120   0.48134E-02   0.14195E+00 0.75559E+02 
c  k            0.75827E-02      26   0.74608E-03   0.37452E+01 0.69010E+03 
c  omega        0.19432E+03      44   0.56942E-03   0.35619E+11 0.36538E+04 
c  TempC        0.39322E+04      62   0.18474E-01   0.12289E+06 0.19972E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6865          79.085          4.1107          4.2643
v  Velocity[Y]            -9.5369          8.0531       0.0011709      0.00087415
v  Velocity[Z]            -20.772          23.358        -0.38917        -0.18516
v  ǁVelocityǁ           0.0032186          79.886          4.5458          4.4315
v  Pressure               -2963.5          46.016           20.82          29.386
v  k                   5.9012e-09          23.252         0.11731         0.10489
v  omega               1.9822e-22      7.8019e+06          5006.3          1404.1
v  TempC                  -122.67           612.7          62.144          67.995
v  Density                0.40486          2.1347          1.1477          1.1636
v  TurbVisc             1.431e-14       0.0022897      0.00016907      0.00024588
v  CourantNb                    0          41.104         0.77775         0.56935
v  FourierNb            0.0025066          4.6712          0.1597         0.20653
v  total_pressure           98362      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41892          2.1347          1.0844          1.1327


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012974          41.286         0.93745         0.77588


 TIME FOR THE TIME STEP              322:        0.63426E+02

===============================================================


 INSTANT    0.302300000E-01   TIME STEP NUMBER             323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.432392717E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155851802E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57566E+02 0.13129E+02
   Friction velocity        uet   :  0.22341E-02 0.64635E+01
   Friction velocity        uk    :  0.70965E-02 0.26485E+01
   Dimensionless distance   yplus :  0.78688E-01 0.61445E+02
   Friction thermal sca.    tstar : -0.66771E+03 0.62521E+02
   Rough dim-less th. sca.  tplus :  0.58710E-01 0.13763E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     129657
   Nb of faces within the viscous sub-layer     :      10052
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1183 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21355E+00      35   0.32941E-01   0.36942E+02 0.12064E+03 
c  Velocity[X]                                      0.29798E+02 
c  Velocity[Y]                                      0.13250E+01 
c  Velocity[Z]                                      0.58184E+01 
c  Pressure     0.13609E-03     123   0.47035E-02   0.13774E+00 0.72754E+02 
c  k            0.75879E-02      26   0.75613E-03   0.37664E+01 0.69088E+03 
c  omega        0.11036E+04      39   0.53880E-04   0.12319E+11 0.22455E+04 
c  TempC        0.39379E+04      64   0.17863E-01   0.12300E+06 0.19947E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7835          83.943          4.1129          4.2669
v  Velocity[Y]            -9.7512          7.9817       0.0011109      0.00086811
v  Velocity[Z]             -20.71          23.352        -0.39254        -0.18637
v  ǁVelocityǁ           0.0036548          83.952          4.5499          4.4349
v  Pressure               -2986.5          46.659          20.926          29.509
v  k                    2.037e-09          23.015          0.1178         0.10521
v  omega               2.1579e-23      3.9235e+06          5007.6          1404.5
v  TempC                  -105.32          603.41          62.353          68.219
v  Density                0.39869           2.347          1.1473          1.1632
v  TurbVisc             5.474e-14       0.0022897      0.00016967      0.00024673
v  CourantNb                    0          40.942         0.77849          0.5698
v  FourierNb            0.0025067          4.6712         0.16026         0.20725
v  total_pressure           98338      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41424           2.347           1.084          1.1323


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014571          41.131         0.93874         0.77705


 TIME FOR THE TIME STEP              323:        0.63305E+02

===============================================================


 INSTANT    0.303300000E-01   TIME STEP NUMBER             324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.241890442E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155854443E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60072E+02 0.13326E+02
   Friction velocity        uet   :  0.20356E-02 0.65029E+01
   Friction velocity        uk    :  0.97022E-02 0.26350E+01
   Dimensionless distance   yplus :  0.10668E+00 0.60943E+02
   Friction thermal sca.    tstar : -0.36431E+03 0.63947E+02
   Rough dim-less th. sca.  tplus :  0.79598E-01 0.13744E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     129498
   Nb of faces within the viscous sub-layer     :      10044
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1190 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21362E+00      36   0.33953E-01   0.38063E+02 0.12233E+03 
c  Velocity[X]                                      0.30712E+02 
c  Velocity[Y]                                      0.13320E+01 
c  Velocity[Z]                                      0.60195E+01 
c  Pressure     0.13826E-03     119   0.48307E-02   0.13852E+00 0.72084E+02 
c  k            0.76021E-02      27   0.75984E-03   0.37802E+01 0.69090E+03 
c  omega        0.34618E+03      43   0.97437E-04   0.36370E+10 0.12408E+04 
c  TempC        0.39436E+04      62   0.17785E-01   0.12071E+06 0.19726E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8995          80.985           4.115          4.2696
v  Velocity[Y]             -9.582          8.0677       0.0010879      0.00087339
v  Velocity[Z]            -20.694          23.446        -0.39593        -0.18758
v  ǁVelocityǁ           0.0028723          81.887           4.554          4.4383
v  Pressure               -3010.7          46.853          21.127          29.709
v  k                   1.8645e-09           23.57         0.11829         0.10553
v  omega                    1e-24      1.9837e+06          5009.6          1404.9
v  TempC                  -108.05          612.92          62.566          68.444
v  Density                0.40292          2.1044          1.1469          1.1628
v  TurbVisc            1.8897e-14       0.0022896      0.00017026      0.00024755
v  CourantNb                    0          39.145         0.77923         0.57026
v  FourierNb            0.0025068          4.6712         0.16079         0.20794
v  total_pressure           98314      1.0137e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40496          1.9305          1.0836          1.1319


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014545          39.329         0.94003          0.7782


 TIME FOR THE TIME STEP              324:        0.63664E+02

===============================================================


 INSTANT    0.304300000E-01   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.908717452E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155850370E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58230E+02 0.13268E+02
   Friction velocity        uet   :  0.16283E-02 0.64842E+01
   Friction velocity        uk    :  0.90803E-02 0.26654E+01
   Dimensionless distance   yplus :  0.10296E+00 0.61603E+02
   Friction thermal sca.    tstar : -0.45074E+03 0.68234E+02
   Rough dim-less th. sca.  tplus :  0.76816E-01 0.13769E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     129442
   Nb of faces within the viscous sub-layer     :      10052
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1201 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21367E+00      36   0.32382E-01   0.37853E+02 0.12186E+03 
c  Velocity[X]                                      0.30508E+02 
c  Velocity[Y]                                      0.13342E+01 
c  Velocity[Z]                                      0.60114E+01 
c  Pressure     0.13826E-03     123   0.45667E-02   0.13728E+00 0.10018E+03 
c  k            0.76218E-02      27   0.75936E-03   0.38020E+01 0.69164E+03 
c  omega        0.18999E+03      46   0.16200E-03   0.22401E+10 0.97562E+03 
c  TempC        0.39493E+04      64   0.18243E-01   0.12073E+06 0.19695E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9958          84.581          4.1172          4.2723
v  Velocity[Y]            -9.7444          8.0438      0.00099183      0.00086952
v  Velocity[Z]            -21.441          23.384        -0.39938        -0.18879
v  ǁVelocityǁ           0.0010991          84.583          4.5581          4.4417
v  Pressure               -3031.7           46.91          21.452           30.03
v  k                   3.1406e-09          23.718         0.11877         0.10585
v  omega                    1e-24      1.2013e+06          5013.6          1405.5
v  TempC                  -120.56          614.97          62.778          68.669
v  Density                0.39859          2.1392          1.1464          1.1624
v  TurbVisc            1.7292e-14       0.0022898      0.00017085      0.00024837
v  CourantNb                    0          41.609         0.77999         0.57071
v  FourierNb            0.0025069          4.6712         0.16133         0.20864
v  total_pressure           98293      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41482          2.1392          1.0832          1.1316


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01265          41.796         0.94132         0.77935


 TIME FOR THE TIME STEP              325:        0.63726E+02

===============================================================


 INSTANT    0.305300000E-01   TIME STEP NUMBER             326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.382383838E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155851095E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60253E+02 0.13442E+02
   Friction velocity        uet   :  0.16041E-02 0.65081E+01
   Friction velocity        uk    :  0.13019E-01 0.26734E+01
   Dimensionless distance   yplus :  0.14311E+00 0.60657E+02
   Friction thermal sca.    tstar : -0.37075E+03 0.68231E+02
   Rough dim-less th. sca.  tplus :  0.10677E+00 0.13732E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     129358
   Nb of faces within the viscous sub-layer     :      10050
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1206 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21375E+00      36   0.32256E-01   0.37061E+02 0.12045E+03 
c  Velocity[X]                                      0.29562E+02 
c  Velocity[Y]                                      0.13525E+01 
c  Velocity[Z]                                      0.61462E+01 
c  Pressure     0.13665E-03     120   0.47407E-02   0.13435E+00 0.69553E+02 
c  k            0.76455E-02      27   0.75210E-03   0.37785E+01 0.68813E+03 
c  omega        0.17692E+03      46   0.13433E-03   0.10695E+10 0.67486E+03 
c  TempC        0.39548E+04      63   0.18264E-01   0.12316E+06 0.19859E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0583          81.416          4.1193           4.275
v  Velocity[Y]             -9.817          8.0314      0.00095275      0.00087425
v  Velocity[Z]             -21.21          23.371        -0.40279        -0.19001
v  ǁVelocityǁ           0.0035162          82.351          4.5622          4.4451
v  Pressure               -3059.7          48.372          21.456           30.09
v  k                   5.0469e-09          24.071         0.11924         0.10617
v  omega                    1e-24      6.0924e+05          5017.5            1406
v  TempC                  -106.21           598.9          62.989          68.894
v  Density                0.39767          2.3147           1.146           1.162
v  TurbVisc            1.2889e-14       0.0022897      0.00017141      0.00024916
v  CourantNb                    0          41.993         0.78074         0.57117
v  FourierNb            0.0025071          4.6712         0.16185         0.20931
v  total_pressure           98265      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41271          2.3147          1.0828          1.1312


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014034          42.186         0.94258         0.78048


 TIME FOR THE TIME STEP              326:        0.63639E+02

===============================================================


 INSTANT    0.306300000E-01   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.270870885E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855613E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58772E+02 0.13329E+02
   Friction velocity        uet   :  0.28713E-02 0.65609E+01
   Friction velocity        uk    :  0.52140E-02 0.26929E+01
   Dimensionless distance   yplus :  0.87121E-01 0.61412E+02
   Friction thermal sca.    tstar : -0.71626E+03 0.67999E+02
   Rough dim-less th. sca.  tplus :  0.65002E-01 0.13762E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     129270
   Nb of faces within the viscous sub-layer     :      10025
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1211 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21382E+00      36   0.34055E-01   0.37519E+02 0.12106E+03 
c  Velocity[X]                                      0.30036E+02 
c  Velocity[Y]                                      0.13446E+01 
c  Velocity[Z]                                      0.61383E+01 
c  Pressure     0.13783E-03     120   0.46165E-02   0.13421E+00 0.72287E+02 
c  k            0.76724E-02      27   0.74432E-03   0.37483E+01 0.68393E+03 
c  omega        0.17349E+03      46   0.12886E-03   0.59978E+09 0.50526E+03 
c  TempC        0.39604E+04      64   0.17751E-01   0.12299E+06 0.19813E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.2011          81.605          4.1215          4.2777
v  Velocity[Y]            -10.036          8.1246      0.00091398      0.00086706
v  Velocity[Z]            -21.268          23.157         -0.4062         -0.1912
v  ǁVelocityǁ           0.0044492          82.611          4.5663          4.4485
v  Pressure               -3089.2           49.59          21.674           30.27
v  k                   9.0832e-09          24.758         0.11972          0.1065
v  omega                    1e-24      5.8703e+05          5019.7          1406.5
v  TempC                   -116.3          593.19            63.2          69.119
v  Density                  0.405          2.1157          1.1456          1.1616
v  TurbVisc            2.0712e-14       0.0022897      0.00017197      0.00024994
v  CourantNb                    0          40.077          0.7815         0.57163
v  FourierNb            0.0025072          4.6712         0.16236         0.20997
v  total_pressure           98236      1.0137e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41785          2.1157          1.0824          1.1308


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015325          40.266         0.94386          0.7816


 TIME FOR THE TIME STEP              327:        0.64057E+02

===============================================================


 INSTANT    0.307300000E-01   TIME STEP NUMBER             328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.746663251E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155851926E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60795E+02 0.13577E+02
   Friction velocity        uet   :  0.20653E-02 0.65579E+01
   Friction velocity        uk    :  0.97283E-02 0.27298E+01
   Dimensionless distance   yplus :  0.92865E-01 0.61247E+02
   Friction thermal sca.    tstar : -0.41001E+03 0.66503E+02
   Rough dim-less th. sca.  tplus :  0.69288E-01 0.13756E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     129105
   Nb of faces within the viscous sub-layer     :      10011
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1219 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21389E+00      37   0.33186E-01   0.38127E+02 0.12191E+03 
c  Velocity[X]                                      0.30604E+02 
c  Velocity[Y]                                      0.13640E+01 
c  Velocity[Z]                                      0.61594E+01 
c  Pressure     0.14065E-03     121   0.46626E-02   0.13574E+00 0.79706E+02 
c  k            0.77025E-02      27   0.74580E-03   0.37455E+01 0.68228E+03 
c  omega        0.17354E+03      46   0.24948E-03   0.63867E+09 0.52087E+03 
c  TempC        0.39660E+04      63   0.17364E-01   0.12238E+06 0.19730E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.2914          81.631          4.1235          4.2804
v  Velocity[Y]            -10.458           8.168       0.0008439      0.00085897
v  Velocity[Z]            -21.323          23.253         -0.4096         -0.1924
v  ǁVelocityǁ           0.0043237          82.654          4.5704          4.4519
v  Pressure               -3117.1          50.572          21.882          30.493
v  k                   6.7185e-09          24.725         0.12018         0.10683
v  omega                    1e-24      5.8574e+05          5022.8            1407
v  TempC                  -125.77           587.7          63.412          69.344
v  Density                0.40767          2.2518          1.1452          1.1611
v  TurbVisc            4.6197e-14       0.0022895      0.00017254      0.00025076
v  CourantNb                    0          41.525         0.78225         0.57208
v  FourierNb            0.0025073          4.6712         0.16289         0.21066
v  total_pressure           98208      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41209          2.0708          1.0821          1.1304


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015724          41.716         0.94514         0.78275


 TIME FOR THE TIME STEP              328:        0.63773E+02

===============================================================


 INSTANT    0.308300000E-01   TIME STEP NUMBER             329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.379469145E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852949E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59193E+02 0.13497E+02
   Friction velocity        uet   :  0.76829E-03 0.65994E+01
   Friction velocity        uk    :  0.10384E-01 0.27280E+01
   Dimensionless distance   yplus :  0.98486E-01 0.61387E+02
   Friction thermal sca.    tstar : -0.29226E+03 0.68346E+02
   Rough dim-less th. sca.  tplus :  0.73482E-01 0.13761E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     128929
   Nb of faces within the viscous sub-layer     :       9980
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1228 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21395E+00      37   0.33091E-01   0.37899E+02 0.12142E+03 
c  Velocity[X]                                      0.30351E+02 
c  Velocity[Y]                                      0.13779E+01 
c  Velocity[Z]                                      0.61705E+01 
c  Pressure     0.13964E-03     121   0.45368E-02   0.13317E+00 0.59207E+02 
c  k            0.77386E-02      27   0.73854E-03   0.37504E+01 0.68137E+03 
c  omega        0.17398E+03      46   0.29137E-03   0.62299E+09 0.51396E+03 
c  TempC        0.39717E+04      66   0.17556E-01   0.12051E+06 0.19546E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.4252            81.7          4.1257          4.2831
v  Velocity[Y]            -9.9378          8.2666       0.0007404      0.00084383
v  Velocity[Z]            -21.676          23.641        -0.41296        -0.19359
v  ǁVelocityǁ           0.0019914          82.713          4.5745          4.4552
v  Pressure               -3148.7          51.411          21.874          30.494
v  k                   5.8084e-09          25.187         0.12063         0.10716
v  omega                    1e-24      5.8478e+05          5025.3          1407.4
v  TempC                  -134.17          598.99          63.621          69.569
v  Density                0.41027          2.3964          1.1447          1.1607
v  TurbVisc            3.4029e-14       0.0022898      0.00017311      0.00025156
v  CourantNb                    0          41.833           0.783         0.57253
v  FourierNb            0.0025074          4.6712          0.1634         0.21134
v  total_pressure           98176      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41082           2.247          1.0817            1.13


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016901           42.03          0.9464         0.78387


 TIME FOR THE TIME STEP              329:        0.63908E+02

===============================================================


 INSTANT    0.309300000E-01   TIME STEP NUMBER             330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.565922198E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856537E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61297E+02 0.13662E+02
   Friction velocity        uet   :  0.19846E-03 0.65906E+01
   Friction velocity        uk    :  0.10080E-01 0.27526E+01
   Dimensionless distance   yplus :  0.13133E+00 0.62394E+02
   Friction thermal sca.    tstar : -0.33373E+03 0.73836E+02
   Rough dim-less th. sca.  tplus :  0.97989E-01 0.13800E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     128831
   Nb of faces within the viscous sub-layer     :       9971
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1231 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21404E+00      36   0.35925E-01   0.37204E+02 0.12017E+03 
c  Velocity[X]                                      0.29609E+02 
c  Velocity[Y]                                      0.13657E+01 
c  Velocity[Z]                                      0.62289E+01 
c  Pressure     0.13807E-03     118   0.44518E-02   0.13014E+00 0.51385E+02 
c  k            0.77796E-02      28   0.72977E-03   0.37758E+01 0.68232E+03 
c  omega        0.17443E+03      46   0.20471E-03   0.55007E+09 0.48245E+03 
c  TempC        0.39774E+04      64   0.17808E-01   0.12081E+06 0.19538E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.5593          82.561          4.1277          4.2857
v  Velocity[Y]              -10.4          8.3814      0.00062903      0.00082827
v  Velocity[Z]            -21.769          23.481        -0.41632        -0.19477
v  ǁVelocityǁ           0.0036265          83.677          4.5785          4.4586
v  Pressure                 -3183          52.345          21.907          30.513
v  k                   6.2368e-09          25.824         0.12108         0.10749
v  omega                    1e-24      5.8388e+05          5028.1          1407.9
v  TempC                  -141.31          610.38           63.83          69.794
v  Density                0.40496          2.5413          1.1443          1.1603
v  TurbVisc            2.9406e-14         0.00229      0.00017369      0.00025237
v  CourantNb                    0          39.815         0.78374         0.57299
v  FourierNb            0.0025076          4.6712         0.16393         0.21203
v  total_pressure           98142      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41893          1.9363          1.0813          1.1296


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018913          40.008         0.94767         0.78502


 TIME FOR THE TIME STEP              330:        0.63971E+02

===============================================================


 INSTANT    0.310300000E-01   TIME STEP NUMBER             331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.780278271E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155852992E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59542E+02 0.13632E+02
   Friction velocity        uet   :  0.11266E-02 0.65719E+01
   Friction velocity        uk    :  0.13376E-01 0.27862E+01
   Dimensionless distance   yplus :  0.14692E+00 0.63524E+02
   Friction thermal sca.    tstar : -0.26549E+03 0.60530E+02
   Rough dim-less th. sca.  tplus :  0.10962E+00 0.13842E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     128661
   Nb of faces within the viscous sub-layer     :       9942
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1233 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21408E+00      37   0.34975E-01   0.38782E+02 0.12257E+03 
c  Velocity[X]                                      0.31055E+02 
c  Velocity[Y]                                      0.13977E+01 
c  Velocity[Z]                                      0.63290E+01 
c  Pressure     0.14056E-03     121   0.43922E-02   0.13100E+00 0.58891E+02 
c  k            0.78254E-02      28   0.72014E-03   0.37795E+01 0.68127E+03 
c  omega        0.60513E+23       2   0.13863E-15   0.49008E+09 0.45521E+03 
c  TempC        0.39832E+04      65   0.18362E-01   0.12167E+06 0.19575E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.6361          81.567          4.1297          4.2884
v  Velocity[Y]            -10.338           8.518      0.00054024       0.0008197
v  Velocity[Z]            -21.948          23.548         -0.4197        -0.19596
v  ǁVelocityǁ           0.0022451          82.693          4.5826          4.4619
v  Pressure               -3214.2          53.582          21.947          30.565
v  k                   7.8923e-09          25.869         0.12152         0.10782
v  omega               1.0922e-17      5.8451e+05          5029.3          1408.2
v  TempC                  -146.61          612.07          64.037          70.018
v  Density                0.39974          2.6789          1.1439          1.1599
v  TurbVisc             3.156e-14       0.0022899      0.00017427      0.00025319
v  CourantNb                    0          42.862         0.78448         0.57344
v  FourierNb            0.0025077          4.6712         0.16445         0.21272
v  total_pressure           98111      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4156          2.1369          1.0809          1.1292


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.0183          43.057         0.94893         0.78615


 TIME FOR THE TIME STEP              331:        0.61888E+02

===============================================================


 INSTANT    0.311300000E-01   TIME STEP NUMBER             332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.644955605E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856011E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61475E+02 0.13800E+02
   Friction velocity        uet   :  0.11315E-02 0.66248E+01
   Friction velocity        uk    :  0.79675E-02 0.27885E+01
   Dimensionless distance   yplus :  0.83856E-01 0.64079E+02
   Friction thermal sca.    tstar : -0.34656E+03 0.57585E+02
   Rough dim-less th. sca.  tplus :  0.62566E-01 0.13863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     128545
   Nb of faces within the viscous sub-layer     :       9926
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1236 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21414E+00      37   0.34572E-01   0.38975E+02 0.12275E+03 
c  Velocity[X]                                      0.31141E+02 
c  Velocity[Y]                                      0.14789E+01 
c  Velocity[Z]                                      0.63555E+01 
c  Pressure     0.14357E-03     116   0.45780E-02   0.13250E+00 0.52957E+02 
c  k            0.78677E-02      28   0.71828E-03   0.37911E+01 0.68099E+03 
c  omega        0.17503E+03      48   0.12518E-03   0.61960E+09 0.51107E+03 
c  TempC        0.39889E+04      67   0.17894E-01   0.12124E+06 0.19509E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.7149          83.359          4.1316           4.291
v  Velocity[Y]            -10.643          8.6644      0.00042285      0.00080559
v  Velocity[Z]            -21.988          23.289        -0.42301        -0.19714
v  ǁVelocityǁ           0.0021283          84.498          4.5865          4.4652
v  Pressure                 -3245          55.157          21.942          30.562
v  k                   1.1084e-08           26.07         0.12195         0.10815
v  omega               3.2949e-18      5.8401e+05          5032.8          1408.8
v  TempC                  -150.17          603.17          64.242          70.243
v  Density                0.39898           2.791          1.1435          1.1595
v  TurbVisc            3.9918e-14       0.0022899      0.00017476      0.00025386
v  CourantNb                    0          42.775         0.78521         0.57388
v  FourierNb            0.0025078          4.6712         0.16486         0.21325
v  total_pressure           98080      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41349          2.2674          1.0805          1.1288


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016025          42.978         0.95008         0.78714


 TIME FOR THE TIME STEP              332:        0.64065E+02

===============================================================


 INSTANT    0.312300000E-01   TIME STEP NUMBER             333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.217765733E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855643E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60727E+02 0.13698E+02
   Friction velocity        uet   :  0.20459E-02 0.65812E+01
   Friction velocity        uk    :  0.13523E-01 0.27991E+01
   Dimensionless distance   yplus :  0.13550E+00 0.64188E+02
   Friction thermal sca.    tstar : -0.31214E+03 0.54179E+02
   Rough dim-less th. sca.  tplus :  0.10110E+00 0.13867E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     128359
   Nb of faces within the viscous sub-layer     :       9905
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1243 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21420E+00      37   0.34688E-01   0.38718E+02 0.12222E+03 
c  Velocity[X]                                      0.30557E+02 
c  Velocity[Y]                                      0.14956E+01 
c  Velocity[Z]                                      0.66651E+01 
c  Pressure     0.14258E-03     119   0.45603E-02   0.13011E+00 0.52989E+02 
c  k            0.79181E-02      28   0.72217E-03   0.37859E+01 0.67912E+03 
c  omega        0.17574E+03      48   0.16491E-03   0.15125E+10 0.79595E+03 
c  TempC        0.39949E+04      65   0.17758E-01   0.12156E+06 0.19502E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.7625          83.554          4.1335          4.2936
v  Velocity[Y]            -10.816          8.6614      0.00030309      0.00078678
v  Velocity[Z]             -21.83          23.509         -0.4263         -0.1983
v  ǁVelocityǁ             0.00124          84.705          4.5905          4.4685
v  Pressure               -3279.4          56.246          21.954          30.565
v  k                   1.9387e-08           26.72         0.12238         0.10848
v  omega               8.9749e-19      8.8205e+05          5036.7          1409.4
v  TempC                  -150.21          605.76          64.445          70.467
v  Density                0.40303           2.872          1.1431          1.1591
v  TurbVisc            5.6029e-14       0.0022898      0.00017536      0.00025468
v  CourantNb                    0          39.994         0.78592         0.57433
v  FourierNb             0.002508          4.6712          0.1654         0.21395
v  total_pressure           98046      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41378          2.1586          1.0802          1.1284


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017152          40.193         0.95133         0.78828


 TIME FOR THE TIME STEP              333:        0.64130E+02

===============================================================


 INSTANT    0.313300000E-01   TIME STEP NUMBER             334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.592011571E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155856312E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61193E+02 0.13856E+02
   Friction velocity        uet   :  0.22960E-02 0.66376E+01
   Friction velocity        uk    :  0.14026E-01 0.28333E+01
   Dimensionless distance   yplus :  0.11796E+00 0.65346E+02
   Friction thermal sca.    tstar : -0.30335E+03 0.55470E+02
   Rough dim-less th. sca.  tplus :  0.88015E-01 0.13910E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     128246
   Nb of faces within the viscous sub-layer     :       9906
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1248 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21428E+00      38   0.37186E-01   0.38429E+02 0.12164E+03 
c  Velocity[X]                                      0.30601E+02 
c  Velocity[Y]                                      0.14262E+01 
c  Velocity[Z]                                      0.64024E+01 
c  Pressure     0.14222E-03     116   0.44046E-02   0.12817E+00 0.49560E+02 
c  k            0.79640E-02      29   0.72283E-03   0.37670E+01 0.67602E+03 
c  omega        0.53208E+05      27   0.49895E-06   0.11239E+10 0.68581E+03 
c  TempC        0.40009E+04      66   0.17745E-01   0.12216E+06 0.19518E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.846          84.572          4.1354          4.2963
v  Velocity[Y]            -10.904          8.7609      0.00020695      0.00077567
v  Velocity[Z]            -22.017          23.832        -0.42955        -0.19944
v  ǁVelocityǁ           0.0013245            85.8          4.5943          4.4718
v  Pressure               -3310.5          57.169          21.938          30.559
v  k                   1.2704e-08          26.852         0.12281         0.10881
v  omega               2.1383e-19      7.8932e+05          5039.8          1409.9
v  TempC                  -121.83          588.25          64.646          70.691
v  Density                0.40184          2.8729          1.1426          1.1587
v  TurbVisc            9.7976e-14       0.0022898      0.00017595      0.00025549
v  CourantNb                    0          42.687         0.78664         0.57477
v  FourierNb            0.0025081          4.6712         0.16594         0.21464
v  total_pressure           98015      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41502          2.1115          1.0798           1.128


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016596          42.888         0.95258         0.78941


 TIME FOR THE TIME STEP              334:        0.62936E+02

===============================================================


 INSTANT    0.314300000E-01   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.780407313E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855205E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61117E+02 0.14242E+02
   Friction velocity        uet   :  0.30770E-03 0.66956E+01
   Friction velocity        uk    :  0.98982E-02 0.28402E+01
   Dimensionless distance   yplus :  0.10491E+00 0.65729E+02
   Friction thermal sca.    tstar : -0.46618E+03 0.72446E+02
   Rough dim-less th. sca.  tplus :  0.78275E-01 0.13924E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     128186
   Nb of faces within the viscous sub-layer     :       9892
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1252 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21431E+00      38   0.36095E-01   0.38787E+02 0.12208E+03 
c  Velocity[X]                                      0.31002E+02 
c  Velocity[Y]                                      0.13630E+01 
c  Velocity[Z]                                      0.64224E+01 
c  Pressure     0.14205E-03     122   0.42086E-02   0.12646E+00 0.91658E+02 
c  k            0.80084E-02      29   0.71501E-03   0.37450E+01 0.67253E+03 
c  omega        0.17813E+03      47   0.12900E-03   0.12056E+10 0.70934E+03 
c  TempC        0.40071E+04      68   0.17507E-01   0.12240E+06 0.19506E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.8506          84.208          4.1372          4.2989
v  Velocity[Y]            -11.606          8.9357       0.0001168      0.00076337
v  Velocity[Z]            -22.417          23.459        -0.43278        -0.20057
v  ǁVelocityǁ           0.0021792          85.515          4.5981          4.4751
v  Pressure                 -3343          57.865          21.656          30.307
v  k                   2.3674e-08          27.526         0.12326         0.10915
v  omega               4.5356e-20      9.7151e+05          5043.2          1410.4
v  TempC                  -95.689          597.52          64.846          70.915
v  Density                0.41001          2.3341          1.1422          1.1583
v  TurbVisc            6.3744e-14       0.0022897      0.00017655      0.00025631
v  CourantNb                    0           43.33         0.78734          0.5752
v  FourierNb            0.0025083          4.6712         0.16648         0.21534
v  total_pressure           97982      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41561          2.3341          1.0794          1.1276


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015997          43.538         0.95382         0.79054


 TIME FOR THE TIME STEP              335:        0.64429E+02

===============================================================


 INSTANT    0.315300000E-01   TIME STEP NUMBER             336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028         0.310694927E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155861461E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60697E+02 0.14713E+02
   Friction velocity        uet   :  0.18720E-02 0.66775E+01
   Friction velocity        uk    :  0.88156E-02 0.28750E+01
   Dimensionless distance   yplus :  0.10160E+00 0.67087E+02
   Friction thermal sca.    tstar : -0.48609E+03 0.68910E+02
   Rough dim-less th. sca.  tplus :  0.75806E-01 0.13972E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127995
   Nb of faces within the viscous sub-layer     :       9921
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1256 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21440E+00      37   0.36724E-01   0.39037E+02 0.12236E+03 
c  Velocity[X]                                      0.31142E+02 
c  Velocity[Y]                                      0.14099E+01 
c  Velocity[Z]                                      0.64847E+01 
c  Pressure     0.14410E-03     117   0.41879E-02   0.12671E+00 0.83916E+02 
c  k            0.80483E-02      29   0.70724E-03   0.37310E+01 0.66979E+03 
c  omega        0.17817E+03      47   0.12059E-03   0.91381E+09 0.61711E+03 
c  TempC        0.40133E+04      66   0.17591E-01   0.12186E+06 0.19431E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.8956          84.863           4.139          4.3015
v  Velocity[Y]            -11.755           9.062      2.2913e-05      0.00075441
v  Velocity[Z]             -22.89          23.746        -0.43597         -0.2017
v  ǁVelocityǁ           0.0033366          86.156           4.602          4.4784
v  Pressure               -3379.6          58.583          21.398          30.047
v  k                   1.5656e-08           28.49         0.12372         0.10948
v  omega               8.4196e-21      7.3151e+05          5047.4          1410.9
v  TempC                   -113.1          601.07          65.048           71.14
v  Density                0.40564          1.9902          1.1418          1.1579
v  TurbVisc            1.4458e-13         0.00229      0.00017716      0.00025714
v  CourantNb                    0            41.4         0.78805         0.57564
v  FourierNb            0.0025084          4.6712         0.16703         0.21605
v  total_pressure           97945      1.0138e+05      1.0135e+05      1.0136e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41469          1.9902           1.079          1.1273


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015407          41.603         0.95508         0.79169


 TIME FOR THE TIME STEP              336:        0.64146E+02

===============================================================


 INSTANT    0.316300000E-01   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.738552867E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155860121E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61991E+02 0.15275E+02
   Friction velocity        uet   :  0.76722E-03 0.65036E+01
   Friction velocity        uk    :  0.13256E-01 0.29239E+01
   Dimensionless distance   yplus :  0.14422E+00 0.68326E+02
   Friction thermal sca.    tstar : -0.35583E+03 0.94280E+02
   Rough dim-less th. sca.  tplus :  0.10760E+00 0.14016E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127822
   Nb of faces within the viscous sub-layer     :       9926
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1257 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21445E+00      38   0.36453E-01   0.39471E+02 0.12291E+03 
c  Velocity[X]                                      0.31229E+02 
c  Velocity[Y]                                      0.14672E+01 
c  Velocity[Z]                                      0.67752E+01 
c  Pressure     0.14421E-03     120   0.43710E-02   0.12528E+00 0.99664E+02 
c  k            0.80885E-02      29   0.69842E-03   0.37315E+01 0.66840E+03 
c  omega        0.17900E+03      47   0.12634E-03   0.98170E+09 0.63871E+03 
c  TempC        0.40195E+04      66   0.17646E-01   0.12085E+06 0.19319E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.9805          88.491          4.1408          4.3041
v  Velocity[Y]            -11.575          9.1444     -0.00013322      0.00072568
v  Velocity[Z]            -22.403          23.704        -0.43914         -0.2028
v  ǁVelocityǁ           0.0041755          88.504          4.6058          4.4816
v  Pressure               -3406.8          58.617          21.065          29.719
v  k                   8.7722e-09          28.609         0.12419         0.10982
v  omega               1.3932e-21      9.5339e+05          5051.2          1411.4
v  TempC                  -123.79          597.71           65.25          71.366
v  Density                  0.404          2.2068          1.1414          1.1575
v  TurbVisc            7.8412e-14       0.0022902      0.00017777      0.00025796
v  CourantNb                    0          43.971         0.78875         0.57607
v  FourierNb            0.0025085          4.6712         0.16759         0.21676
v  total_pressure           97918      1.0138e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41479          2.2068          1.0786          1.1269


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014858          44.176         0.95634         0.79283


 TIME FOR THE TIME STEP              337:        0.64084E+02

===============================================================


 INSTANT    0.317300000E-01   TIME STEP NUMBER             338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.935382988E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155862560E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60455E+02 0.16678E+02
   Friction velocity        uet   :  0.79780E-03 0.66459E+01
   Friction velocity        uk    :  0.10508E-01 0.29286E+01
   Dimensionless distance   yplus :  0.13123E+00 0.68148E+02
   Friction thermal sca.    tstar : -0.45196E+03 0.14330E+03
   Rough dim-less th. sca.  tplus :  0.97913E-01 0.14010E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127680
   Nb of faces within the viscous sub-layer     :       9949
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1261 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21450E+00      38   0.37012E-01   0.38874E+02 0.12186E+03 
c  Velocity[X]                                      0.30818E+02 
c  Velocity[Y]                                      0.14664E+01 
c  Velocity[Z]                                      0.65894E+01 
c  Pressure     0.14552E-03     119   0.43933E-02   0.12484E+00 0.10587E+03 
c  k            0.81169E-02      29   0.68990E-03   0.37397E+01 0.66777E+03 
c  omega        0.63510E+13       2   0.25456E-12   0.75010E+09 0.55817E+03 
c  TempC        0.40255E+04      66   0.17718E-01   0.12109E+06 0.19307E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -9.062          86.784          4.1425          4.3067
v  Velocity[Y]            -11.549          9.1709     -0.00020549      0.00071485
v  Velocity[Z]            -23.005          23.472        -0.44221        -0.20388
v  ǁVelocityǁ           0.0045535          88.249          4.6096          4.4849
v  Pressure               -3438.1          58.958          20.735          29.367
v  k                   1.9206e-09          28.425         0.12467         0.11015
v  omega               2.0234e-22       5.853e+05            5054          1411.8
v  TempC                  -114.29           614.7          65.453          71.591
v  Density                0.40556          2.3647           1.141          1.1571
v  TurbVisc            3.2416e-14       0.0022901      0.00017838      0.00025878
v  CourantNb                    0           43.94         0.78944          0.5765
v  FourierNb            0.0025087          4.6712         0.16814         0.21747
v  total_pressure           97887      1.0138e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41996          2.3647          1.0783          1.1265


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014293          44.155         0.95758         0.79397


 TIME FOR THE TIME STEP              338:        0.62126E+02

===============================================================


 INSTANT    0.318300000E-01   TIME STEP NUMBER             339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.105685441E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155862579E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61855E+02 0.16984E+02
   Friction velocity        uet   :  0.10833E-02 0.67022E+01
   Friction velocity        uk    :  0.81975E-02 0.29211E+01
   Dimensionless distance   yplus :  0.13359E+00 0.68096E+02
   Friction thermal sca.    tstar : -0.40718E+03 0.87704E+02
   Rough dim-less th. sca.  tplus :  0.99677E-01 0.14008E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127550
   Nb of faces within the viscous sub-layer     :       9954
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1267 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21457E+00      37   0.35950E-01   0.38852E+02 0.12171E+03 
c  Velocity[X]                                      0.30646E+02 
c  Velocity[Y]                                      0.14425E+01 
c  Velocity[Z]                                      0.67630E+01 
c  Pressure     0.14352E-03     119   0.40771E-02   0.12157E+00 0.12208E+03 
c  k            0.81529E-02      30   0.68295E-03   0.37397E+01 0.66632E+03 
c  omega        0.17846E+03      48   0.13212E-03   0.85576E+09 0.59513E+03 
c  TempC        0.40315E+04      68   0.17677E-01   0.12192E+06 0.19341E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.0972          85.839          4.1442          4.3092
v  Velocity[Y]            -11.702          9.0827     -0.00029738      0.00069707
v  Velocity[Z]            -23.411          23.701        -0.44528        -0.20494
v  ǁVelocityǁ           0.0039164          87.341          4.6133          4.4881
v  Pressure               -3478.4          59.949          20.301          28.944
v  k                   1.6249e-08          29.678         0.12517         0.11048
v  omega               2.5303e-23      6.6675e+05          5058.5          1412.4
v  TempC                  -114.75          624.68          65.658          71.815
v  Density                0.39779          2.2232          1.1406          1.1566
v  TurbVisc            9.5571e-15       0.0022902      0.00017886      0.00025943
v  CourantNb                    0          41.832         0.79014         0.57693
v  FourierNb            0.0025088          4.6712         0.16857           0.218
v  total_pressure           97847      1.0138e+05      1.0135e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4173          2.2232          1.0779          1.1261


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013786          42.042          0.9587         0.79493


 TIME FOR THE TIME STEP              339:        0.64434E+02

===============================================================


 INSTANT    0.319300000E-01   TIME STEP NUMBER             340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.934207546E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155863792E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59763E+02 0.17660E+02
   Friction velocity        uet   :  0.20930E-02 0.66674E+01
   Friction velocity        uk    :  0.13724E-01 0.29841E+01
   Dimensionless distance   yplus :  0.15449E+00 0.69975E+02
   Friction thermal sca.    tstar : -0.40258E+03 0.66303E+02
   Rough dim-less th. sca.  tplus :  0.11527E+00 0.14073E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127404
   Nb of faces within the viscous sub-layer     :       9980
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1270 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21464E+00      38   0.38017E-01   0.39296E+02 0.12228E+03 
c  Velocity[X]                                      0.30992E+02 
c  Velocity[Y]                                      0.14556E+01 
c  Velocity[Z]                                      0.68484E+01 
c  Pressure     0.14489E-03     118   0.40894E-02   0.12117E+00 0.12310E+03 
c  k            0.81934E-02      29   0.68365E-03   0.37245E+01 0.66345E+03 
c  omega        0.80699E+10       2   0.18148E-09   0.58618E+10 0.15403E+04 
c  TempC        0.40374E+04      67   0.17667E-01   0.12181E+06 0.19301E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.1406           86.94          4.1458          4.3118
v  Velocity[Y]            -12.421           9.009     -0.00038677      0.00068622
v  Velocity[Z]            -23.665          24.089        -0.44824        -0.20598
v  ǁVelocityǁ           0.0051446          88.616          4.6169          4.4913
v  Pressure               -3518.1          60.919          19.887          28.518
v  k                   1.6596e-08          30.146         0.12567         0.11081
v  omega                2.547e-24       2.636e+06          5062.6            1413
v  TempC                  -125.78          595.56          65.865           72.04
v  Density                0.39338          2.2297          1.1402          1.1562
v  TurbVisc            9.0619e-14       0.0022899      0.00017946      0.00026026
v  CourantNb                    0          44.328          0.7908         0.57735
v  FourierNb             0.002509          4.6712         0.16912         0.21871
v  total_pressure           97807      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41739          2.2297          1.0775          1.1257


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013259          44.541         0.95992         0.79607


 TIME FOR THE TIME STEP              340:        0.62283E+02

===============================================================


 INSTANT    0.320300000E-01   TIME STEP NUMBER             341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.192106491E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155863847E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60956E+02 0.18725E+02
   Friction velocity        uet   :  0.22473E-02 0.67087E+01
   Friction velocity        uk    :  0.10297E-01 0.30063E+01
   Dimensionless distance   yplus :  0.11058E+00 0.70162E+02
   Friction thermal sca.    tstar : -0.36949E+03 0.56305E+02
   Rough dim-less th. sca.  tplus :  0.82507E-01 0.14079E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127268
   Nb of faces within the viscous sub-layer     :      10010
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1273 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21465E+00      38   0.35396E-01   0.40643E+02 0.12425E+03 
c  Velocity[X]                                      0.32290E+02 
c  Velocity[Y]                                      0.15064E+01 
c  Velocity[Z]                                      0.68470E+01 
c  Pressure     0.14907E-03     124   0.42206E-02   0.12284E+00 0.18687E+03 
c  k            0.82367E-02      30   0.68782E-03   0.37408E+01 0.66338E+03 
c  omega        0.26942E+03      46   0.12902E-03   0.29356E+10 0.10946E+04 
c  TempC        0.40433E+04      68   0.18121E-01   0.12141E+06 0.19239E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.5376          87.881          4.1475          4.3143
v  Velocity[Y]            -12.452          8.9655      -0.0005028      0.00066849
v  Velocity[Z]            -24.184          24.153        -0.45112        -0.20701
v  ǁVelocityǁ           0.0023887           89.51          4.6206          4.4945
v  Pressure               -3553.4          61.499          19.184          27.851
v  k                   9.0984e-09          30.858         0.12618         0.11115
v  omega                    1e-24       1.344e+06          5068.2          1413.7
v  TempC                  -103.72          608.69          66.071          72.265
v  Density                0.40656          2.3966          1.1397          1.1558
v  TurbVisc            1.0581e-13       0.0022899      0.00017994      0.00026091
v  CourantNb                    0          44.468         0.79147         0.57778
v  FourierNb            0.0025091          4.6712         0.16955         0.21925
v  total_pressure           97772      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4192          2.3966          1.0771          1.1253


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013368          44.691         0.96102         0.79703


 TIME FOR THE TIME STEP              341:        0.64496E+02

===============================================================


 INSTANT    0.321300000E-01   TIME STEP NUMBER             342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.763445489E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868141E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59078E+02 0.19630E+02
   Friction velocity        uet   :  0.20612E-02 0.67474E+01
   Friction velocity        uk    :  0.15287E-01 0.30416E+01
   Dimensionless distance   yplus :  0.15168E+00 0.71557E+02
   Friction thermal sca.    tstar : -0.35970E+03 0.50821E+02
   Rough dim-less th. sca.  tplus :  0.11317E+00 0.14126E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127128
   Nb of faces within the viscous sub-layer     :      10052
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1279 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21476E+00      39   0.38038E-01   0.38797E+02 0.12128E+03 
c  Velocity[X]                                      0.30545E+02 
c  Velocity[Y]                                      0.14792E+01 
c  Velocity[Z]                                      0.67732E+01 
c  Pressure     0.14513E-03     121   0.40409E-02   0.11784E+00 0.18053E+03 
c  k            0.82840E-02      30   0.68574E-03   0.37323E+01 0.66111E+03 
c  omega        0.19139E+03      47   0.98576E-03   0.14870E+11 0.24021E+04 
c  TempC        0.40490E+04      67   0.18146E-01   0.12176E+06 0.19236E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.7616          88.517          4.1492          4.3169
v  Velocity[Y]            -12.331          8.8894     -0.00059232      0.00065403
v  Velocity[Z]            -23.331          23.982          -0.454        -0.20802
v  ǁVelocityǁ          0.00098822          90.171          4.6243          4.4976
v  Pressure               -3591.9           61.97          18.542          27.199
v  k                    2.465e-09          31.571         0.12668         0.11148
v  omega                    1e-24      6.3116e+06          5076.6          1414.4
v  TempC                  -121.29          597.24          66.279          72.489
v  Density                0.40051          2.0846          1.1393          1.1554
v  TurbVisc            4.0055e-14       0.0022897      0.00018055      0.00026173
v  CourantNb                    0          42.139         0.79215          0.5782
v  FourierNb            0.0025093          4.6712         0.17011         0.21996
v  total_pressure           97733      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4156          2.0846          1.0767          1.1249


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014102          42.359         0.96226         0.79816


 TIME FOR THE TIME STEP              342:        0.64351E+02

===============================================================


 INSTANT    0.322300000E-01   TIME STEP NUMBER             343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.630441464E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866834E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60242E+02 0.20456E+02
   Friction velocity        uet   :  0.16480E-02 0.67072E+01
   Friction velocity        uk    :  0.14335E-01 0.30765E+01
   Dimensionless distance   yplus :  0.14040E+00 0.72466E+02
   Friction thermal sca.    tstar : -0.38890E+03 0.47806E+02
   Rough dim-less th. sca.  tplus :  0.10475E+00 0.14156E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     127012
   Nb of faces within the viscous sub-layer     :      10099
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1283 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21479E+00      39   0.37593E-01   0.39981E+02 0.12300E+03 
c  Velocity[X]                                      0.31567E+02 
c  Velocity[Y]                                      0.15419E+01 
c  Velocity[Z]                                      0.68725E+01 
c  Pressure     0.14896E-03     120   0.41004E-02   0.11925E+00 0.15612E+03 
c  k            0.83271E-02      30   0.67937E-03   0.37144E+01 0.65795E+03 
c  omega        0.68281E+23       2   0.21913E-22   0.42645E+10 0.13121E+04 
c  TempC        0.40548E+04      67   0.17983E-01   0.12271E+06 0.19280E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.9615          87.923          4.1508          4.3194
v  Velocity[Y]            -12.444          8.7912     -0.00068221      0.00064879
v  Velocity[Z]            -23.557          24.062        -0.45679          -0.209
v  ǁVelocityǁ           0.0019475          89.664          4.6279          4.5008
v  Pressure               -3630.7          62.305          18.028           26.66
v  k                   7.5974e-09           32.79         0.12717         0.11181
v  omega               1.1772e-16      3.1733e+06          5078.3          1414.7
v  TempC                  -123.89          595.57          66.486          72.714
v  Density                0.40577          2.3257          1.1389           1.155
v  TurbVisc            1.1474e-14       0.0022898      0.00018114      0.00026255
v  CourantNb                    0          44.769         0.79282         0.57862
v  FourierNb            0.0025094          4.6712         0.17066         0.22066
v  total_pressure           97694      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40577          2.3257          1.0763          1.1245


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01472          44.991         0.96347         0.79928


 TIME FOR THE TIME STEP              343:        0.62283E+02

===============================================================


 INSTANT    0.323300000E-01   TIME STEP NUMBER             344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.100401213E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155865572E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58648E+02 0.21863E+02
   Friction velocity        uet   :  0.15892E-02 0.67706E+01
   Friction velocity        uk    :  0.12169E-01 0.31353E+01
   Dimensionless distance   yplus :  0.11842E+00 0.73528E+02
   Friction thermal sca.    tstar : -0.43102E+03 0.45997E+02
   Rough dim-less th. sca.  tplus :  0.88352E-01 0.14191E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     126878
   Nb of faces within the viscous sub-layer     :      10155
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1284 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21486E+00      38   0.38165E-01   0.39400E+02 0.12199E+03 
c  Velocity[X]                                      0.31022E+02 
c  Velocity[Y]                                      0.15162E+01 
c  Velocity[Z]                                      0.68620E+01 
c  Pressure     0.14835E-03     125   0.39748E-02   0.11705E+00 0.19954E+03 
c  k            0.83708E-02      30   0.67515E-03   0.37061E+01 0.65575E+03 
c  omega        0.22640E+03      46   0.22158E-03   0.15599E+10 0.79668E+03 
c  TempC        0.40606E+04      68   0.17718E-01   0.12309E+06 0.19279E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.3865          89.589          4.1524          4.3219
v  Velocity[Y]            -12.632          8.6496     -0.00074665      0.00063495
v  Velocity[Z]            -23.734          24.171        -0.45953        -0.20997
v  ǁVelocityǁ           0.0036047          91.385          4.6314          4.5039
v  Pressure               -3675.3          62.961          17.298          25.962
v  k                   3.1387e-09          33.192         0.12765         0.11214
v  omega               1.1979e-16      1.6036e+06            5083          1415.3
v  TempC                  -123.03          614.69          66.695          72.938
v  Density                0.40655          2.3662          1.1385          1.1546
v  TurbVisc            3.2137e-14       0.0022897      0.00018162      0.00026319
v  CourantNb                    0          45.083         0.79345         0.57903
v  FourierNb            0.0025096          4.6712         0.17108          0.2212
v  total_pressure           97650      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41553          2.3662           1.076          1.1241


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015363          45.317         0.96453         0.80023


 TIME FOR THE TIME STEP              344:        0.64501E+02

===============================================================


 INSTANT    0.324300000E-01   TIME STEP NUMBER             345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.967819975E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868661E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59789E+02 0.23196E+02
   Friction velocity        uet   :  0.43332E-03 0.67291E+01
   Friction velocity        uk    :  0.93159E-02 0.31545E+01
   Dimensionless distance   yplus :  0.92587E-01 0.74088E+02
   Friction thermal sca.    tstar : -0.60601E+03 0.53703E+02
   Rough dim-less th. sca.  tplus :  0.69080E-01 0.14209E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     126708
   Nb of faces within the viscous sub-layer     :      10218
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1288 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21489E+00      39   0.38620E-01   0.40537E+02 0.12363E+03 
c  Velocity[X]                                      0.32046E+02 
c  Velocity[Y]                                      0.15314E+01 
c  Velocity[Z]                                      0.69593E+01 
c  Pressure     0.15048E-03     126   0.39434E-02   0.11690E+00 0.23355E+03 
c  k            0.84163E-02      30   0.66998E-03   0.36967E+01 0.65346E+03 
c  omega        0.18502E+03      47   0.17197E-03   0.10307E+10 0.64720E+03 
c  TempC        0.40665E+04      67   0.18010E-01   0.12150E+06 0.19123E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.3312          89.872           4.154          4.3244
v  Velocity[Y]            -13.308          8.5315     -0.00084567      0.00061876
v  Velocity[Z]            -24.288           24.33        -0.46222        -0.21091
v  ǁVelocityǁ           0.0035817          91.752           4.635           4.507
v  Pressure               -3714.6          64.149          16.461          25.144
v  k                    3.549e-09           34.17         0.12813         0.11247
v  omega               1.2186e-16       8.177e+05          5089.6            1416
v  TempC                   -112.5          597.37          66.904          73.164
v  Density                 0.3978          2.3527           1.138          1.1542
v  TurbVisc            1.5737e-14         0.00229      0.00018223      0.00026401
v  CourantNb                    0          42.884         0.79409         0.57944
v  FourierNb            0.0025097          4.6712         0.17165         0.22191
v  total_pressure           97610      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41524          2.3527          1.0756          1.1238


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014797          43.112         0.96573         0.80136


 TIME FOR THE TIME STEP              345:        0.64916E+02

===============================================================


 INSTANT    0.325300000E-01   TIME STEP NUMBER             346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.147861713E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870020E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57880E+02 0.24098E+02
   Friction velocity        uet   :  0.69559E-03 0.67964E+01
   Friction velocity        uk    :  0.13004E-01 0.32007E+01
   Dimensionless distance   yplus :  0.12923E+00 0.76238E+02
   Friction thermal sca.    tstar : -0.39426E+03 0.51616E+02
   Rough dim-less th. sca.  tplus :  0.96424E-01 0.14277E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     126621
   Nb of faces within the viscous sub-layer     :      10275
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1294 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21496E+00      39   0.37762E-01   0.40176E+02 0.12297E+03 
c  Velocity[X]                                      0.31551E+02 
c  Velocity[Y]                                      0.15415E+01 
c  Velocity[Z]                                      0.70837E+01 
c  Pressure     0.14990E-03     122   0.39144E-02   0.11478E+00 0.22705E+03 
c  k            0.84704E-02      29   0.66243E-03   0.36980E+01 0.65217E+03 
c  omega        0.18245E+03      47   0.20298E-03   0.10571E+10 0.65418E+03 
c  TempC        0.40722E+04      67   0.18176E-01   0.12135E+06 0.19082E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.3555          90.386          4.1556          4.3269
v  Velocity[Y]            -13.144          8.4329      -0.0009032      0.00061646
v  Velocity[Z]            -24.705          24.483        -0.46485        -0.21183
v  ǁVelocityǁ           0.0035632          92.274          4.6385          4.5101
v  Pressure               -3753.8           64.97          15.667          24.354
v  k                   3.9828e-09           35.07         0.12859         0.11279
v  omega               1.8468e-17       5.837e+05          5096.1          1416.6
v  TempC                  -128.95          614.71          67.114          73.389
v  Density                0.40571          2.1985          1.1376          1.1538
v  TurbVisc            2.3841e-14       0.0022903      0.00018285      0.00026484
v  CourantNb                    0          45.205         0.79475         0.57986
v  FourierNb            0.0025099          4.6712         0.17221         0.22263
v  total_pressure           97571      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41442          2.1985          1.0752          1.1234


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01414          45.437         0.96696         0.80249


 TIME FOR THE TIME STEP              346:        0.64785E+02

===============================================================


 INSTANT    0.326300000E-01   TIME STEP NUMBER             347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.117301131E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869248E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58717E+02 0.25112E+02
   Friction velocity        uet   :  0.83572E-03 0.68130E+01
   Friction velocity        uk    :  0.92630E-02 0.32426E+01
   Dimensionless distance   yplus :  0.10787E+00 0.75940E+02
   Friction thermal sca.    tstar : -0.42947E+03 0.48775E+02
   Rough dim-less th. sca.  tplus :  0.80486E-01 0.14268E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     126573
   Nb of faces within the viscous sub-layer     :      10322
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1303 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21501E+00      39   0.39091E-01   0.39226E+02 0.12140E+03 
c  Velocity[X]                                      0.30660E+02 
c  Velocity[Y]                                      0.15283E+01 
c  Velocity[Z]                                      0.70376E+01 
c  Pressure     0.14949E-03     132   0.39925E-02   0.11258E+00 0.29990E+03 
c  k            0.85188E-02      30   0.65058E-03   0.36912E+01 0.65018E+03 
c  omega        0.18285E+03      48   0.17170E-03   0.71078E+09 0.53595E+03 
c  TempC        0.40780E+04      69   0.18365E-01   0.12238E+06 0.19132E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.6073          90.246          4.1571          4.3294
v  Velocity[Y]            -14.096            8.33     -0.00095736      0.00061209
v  Velocity[Z]            -24.886          24.681        -0.46745        -0.21275
v  ǁVelocityǁ           0.0050262          92.325           4.642          4.5132
v  Pressure                 -3797          65.335          14.601          23.328
v  k                   7.4523e-09          36.028         0.12904         0.11312
v  omega               2.1265e-18      5.8335e+05          5100.7          1417.1
v  TempC                  -107.04          600.84          67.322          73.613
v  Density                0.39779          2.4493          1.1372          1.1534
v  TurbVisc            2.9842e-14       0.0022902      0.00018345      0.00026566
v  CourantNb                    0          45.714         0.79536         0.58027
v  FourierNb            0.0025101          4.6712         0.17276         0.22334
v  total_pressure           97528      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39779          2.4493          1.0748           1.123


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013088          45.958         0.96813          0.8036


 TIME FOR THE TIME STEP              347:        0.65306E+02

===============================================================


 INSTANT    0.327300000E-01   TIME STEP NUMBER             348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.845438750E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155873066E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57304E+02 0.26804E+02
   Friction velocity        uet   :  0.18423E-02 0.67778E+01
   Friction velocity        uk    :  0.10093E-01 0.32866E+01
   Dimensionless distance   yplus :  0.12350E+00 0.78052E+02
   Friction thermal sca.    tstar : -0.47868E+03 0.56269E+02
   Rough dim-less th. sca.  tplus :  0.92142E-01 0.14333E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     126492
   Nb of faces within the viscous sub-layer     :      10378
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1306 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21507E+00      39   0.39749E-01   0.40057E+02 0.12257E+03 
c  Velocity[X]                                      0.31469E+02 
c  Velocity[Y]                                      0.15072E+01 
c  Velocity[Z]                                      0.70804E+01 
c  Pressure     0.14971E-03     123   0.37678E-02   0.11102E+00 0.29181E+03 
c  k            0.85739E-02      29   0.64048E-03   0.36849E+01 0.64824E+03 
c  omega        0.10214E+08      11   0.29933E-07   0.46500E+12 0.80783E+04 
c  TempC        0.40838E+04      68   0.17790E-01   0.12193E+06 0.19067E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.6375          91.521          4.1586          4.3319
v  Velocity[Y]            -14.019          8.1397      -0.0010184      0.00061155
v  Velocity[Z]            -24.636          24.665        -0.46996        -0.21363
v  ǁVelocityǁ           0.0042036          93.616          4.6455          4.5163
v  Pressure               -3843.3          66.038          13.648          22.342
v  k                   4.2782e-10          36.618         0.12948         0.11345
v  omega               2.4869e-19      3.7921e+07          5127.8          1418.9
v  TempC                  -124.83          620.51           67.53          73.838
v  Density                0.40411          2.1262          1.1368           1.153
v  TurbVisc            4.4229e-14       0.0022901      0.00018406      0.00026649
v  CourantNb                    0           43.85         0.79597         0.58068
v  FourierNb            0.0025103          4.6712         0.17331         0.22405
v  total_pressure           97482      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41508          2.1262          1.0744          1.1226


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.011013          44.089         0.96929         0.80472


 TIME FOR THE TIME STEP              348:        0.63132E+02

===============================================================


 INSTANT    0.328300000E-01   TIME STEP NUMBER             349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.145466392E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872123E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58301E+02 0.28080E+02
   Friction velocity        uet   :  0.27717E-02 0.67400E+01
   Friction velocity        uk    :  0.65356E-02 0.33135E+01
   Dimensionless distance   yplus :  0.85959E-01 0.80004E+02
   Friction thermal sca.    tstar : -0.53540E+03 0.52065E+02
   Rough dim-less th. sca.  tplus :  0.64135E-01 0.14392E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     126362
   Nb of faces within the viscous sub-layer     :      10396
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1314 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21511E+00      39   0.39494E-01   0.40657E+02 0.12337E+03 
c  Velocity[X]                                      0.31820E+02 
c  Velocity[Y]                                      0.15426E+01 
c  Velocity[Z]                                      0.72938E+01 
c  Pressure     0.15144E-03     123   0.37528E-02   0.11044E+00 0.27815E+03 
c  k            0.86251E-02      29   0.64211E-03   0.37029E+01 0.64846E+03 
c  omega        0.14332E+05      31   0.96687E-05   0.11653E+12 0.56492E+04 
c  TempC        0.40896E+04      70   0.18325E-01   0.12125E+06 0.18985E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.7115          91.024          4.1601          4.3344
v  Velocity[Y]             -14.21          7.9528      -0.0010497      0.00060318
v  Velocity[Z]            -25.514          24.468        -0.47243         -0.2145
v  ǁVelocityǁ           0.0039091          93.211          4.6489          4.5194
v  Pressure               -3883.5          66.379          12.725           21.42
v  k                   1.3915e-09           37.76         0.12992         0.11377
v  omega               3.1686e-20      1.8985e+07          5121.4          1418.8
v  TempC                  -127.88          583.02          67.738          74.063
v  Density                0.39521          2.3812          1.1364          1.1526
v  TurbVisc            2.4427e-15       0.0022901      0.00018468      0.00026732
v  CourantNb                    0          46.182         0.79662         0.58109
v  FourierNb            0.0025104          4.6712         0.17388         0.22476
v  total_pressure           97442      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41889          2.3812           1.074          1.1222


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012455          46.423         0.97049         0.80585


 TIME FOR THE TIME STEP              349:        0.64268E+02

===============================================================


 INSTANT    0.329300000E-01   TIME STEP NUMBER             350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.159118423E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871525E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56403E+02 0.28996E+02
   Friction velocity        uet   :  0.25318E-02 0.68599E+01
   Friction velocity        uk    :  0.12393E-01 0.33648E+01
   Dimensionless distance   yplus :  0.13312E+00 0.79348E+02
   Friction thermal sca.    tstar : -0.31132E+03 0.57240E+02
   Rough dim-less th. sca.  tplus :  0.99324E-01 0.14372E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     126265
   Nb of faces within the viscous sub-layer     :      10418
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1317 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21517E+00      39   0.41089E-01   0.40536E+02 0.12308E+03 
c  Velocity[X]                                      0.31824E+02 
c  Velocity[Y]                                      0.15966E+01 
c  Velocity[Z]                                      0.71153E+01 
c  Pressure     0.15432E-03     123   0.36655E-02   0.11084E+00 0.30009E+03 
c  k            0.86813E-02      29   0.64633E-03   0.37107E+01 0.64777E+03 
c  omega        0.36073E+04      36   0.19710E-04   0.30374E+11 0.32986E+04 
c  TempC        0.40954E+04      68   0.18089E-01   0.12184E+06 0.19001E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.7999          93.686          4.1616          4.3369
v  Velocity[Y]             -14.51          7.7778       -0.001074      0.00059506
v  Velocity[Z]            -25.652          24.892        -0.47489        -0.21535
v  ǁVelocityǁ           0.0038119          95.853          4.6523          4.5225
v  Pressure               -3927.5           67.22          11.744          20.436
v  k                   3.6224e-09          38.022         0.13036         0.11409
v  omega               3.9663e-21      9.5171e+06          5120.6          1418.9
v  TempC                   -124.4          586.52          67.944          74.288
v  Density                0.41252          2.4312          1.1359          1.1522
v  TurbVisc            5.4973e-15         0.00229      0.00018528      0.00026814
v  CourantNb                    0          46.647         0.79724         0.58149
v  FourierNb            0.0025106          4.6712         0.17443         0.22547
v  total_pressure           97397      1.0139e+05      1.0134e+05      1.0135e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41731          2.4312          1.0736          1.1218


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012561          46.901         0.97167         0.80696


 TIME FOR THE TIME STEP              350:        0.63929E+02

===============================================================


 INSTANT    0.330300000E-01   TIME STEP NUMBER             351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.145988654E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155872227E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57224E+02 0.30014E+02
   Friction velocity        uet   :  0.20728E-02 0.68341E+01
   Friction velocity        uk    :  0.12830E-01 0.33765E+01
   Dimensionless distance   yplus :  0.13050E+00 0.79981E+02
   Friction thermal sca.    tstar : -0.30319E+03 0.63274E+02
   Rough dim-less th. sca.  tplus :  0.97368E-01 0.14391E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     126094
   Nb of faces within the viscous sub-layer     :      10466
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1320 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21522E+00      39   0.39364E-01   0.40245E+02 0.12253E+03 
c  Velocity[X]                                      0.31454E+02 
c  Velocity[Y]                                      0.15637E+01 
c  Velocity[Z]                                      0.72269E+01 
c  Pressure     0.15307E-03     122   0.36153E-02   0.10815E+00 0.26697E+03 
c  k            0.87333E-02      30   0.64455E-03   0.36913E+01 0.64458E+03 
c  omega        0.93808E+03      41   0.40144E-03   0.63885E+12 0.84798E+04 
c  TempC        0.41014E+04      68   0.18064E-01   0.12224E+06 0.19003E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.8543          92.265          4.1629          4.3394
v  Velocity[Y]            -14.476          7.5954       -0.001154      0.00058118
v  Velocity[Z]            -25.199          25.113        -0.47725        -0.21619
v  ǁVelocityǁ           0.0054307          94.593          4.6556          4.5255
v  Pressure                 -3977          67.157          10.883          19.579
v  k                   4.3032e-10          39.642         0.13081         0.11442
v  omega               5.3034e-22      3.5926e+07          5142.8          1421.1
v  TempC                   -114.1          589.17          68.151          74.513
v  Density                0.41084          2.3743          1.1355          1.1518
v  TurbVisc            1.5603e-14       0.0022899      0.00018588      0.00026897
v  CourantNb                    0          44.689         0.79785          0.5819
v  FourierNb            0.0025108          4.6712         0.17497         0.22617
v  total_pressure           97348      1.0139e+05      1.0134e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41906          2.3743          1.0732          1.1214


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012953          44.938         0.97283         0.80807


 TIME FOR THE TIME STEP              351:        0.64462E+02

===============================================================


 INSTANT    0.331300000E-01   TIME STEP NUMBER             352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.116383081E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870951E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55754E+02 0.31075E+02
   Friction velocity        uet   :  0.12709E-02 0.68048E+01
   Friction velocity        uk    :  0.10279E-01 0.34477E+01
   Dimensionless distance   yplus :  0.13379E+00 0.83246E+02
   Friction thermal sca.    tstar : -0.37959E+03 0.69174E+02
   Rough dim-less th. sca.  tplus :  0.99824E-01 0.14486E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125996
   Nb of faces within the viscous sub-layer     :      10460
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1327 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21526E+00      40   0.39357E-01   0.39599E+02 0.12144E+03 
c  Velocity[X]                                      0.30867E+02 
c  Velocity[Y]                                      0.15411E+01 
c  Velocity[Z]                                      0.71905E+01 
c  Pressure     0.15150E-03     117   0.36430E-02   0.10540E+00 0.23263E+03 
c  k            0.87932E-02      30   0.63720E-03   0.36646E+01 0.64075E+03 
c  omega        0.20656E+05      31   0.90932E-05   0.15981E+12 0.62391E+04 
c  TempC        0.41074E+04      67   0.17934E-01   0.12279E+06 0.19016E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.9832          94.013          4.1642          4.3419
v  Velocity[Y]            -15.006          7.5433      -0.0012127      0.00057584
v  Velocity[Z]            -25.915          25.239        -0.47962        -0.21702
v  ǁVelocityǁ           0.0072039          96.501          4.6589          4.5285
v  Pressure               -4019.8          65.442          10.156          18.841
v  k                   1.1623e-09          40.649         0.13128         0.11475
v  omega               6.7068e-23      1.7986e+07          5134.1          1420.4
v  TempC                  -128.38          610.89          68.359          74.739
v  Density                0.40958          2.2205          1.1351          1.1514
v  TurbVisc            1.8539e-15       0.0022902      0.00018648      0.00026979
v  CourantNb                    0          47.313         0.79846          0.5823
v  FourierNb             0.002511          4.6712         0.17553         0.22688
v  total_pressure           97305      1.0139e+05      1.0134e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41692          2.2205          1.0728           1.121


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013955          47.564         0.97398         0.80917


 TIME FOR THE TIME STEP              352:        0.63916E+02

===============================================================


 INSTANT    0.332300000E-01   TIME STEP NUMBER             353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.226162195E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868706E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56330E+02 0.32385E+02
   Friction velocity        uet   :  0.24244E-03 0.68841E+01
   Friction velocity        uk    :  0.13491E-01 0.34913E+01
   Dimensionless distance   yplus :  0.13401E+00 0.82375E+02
   Friction thermal sca.    tstar : -0.38824E+03 0.83405E+02
   Rough dim-less th. sca.  tplus :  0.99987E-01 0.14461E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125912
   Nb of faces within the viscous sub-layer     :      10453
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1333 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21530E+00      39   0.39736E-01   0.40868E+02 0.12327E+03 
c  Velocity[X]                                      0.31857E+02 
c  Velocity[Y]                                      0.16237E+01 
c  Velocity[Z]                                      0.73873E+01 
c  Pressure     0.15503E-03     123   0.37155E-02   0.10595E+00 0.24989E+03 
c  k            0.88389E-02      30   0.63217E-03   0.36546E+01 0.63844E+03 
c  omega        0.51991E+04      35   0.25372E-04   0.40487E+11 0.37295E+04 
c  TempC        0.41134E+04      69   0.18882E-01   0.12176E+06 0.18906E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.6799          94.013          4.1657          4.3443
v  Velocity[Y]            -15.351           7.602      -0.0012467       0.0005725
v  Velocity[Z]            -24.877          25.235        -0.48193        -0.21783
v  ǁVelocityǁ           0.0063491          96.486          4.6623          4.5315
v  Pressure               -4065.9          65.364          9.3583          18.072
v  k                   1.1068e-08          41.848         0.13176         0.11508
v  omega               8.5103e-24      9.0156e+06          5131.3          1420.2
v  TempC                   -108.9          597.33           68.57          74.965
v  Density                0.39951          2.4396          1.1346          1.1509
v  TurbVisc            5.8418e-15       0.0022904      0.00018708      0.00027062
v  CourantNb                    0          47.863         0.79907         0.58269
v  FourierNb            0.0025111          4.6712         0.17608         0.22759
v  total_pressure           97259      1.0139e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39951          2.4396          1.0724          1.1206


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013529          48.127         0.97514         0.81028


 TIME FOR THE TIME STEP              353:        0.64290E+02

===============================================================


 INSTANT    0.333300000E-01   TIME STEP NUMBER             354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.179047359E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870210E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55049E+02 0.33683E+02
   Friction velocity        uet   :  0.14127E-02 0.68234E+01
   Friction velocity        uk    :  0.89466E-02 0.35424E+01
   Dimensionless distance   yplus :  0.15308E+00 0.84004E+02
   Friction thermal sca.    tstar : -0.24091E+03 0.10441E+03
   Rough dim-less th. sca.  tplus :  0.11422E+00 0.14508E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125884
   Nb of faces within the viscous sub-layer     :      10477
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1338 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21538E+00      40   0.41206E-01   0.40643E+02 0.12282E+03 
c  Velocity[X]                                      0.31930E+02 
c  Velocity[Y]                                      0.15590E+01 
c  Velocity[Z]                                      0.71537E+01 
c  Pressure     0.15422E-03     122   0.35429E-02   0.10367E+00 0.25497E+03 
c  k            0.88985E-02      29   0.62380E-03   0.36630E+01 0.63780E+03 
c  omega        0.13273E+04      40   0.58266E-04   0.11463E+11 0.20906E+04 
c  TempC        0.41191E+04      71   0.18117E-01   0.12141E+06 0.18850E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.8731          95.751          4.1671          4.3468
v  Velocity[Y]            -15.597          7.2432      -0.0012846      0.00057223
v  Velocity[Z]            -25.536          24.968        -0.48424        -0.21863
v  ǁVelocityǁ           0.0034968          98.368          4.6658          4.5346
v  Pressure               -4117.9          63.338          8.5343          17.285
v  k                   2.5592e-09          42.726         0.13224         0.11541
v  omega                    1e-24      4.5301e+06          5134.3          1420.6
v  TempC                  -126.37          599.61          68.783          75.191
v  Density                0.40573          2.1503          1.1342          1.1505
v  TurbVisc            3.6145e-14       0.0022903      0.00018769      0.00027145
v  CourantNb                    0          44.999         0.79969         0.58309
v  FourierNb            0.0025113          4.6712         0.17663          0.2283
v  total_pressure           97207      1.0139e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40573          2.1503          1.0719          1.1202


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012746          45.259         0.97632         0.81139


 TIME FOR THE TIME STEP              354:        0.64558E+02

===============================================================


 INSTANT    0.334300000E-01   TIME STEP NUMBER             355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.170193564E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870509E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55784E+02 0.35037E+02
   Friction velocity        uet   :  0.14101E-02 0.67958E+01
   Friction velocity        uk    :  0.10415E-01 0.35795E+01
   Dimensionless distance   yplus :  0.10435E+00 0.85829E+02
   Friction thermal sca.    tstar : -0.25829E+03 0.12097E+03
   Rough dim-less th. sca.  tplus :  0.77856E-01 0.14559E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125725
   Nb of faces within the viscous sub-layer     :      10509
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1343 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21542E+00      40   0.40344E-01   0.40395E+02 0.12234E+03 
c  Velocity[X]                                      0.31470E+02 
c  Velocity[Y]                                      0.15759E+01 
c  Velocity[Z]                                      0.73487E+01 
c  Pressure     0.15527E-03     119   0.34708E-02   0.10262E+00 0.22500E+03 
c  k            0.89492E-02      30   0.62255E-03   0.36753E+01 0.63749E+03 
c  omega        0.38523E+03      45   0.12543E-03   0.41961E+10 0.12814E+04 
c  TempC        0.41249E+04      69   0.18491E-01   0.12162E+06 0.18837E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.4982          95.135          4.1685          4.3493
v  Velocity[Y]            -16.173          7.7403      -0.0012942      0.00057116
v  Velocity[Z]            -26.157          25.342        -0.48651        -0.21943
v  ǁVelocityǁ           0.0061705          97.953          4.6691          4.5376
v  Pressure                 -4171          59.765           7.854          16.603
v  k                   1.2528e-09          44.897         0.13272         0.11573
v  omega                    1e-24      2.2869e+06            5137          1420.8
v  TempC                  -129.69          605.58          68.997          75.417
v  Density                0.40467          2.4061          1.1338          1.1501
v  TurbVisc             1.346e-14       0.0022901      0.00018828      0.00027228
v  CourantNb                    0          48.132         0.80032          0.5835
v  FourierNb            0.0025115          4.6712         0.17718           0.229
v  total_pressure           97154      1.0138e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41423          2.4061          1.0715          1.1198


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012699          48.394          0.9775          0.8125


 TIME FOR THE TIME STEP              355:        0.64738E+02

===============================================================


 INSTANT    0.335300000E-01   TIME STEP NUMBER             356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.185638487E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869626E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54361E+02 0.36305E+02
   Friction velocity        uet   :  0.15066E-02 0.69063E+01
   Friction velocity        uk    :  0.11803E-01 0.36694E+01
   Dimensionless distance   yplus :  0.12063E+00 0.86200E+02
   Friction thermal sca.    tstar : -0.29110E+03 0.88391E+02
   Rough dim-less th. sca.  tplus :  0.90007E-01 0.14569E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125707
   Nb of faces within the viscous sub-layer     :      10554
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1344 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21546E+00      40   0.40761E-01   0.40301E+02 0.12209E+03 
c  Velocity[X]                                      0.31376E+02 
c  Velocity[Y]                                      0.15380E+01 
c  Velocity[Z]                                      0.73871E+01 
c  Pressure     0.15490E-03     118   0.34311E-02   0.10068E+00 0.21583E+03 
c  k            0.90097E-02      30   0.62079E-03   0.36641E+01 0.63512E+03 
c  omega        0.20785E+03      47   0.17260E-03   0.21357E+10 0.91670E+03 
c  TempC        0.41305E+04      72   0.17974E-01   0.12263E+06 0.18886E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.13          97.208            4.17          4.3518
v  Velocity[Y]            -14.411          7.8511      -0.0012829      0.00057524
v  Velocity[Z]            -26.258          25.228        -0.48879        -0.22021
v  ǁVelocityǁ           0.0057309          99.626          4.6725          4.5407
v  Pressure               -4219.8          55.551          7.1999          15.959
v  k                   1.4334e-09          46.029         0.13321         0.11605
v  omega                    1e-24      1.1644e+06            5141          1421.3
v  TempC                  -124.92          608.05          69.214          75.643
v  Density                0.40192          2.4619          1.1333          1.1497
v  TurbVisc             3.736e-15       0.0022899      0.00018887       0.0002731
v  CourantNb                    0          48.651         0.80093         0.58389
v  FourierNb            0.0025117          4.6712         0.17772          0.2297
v  total_pressure           97105      1.0138e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41725          2.4619          1.0711          1.1194


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013559          48.928         0.97865          0.8136


 TIME FOR THE TIME STEP              356:        0.64455E+02

===============================================================


 INSTANT    0.336300000E-01   TIME STEP NUMBER             357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.157204917E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155868515E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55368E+02 0.37672E+02
   Friction velocity        uet   :  0.16557E-02 0.68720E+01
   Friction velocity        uk    :  0.13982E-01 0.37154E+01
   Dimensionless distance   yplus :  0.14657E+00 0.87685E+02
   Friction thermal sca.    tstar : -0.28811E+03 0.71520E+02
   Rough dim-less th. sca.  tplus :  0.10936E+00 0.14610E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125569
   Nb of faces within the viscous sub-layer     :      10581
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1344 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21553E+00      40   0.41610E-01   0.40022E+02 0.12156E+03 
c  Velocity[X]                                      0.31093E+02 
c  Velocity[Y]                                      0.15842E+01 
c  Velocity[Z]                                      0.73441E+01 
c  Pressure     0.15611E-03     113   0.33192E-02   0.99550E-01 0.20023E+03 
c  k            0.90712E-02      30   0.61876E-03   0.36619E+01 0.63350E+03 
c  omega        0.19159E+03      48   0.61283E-03   0.44509E+11 0.38699E+04 
c  TempC        0.41362E+04      71   0.18507E-01   0.12215E+06 0.18820E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.659          96.157          4.1714          4.3543
v  Velocity[Y]            -15.705           7.591      -0.0013177       0.0005681
v  Velocity[Z]            -26.903          25.643        -0.49106        -0.22099
v  ǁVelocityǁ           0.0054562            98.7          4.6758          4.5437
v  Pressure                 -4284          53.443          6.5929          15.378
v  k                   5.7138e-09          47.601         0.13368         0.11638
v  omega                    1e-24      8.5501e+06          5150.2          1422.3
v  TempC                  -119.49          603.96          69.431          75.869
v  Density                 0.4008          2.3827          1.1329          1.1493
v  TurbVisc            5.3006e-15       0.0022898      0.00018946      0.00027393
v  CourantNb                    0          45.224         0.80156         0.58429
v  FourierNb            0.0025119          4.6712         0.17826         0.23041
v  total_pressure           97041      1.0138e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41715          2.3827          1.0707           1.119


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014336          45.497         0.97982          0.8147


 TIME FOR THE TIME STEP              357:        0.64255E+02

===============================================================


 INSTANT    0.337300000E-01   TIME STEP NUMBER             358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.221546323E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870990E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54124E+02 0.38917E+02
   Friction velocity        uet   :  0.13111E-02 0.67274E+01
   Friction velocity        uk    :  0.98208E-02 0.37783E+01
   Dimensionless distance   yplus :  0.11172E+00 0.90348E+02
   Friction thermal sca.    tstar : -0.36164E+03 0.64586E+02
   Rough dim-less th. sca.  tplus :  0.83357E-01 0.14681E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125503
   Nb of faces within the viscous sub-layer     :      10606
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1346 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21558E+00      40   0.41840E-01   0.41769E+02 0.12408E+03 
c  Velocity[X]                                      0.32569E+02 
c  Velocity[Y]                                      0.16185E+01 
c  Velocity[Z]                                      0.75821E+01 
c  Pressure     0.15802E-03     102   0.34550E-02   0.98995E-01 0.14216E+03 
c  k            0.91451E-02      30   0.61673E-03   0.36678E+01 0.63259E+03 
c  omega        0.16520E+04      40   0.31293E-04   0.11784E+11 0.21065E+04 
c  TempC        0.41419E+04      73   0.18410E-01   0.12176E+06 0.18762E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.099          98.287          4.1729          4.3568
v  Velocity[Y]            -16.346          7.3219       -0.001304      0.00056876
v  Velocity[Z]            -27.273          25.886         -0.4933        -0.22175
v  ǁVelocityǁ           0.0029872          101.24          4.6791          4.5467
v  Pressure                 -4338          51.071          6.2136          14.985
v  k                   4.8806e-09          49.083         0.13415          0.1167
v  omega                    1e-24      4.2975e+06          5152.2          1422.5
v  TempC                  -133.65          636.63          69.648          76.095
v  Density                0.40266          2.2984          1.1324          1.1489
v  TurbVisc            1.7037e-14       0.0022897      0.00019004      0.00027475
v  CourantNb                    0          48.575         0.80218         0.58469
v  FourierNb            0.0025121          4.6712          0.1788          0.2311
v  total_pressure           96987      1.0138e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41546          2.2984          1.0702          1.1186


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.015462          48.854         0.98098         0.81579


 TIME FOR THE TIME STEP              358:        0.63261E+02

===============================================================


 INSTANT    0.338300000E-01   TIME STEP NUMBER             359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.289272660E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155865739E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54748E+02 0.40918E+02
   Friction velocity        uet   :  0.13810E-02 0.69114E+01
   Friction velocity        uk    :  0.10651E-01 0.38368E+01
   Dimensionless distance   yplus :  0.13495E+00 0.89568E+02
   Friction thermal sca.    tstar : -0.39614E+03 0.76847E+02
   Rough dim-less th. sca.  tplus :  0.10069E+00 0.14661E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125347
   Nb of faces within the viscous sub-layer     :      10627
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1349 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21564E+00      40   0.42356E-01   0.40876E+02 0.12264E+03 
c  Velocity[X]                                      0.31540E+02 
c  Velocity[Y]                                      0.16433E+01 
c  Velocity[Z]                                      0.76932E+01 
c  Pressure     0.15645E-03     111   0.32108E-02   0.96121E-01 0.15421E+03 
c  k            0.92156E-02      30   0.61240E-03   0.36683E+01 0.63117E+03 
c  omega        0.21053E+17       2   0.83563E-16   0.36087E+10 0.11833E+04 
c  TempC        0.41474E+04      77   0.18382E-01   0.12186E+06 0.18741E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.518          98.963          4.1745          4.3593
v  Velocity[Y]            -17.012          8.2441      -0.0012896      0.00056589
v  Velocity[Z]            -27.321          25.948        -0.49552         -0.2225
v  ǁVelocityǁ           0.0033917          102.06          4.6825          4.5497
v  Pressure               -4402.2          48.417          5.7888           14.57
v  k                   1.8108e-09          51.051          0.1346         0.11703
v  omega                    1e-24      2.1711e+06            5154          1422.8
v  TempC                  -106.43          601.23          69.864          76.321
v  Density                0.38821          2.5318           1.132          1.1485
v  TurbVisc            2.0413e-14       0.0022898      0.00019063      0.00027556
v  CourantNb                    0          49.274          0.8028         0.58509
v  FourierNb            0.0025123          4.6712         0.17934          0.2318
v  total_pressure           96923      1.0137e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41015          2.5318          1.0698          1.1182


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014853          49.568         0.98214         0.81689


 TIME FOR THE TIME STEP              359:        0.62103E+02

===============================================================


 INSTANT    0.339300000E-01   TIME STEP NUMBER             360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.216027960E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155869438E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53088E+02 0.42578E+02
   Friction velocity        uet   :  0.83489E-03 0.68889E+01
   Friction velocity        uk    :  0.10671E-01 0.39130E+01
   Dimensionless distance   yplus :  0.12437E+00 0.91911E+02
   Friction thermal sca.    tstar : -0.27142E+03 0.92584E+02
   Rough dim-less th. sca.  tplus :  0.92791E-01 0.14722E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125223
   Nb of faces within the viscous sub-layer     :      10686
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1351 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21567E+00      41   0.42691E-01   0.41966E+02 0.12416E+03 
c  Velocity[X]                                      0.32303E+02 
c  Velocity[Y]                                      0.16153E+01 
c  Velocity[Z]                                      0.80474E+01 
c  Pressure     0.15909E-03     104   0.32782E-02   0.96120E-01 0.10808E+03 
c  k            0.92972E-02      30   0.60598E-03   0.36603E+01 0.62892E+03 
c  omega        0.21843E+03      48   0.11316E-03   0.14165E+10 0.74337E+03 
c  TempC        0.41532E+04      76   0.18116E-01   0.12285E+06 0.18788E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.778          98.676           4.176          4.3618
v  Velocity[Y]            -17.644          8.0811      -0.0013131      0.00055203
v  Velocity[Z]            -26.361          26.154        -0.49775        -0.22323
v  ǁVelocityǁ           0.0047483          102.04          4.6857          4.5527
v  Pressure               -4472.6          45.818          5.5128          14.312
v  k                   2.7513e-09          53.705         0.13507         0.11735
v  omega                    1e-24      1.1074e+06          5158.2          1423.3
v  TempC                  -124.24           609.1           70.08          76.547
v  Density                0.40392          2.1184          1.1316          1.1481
v  TurbVisc            7.1368e-15       0.0022897      0.00019109      0.00027622
v  CourantNb                    0          46.898         0.80338         0.58548
v  FourierNb            0.0025125          4.6712         0.17975         0.23233
v  total_pressure           96852      1.0137e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41488          2.1184          1.0694          1.1178


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016562          47.187         0.98313          0.8178


 TIME FOR THE TIME STEP              360:        0.64240E+02

===============================================================


 INSTANT    0.340300000E-01   TIME STEP NUMBER             361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.138080615E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155864205E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53389E+02 0.44657E+02
   Friction velocity        uet   :  0.14075E-02 0.67298E+01
   Friction velocity        uk    :  0.12904E-01 0.40135E+01
   Dimensionless distance   yplus :  0.15194E+00 0.93388E+02
   Friction thermal sca.    tstar : -0.28956E+03 0.91132E+02
   Rough dim-less th. sca.  tplus :  0.11336E+00 0.14760E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125085
   Nb of faces within the viscous sub-layer     :      10739
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1352 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21573E+00      41   0.43975E-01   0.41433E+02 0.12326E+03 
c  Velocity[X]                                      0.31926E+02 
c  Velocity[Y]                                      0.16406E+01 
c  Velocity[Z]                                      0.78670E+01 
c  Pressure     0.16057E-03     115   0.31594E-02   0.95083E-01 0.11779E+03 
c  k            0.93794E-02      30   0.60082E-03   0.36396E+01 0.62569E+03 
c  omega        0.20210E+05      32   0.12950E-05   0.23119E+10 0.94650E+03 
c  TempC        0.41589E+04      77   0.18369E-01   0.12197E+06 0.18692E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -11.82          100.61          4.1776          4.3643
v  Velocity[Y]            -16.862          8.1798      -0.0013346      0.00054211
v  Velocity[Z]            -27.134          26.024        -0.49998        -0.22397
v  ǁVelocityǁ           0.0041611          103.66           4.689          4.5557
v  Pressure               -4531.7          47.871          5.2088          14.045
v  k                   4.7181e-09          56.121         0.13552         0.11768
v  omega                    1e-24      1.4991e+06          5162.3          1423.8
v  TempC                  -128.36          602.85          70.295          76.774
v  Density                0.40032          2.3717          1.1311          1.1477
v  TurbVisc            2.2739e-14       0.0022897      0.00019167      0.00027703
v  CourantNb                    0           50.28         0.80398         0.58587
v  FourierNb            0.0025126          4.6712         0.18028         0.23302
v  total_pressure           96793      1.0137e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41604          2.3717          1.0689          1.1173


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018844          50.576         0.98427         0.81889


 TIME FOR THE TIME STEP              361:        0.64165E+02

===============================================================


 INSTANT    0.341300000E-01   TIME STEP NUMBER             362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.285732298E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155863814E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52155E+02 0.46138E+02
   Friction velocity        uet   :  0.96116E-03 0.69624E+01
   Friction velocity        uk    :  0.11576E-01 0.41028E+01
   Dimensionless distance   yplus :  0.16366E+00 0.94320E+02
   Friction thermal sca.    tstar : -0.33261E+03 0.82053E+02
   Rough dim-less th. sca.  tplus :  0.12211E+00 0.14784E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     125007
   Nb of faces within the viscous sub-layer     :      10785
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1355 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21579E+00      40   0.44736E-01   0.41186E+02 0.12278E+03 
c  Velocity[X]                                      0.31820E+02 
c  Velocity[Y]                                      0.16200E+01 
c  Velocity[Z]                                      0.77463E+01 
c  Pressure     0.16050E-03     101   0.30835E-02   0.93319E-01 0.81701E+02 
c  k            0.94630E-02      30   0.59443E-03   0.36350E+01 0.62387E+03 
c  omega        0.20496E+03      49   0.10600E-03   0.10059E+10 0.62487E+03 
c  TempC        0.41646E+04      79   0.18338E-01   0.12158E+06 0.18634E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.095          102.62          4.1791          4.3668
v  Velocity[Y]            -17.301          8.4091      -0.0013298      0.00053806
v  Velocity[Z]            -27.317          26.142        -0.50217         -0.2247
v  ǁVelocityǁ           0.0026441          105.87          4.6922          4.5587
v  Pressure               -4596.1          81.352            5.06            13.9
v  k                   3.8411e-09          57.639         0.13596           0.118
v  omega                    1e-24      7.7663e+05          5166.7          1424.3
v  TempC                  -121.92          590.24          70.509          77.001
v  Density                0.40318          2.4393          1.1307          1.1473
v  TurbVisc            2.4248e-14       0.0022898      0.00019227      0.00027785
v  CourantNb                    0          51.374         0.80455         0.58626
v  FourierNb            0.0025128          4.6712         0.18083         0.23372
v  total_pressure           96729      1.0141e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41532          2.4393          1.0685          1.1169


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017801          51.692         0.98539         0.81998


 TIME FOR THE TIME STEP              362:        0.63384E+02

===============================================================


 INSTANT    0.342300000E-01   TIME STEP NUMBER             363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.247682237E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155861860E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52721E+02 0.48085E+02
   Friction velocity        uet   :  0.21510E-02 0.69604E+01
   Friction velocity        uk    :  0.10505E-01 0.41579E+01
   Dimensionless distance   yplus :  0.12733E+00 0.94969E+02
   Friction thermal sca.    tstar : -0.45067E+03 0.71424E+02
   Rough dim-less th. sca.  tplus :  0.95002E-01 0.14800E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     124832
   Nb of faces within the viscous sub-layer     :      10843
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1358 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21585E+00      41   0.44899E-01   0.41288E+02 0.12283E+03 
c  Velocity[X]                                      0.31750E+02 
c  Velocity[Y]                                      0.16595E+01 
c  Velocity[Z]                                      0.78777E+01 
c  Pressure     0.16109E-03     106   0.30821E-02   0.91829E-01 0.72337E+02 
c  k            0.95683E-02      30   0.58593E-03   0.36466E+01 0.62328E+03 
c  omega        0.19116E+03      49   0.18374E-03   0.11605E+10 0.66999E+03 
c  TempC        0.41704E+04      80   0.18882E-01   0.12160E+06 0.18607E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.124          103.45          4.1806          4.3694
v  Velocity[Y]            -19.736          8.9905      -0.0013296      0.00053411
v  Velocity[Z]            -28.624          26.433        -0.50431        -0.22541
v  ǁVelocityǁ           0.0046505          107.18          4.6953          4.5616
v  Pressure               -4651.8          133.72          5.0476          13.896
v  k                   2.8931e-09           60.46          0.1364         0.11833
v  omega                    1e-24      5.8836e+05          5173.1          1424.9
v  TempC                  -111.97          606.53          70.723          77.228
v  Density                0.40906          2.3354          1.1302          1.1469
v  TurbVisc            1.9738e-14       0.0022898      0.00019286      0.00027867
v  CourantNb                    0          48.051         0.80514         0.58664
v  FourierNb             0.002513          4.6712         0.18137         0.23442
v  total_pressure           96673      1.0146e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41769          2.3354           1.068          1.1165


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017255          48.354         0.98651         0.82106


 TIME FOR THE TIME STEP              363:        0.64149E+02

===============================================================


 INSTANT    0.343300000E-01   TIME STEP NUMBER             364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.343433460E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155858550E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51920E+02 0.49792E+02
   Friction velocity        uet   :  0.19032E-02 0.70278E+01
   Friction velocity        uk    :  0.46194E-02 0.42586E+01
   Dimensionless distance   yplus :  0.55458E-01 0.98201E+02
   Friction thermal sca.    tstar : -0.59710E+03 0.74263E+02
   Rough dim-less th. sca.  tplus :  0.41378E-01 0.14880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     124669
   Nb of faces within the viscous sub-layer     :      10888
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1359 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21586E+00      42   0.44450E-01   0.42275E+02 0.12418E+03 
c  Velocity[X]                                      0.32440E+02 
c  Velocity[Y]                                      0.17130E+01 
c  Velocity[Z]                                      0.81223E+01 
c  Pressure     0.16234E-03      96   0.30321E-02   0.90862E-01 0.69390E+02 
c  k            0.96743E-02      30   0.58023E-03   0.36420E+01 0.62130E+03 
c  omega        0.19097E+03      50   0.28013E-03   0.92039E+10 0.18548E+04 
c  TempC        0.41762E+04      80   0.18424E-01   0.12184E+06 0.18598E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -12.32          102.83          4.1821          4.3719
v  Velocity[Y]            -16.235          8.5587      -0.0012926      0.00053906
v  Velocity[Z]            -29.247          26.302        -0.50645        -0.22611
v  ǁVelocityǁ           0.0032832          106.23          4.6985          4.5646
v  Pressure               -4719.9          169.12          5.0796          13.948
v  k                   2.1385e-09          64.857         0.13685         0.11865
v  omega                    1e-24      3.9553e+06          5181.5          1425.9
v  TempC                   -126.7          602.29          70.935          77.454
v  Density                0.40149          2.1912          1.1298          1.1464
v  TurbVisc            1.4866e-14       0.0022897      0.00019346      0.00027949
v  CourantNb                    0          51.676          0.8057         0.58703
v  FourierNb            0.0025132          4.6712         0.18192         0.23512
v  total_pressure           96605      1.0149e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41251          2.1912          1.0676          1.1161


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014478          52.004         0.98762         0.82215


 TIME FOR THE TIME STEP              364:        0.63660E+02

===============================================================


 INSTANT    0.344300000E-01   TIME STEP NUMBER             365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.297246207E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155859107E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51853E+02 0.51459E+02
   Friction velocity        uet   :  0.18250E-02 0.68936E+01
   Friction velocity        uk    :  0.10147E-01 0.44107E+01
   Dimensionless distance   yplus :  0.11892E+00 0.97857E+02
   Friction thermal sca.    tstar : -0.46156E+03 0.78625E+02
   Rough dim-less th. sca.  tplus :  0.88731E-01 0.14871E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     124539
   Nb of faces within the viscous sub-layer     :      10921
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1361 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21592E+00      41   0.45118E-01   0.41791E+02 0.12335E+03 
c  Velocity[X]                                      0.31871E+02 
c  Velocity[Y]                                      0.17608E+01 
c  Velocity[Z]                                      0.81588E+01 
c  Pressure     0.16311E-03     108   0.29563E-02   0.89477E-01 0.81017E+02 
c  k            0.97906E-02      31   0.56858E-03   0.36293E+01 0.61864E+03 
c  omega        0.27102E+03      49   0.16664E-03   0.62666E+10 0.15359E+04 
c  TempC        0.41821E+04      81   0.18666E-01   0.12106E+06 0.18510E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.114          105.93          4.1837          4.3744
v  Velocity[Y]            -17.733          9.1097      -0.0013054      0.00052115
v  Velocity[Z]            -27.579           26.19        -0.50857        -0.22681
v  ǁVelocityǁ           0.0042295          109.41          4.7017          4.5675
v  Pressure               -4792.5          223.43          5.0809          13.991
v  k                   5.7224e-10          67.218         0.13728         0.11898
v  omega                    1e-24      3.2189e+06          5185.3          1426.4
v  TempC                  -103.69          625.52          71.144           77.68
v  Density                0.40343          2.4117          1.1294           1.146
v  TurbVisc            1.0988e-14         0.00229      0.00019407      0.00028032
v  CourantNb                    0          49.138         0.80628         0.58741
v  FourierNb            0.0025134          4.6712         0.18247         0.23583
v  total_pressure           96532      1.0155e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41792          2.4117          1.0671          1.1157


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010595          49.467         0.98874         0.82324


 TIME FOR THE TIME STEP              365:        0.64312E+02

===============================================================


 INSTANT    0.345300000E-01   TIME STEP NUMBER             366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.284570319E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155862203E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50776E+02 0.54446E+02
   Friction velocity        uet   :  0.13733E-02 0.71012E+01
   Friction velocity        uk    :  0.82901E-02 0.44903E+01
   Dimensionless distance   yplus :  0.10622E+00 0.10087E+03
   Friction thermal sca.    tstar : -0.41193E+03 0.69086E+02
   Rough dim-less th. sca.  tplus :  0.79249E-01 0.14943E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     124408
   Nb of faces within the viscous sub-layer     :      10947
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1365 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21602E+00      41   0.46044E-01   0.41742E+02 0.12317E+03 
c  Velocity[X]                                      0.31924E+02 
c  Velocity[Y]                                      0.17081E+01 
c  Velocity[Z]                                      0.81092E+01 
c  Pressure     0.16200E-03     102   0.29808E-02   0.87175E-01 0.78130E+02 
c  k            0.99017E-02      31   0.56365E-03   0.36274E+01 0.61685E+03 
c  omega        0.22959E+03      49   0.13249E-03   0.19913E+10 0.87170E+03 
c  TempC        0.41881E+04      81   0.18433E-01   0.12120E+06 0.18494E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -12.4           107.8          4.1852           4.377
v  Velocity[Y]            -19.778          9.1101      -0.0012795      0.00051955
v  Velocity[Z]            -28.382          26.565        -0.51065        -0.22748
v  ǁVelocityǁ            0.003035          111.72          4.7047          4.5705
v  Pressure                 -4853          262.26          5.1834          14.095
v  k                   9.3574e-10          69.932         0.13772          0.1193
v  omega                    1e-24      1.6348e+06          5186.7          1426.7
v  TempC                  -117.45          622.83          71.352          77.907
v  Density                0.39301          2.0842           1.129          1.1456
v  TurbVisc            5.1085e-15       0.0022902      0.00019468      0.00028114
v  CourantNb                    0           52.56         0.80683         0.58779
v  FourierNb            0.0025137          4.6712         0.18302         0.23654
v  total_pressure           96472      1.0159e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41253          2.0334          1.0667          1.1153


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012179          52.901         0.98985         0.82433


 TIME FOR THE TIME STEP              366:        0.63851E+02

===============================================================


 INSTANT    0.346300000E-01   TIME STEP NUMBER             367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.344313464E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155854537E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51086E+02 0.56748E+02
   Friction velocity        uet   :  0.15076E-02 0.72415E+01
   Friction velocity        uk    :  0.90238E-02 0.45801E+01
   Dimensionless distance   yplus :  0.97763E-01 0.10079E+03
   Friction thermal sca.    tstar : -0.39331E+03 0.60907E+02
   Rough dim-less th. sca.  tplus :  0.72942E-01 0.14942E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     124259
   Nb of faces within the viscous sub-layer     :      10956
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1366 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21604E+00      42   0.45861E-01   0.42073E+02 0.12355E+03 
c  Velocity[X]                                      0.32188E+02 
c  Velocity[Y]                                      0.17653E+01 
c  Velocity[Z]                                      0.81203E+01 
c  Pressure     0.16744E-03     106   0.29149E-02   0.88089E-01 0.88404E+02 
c  k            0.10024E-01      31   0.56102E-03   0.36415E+01 0.61619E+03 
c  omega        0.25604E+22       2   0.72034E-21   0.24075E+10 0.95708E+03 
c  TempC        0.41942E+04      81   0.18696E-01   0.12134E+06 0.18477E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.175          106.59          4.1868          4.3795
v  Velocity[Y]            -18.751          9.5499      -0.0012646      0.00052076
v  Velocity[Z]             -29.08          26.791        -0.51262        -0.22813
v  ǁVelocityǁ           0.0052228          110.33          4.7078          4.5734
v  Pressure               -4929.4          329.89          5.2749          14.228
v  k                   3.9278e-10          76.085         0.13819         0.11963
v  omega                    1e-24      1.8876e+06          5189.5          1427.1
v  TempC                  -129.02           606.5          71.557          78.133
v  Density                0.39419          2.2684          1.1285          1.1452
v  TurbVisc            4.8071e-15         0.00229      0.00019528      0.00028195
v  CourantNb                    0          53.337         0.80739         0.58817
v  FourierNb            0.0025139          4.6712         0.18356         0.23723
v  total_pressure           96396      1.0165e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.39419          2.2684          1.0662          1.1148


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017127          53.702         0.99095          0.8254


 TIME FOR THE TIME STEP              367:        0.62394E+02

===============================================================


 INSTANT    0.347300000E-01   TIME STEP NUMBER             368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.390670082E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155858853E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50112E+02 0.58029E+02
   Friction velocity        uet   :  0.53547E-03 0.70888E+01
   Friction velocity        uk    :  0.99428E-02 0.47774E+01
   Dimensionless distance   yplus :  0.11747E+00 0.10388E+03
   Friction thermal sca.    tstar : -0.35376E+03 0.58312E+02
   Rough dim-less th. sca.  tplus :  0.87647E-01 0.15013E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     124184
   Nb of faces within the viscous sub-layer     :      10985
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1370 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21609E+00      42   0.45699E-01   0.42051E+02 0.12341E+03 
c  Velocity[X]                                      0.32061E+02 
c  Velocity[Y]                                      0.17550E+01 
c  Velocity[Z]                                      0.82350E+01 
c  Pressure     0.16493E-03     103   0.28481E-02   0.85069E-01 0.10354E+03 
c  k            0.10209E-01      31   0.54259E-03   0.36261E+01 0.61294E+03 
c  omega        0.19675E+03      52   0.11681E-03   0.10508E+10 0.63275E+03 
c  TempC        0.42004E+04      82   0.18300E-01   0.12161E+06 0.18470E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.456          111.29          4.1883          4.3821
v  Velocity[Y]            -20.891          9.9354      -0.0012789      0.00051074
v  Velocity[Z]            -29.799          26.568        -0.51455        -0.22876
v  ǁVelocityǁ           0.0050847          115.47          4.7109          4.5764
v  Pressure               -5013.2          361.35          5.4854          14.462
v  k                   7.8314e-11          78.866         0.13869         0.11997
v  omega                    1e-24      9.6436e+05          5192.5          1427.6
v  TempC                  -116.08          599.05          71.762           78.36
v  Density                 0.4015          2.4505          1.1281          1.1448
v  TurbVisc            2.0176e-15       0.0022901      0.00019577      0.00028261
v  CourantNb                    0          50.825         0.80792         0.58854
v  FourierNb             0.002514          4.6712         0.18399         0.23777
v  total_pressure           96312      1.0169e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.40514          2.4505          1.0658          1.1144


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016511          51.187         0.99191         0.82631


 TIME FOR THE TIME STEP              368:        0.64137E+02

===============================================================


 INSTANT    0.348300000E-01   TIME STEP NUMBER             369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.336926974E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155855057E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49840E+02 0.62048E+02
   Friction velocity        uet   :  0.77594E-03 0.74228E+01
   Friction velocity        uk    :  0.10706E-01 0.48640E+01
   Dimensionless distance   yplus :  0.10340E+00 0.10722E+03
   Friction thermal sca.    tstar : -0.45280E+03 0.59669E+02
   Rough dim-less th. sca.  tplus :  0.77145E-01 0.15089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123975
   Nb of faces within the viscous sub-layer     :      11011
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1371 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21616E+00      42   0.46798E-01   0.42308E+02 0.12368E+03 
c  Velocity[X]                                      0.32437E+02 
c  Velocity[Y]                                      0.16987E+01 
c  Velocity[Z]                                      0.81719E+01 
c  Pressure     0.16435E-03     106   0.27993E-02   0.83002E-01 0.85024E+02 
c  k            0.10362E-01      32   0.56233E-03   0.36273E+01 0.61091E+03 
c  omega        0.20421E+03      52   0.32887E-03   0.15551E+11 0.23651E+04 
c  TempC        0.42066E+04      83   0.18257E-01   0.12161E+06 0.18443E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.306          108.92          4.1898          4.3847
v  Velocity[Y]            -24.044          10.539      -0.0012654      0.00050695
v  Velocity[Z]             -31.87          26.911        -0.51645        -0.22937
v  ǁVelocityǁ           0.0042148          113.93           4.714          4.5793
v  Pressure               -5080.5          422.89          5.5404          14.564
v  k                   4.2668e-10          87.274         0.13921          0.1203
v  omega                    1e-24      4.4544e+06            5202          1428.6
v  TempC                  -113.67          601.64          71.968          78.586
v  Density                0.40493          2.2485          1.1277          1.1444
v  TurbVisc            4.0225e-16       0.0022897      0.00019638      0.00028343
v  CourantNb                    0          54.599         0.80847         0.58891
v  FourierNb            0.0025143          4.6712         0.18454         0.23848
v  total_pressure           96245      1.0175e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41131          2.2485          1.0653           1.114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.010556          54.973         0.99301         0.82739


 TIME FOR THE TIME STEP              369:        0.64327E+02

===============================================================


 INSTANT    0.349300000E-01   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.364810072E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155859246E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48881E+02 0.64290E+02
   Friction velocity        uet   :  0.11833E-02 0.72734E+01
   Friction velocity        uk    :  0.64598E-02 0.51168E+01
   Dimensionless distance   yplus :  0.68092E-01 0.10900E+03
   Friction thermal sca.    tstar : -0.41890E+03 0.61961E+02
   Rough dim-less th. sca.  tplus :  0.50804E-01 0.15128E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123916
   Nb of faces within the viscous sub-layer     :      11022
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1374 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21623E+00      43   0.49524E-01   0.43843E+02 0.12578E+03 
c  Velocity[X]                                      0.33833E+02 
c  Velocity[Y]                                      0.17289E+01 
c  Velocity[Z]                                      0.82814E+01 
c  Pressure     0.16606E-03      93   0.27749E-02   0.82107E-01 0.67992E+02 
c  k            0.10570E-01      32   0.53291E-03   0.35782E+01 0.60480E+03 
c  omega        0.37104E+03      49   0.13851E-03   0.43382E+10 0.12726E+04 
c  TempC        0.42128E+04      83   0.18259E-01   0.12059E+06 0.18338E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.364          113.29          4.1915          4.3873
v  Velocity[Y]            -21.007          10.405      -0.0012223       0.0005103
v  Velocity[Z]            -32.441          26.892        -0.51832        -0.22995
v  ǁVelocityǁ           0.0035618          117.87          4.7172          4.5823
v  Pressure               -5164.5          465.73          5.5437          14.595
v  k                   2.9495e-10          91.681         0.13975         0.12064
v  omega                    1e-24      2.2502e+06          5203.4          1428.9
v  TempC                  -127.15           586.5          72.176          78.814
v  Density                0.40374          2.2146          1.1272           1.144
v  TurbVisc            2.1914e-15       0.0022896      0.00019698      0.00028426
v  CourantNb                    0          55.447         0.80903         0.58929
v  FourierNb            0.0025145          4.6712         0.18509         0.23918
v  total_pressure           96161      1.0179e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41708          2.2146          1.0648          1.1136


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.013211           55.85         0.99412         0.82847


 TIME FOR THE TIME STEP              370:        0.63569E+02

===============================================================


 INSTANT    0.350300000E-01   TIME STEP NUMBER             371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.362292711E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155860711E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49157E+02 0.67625E+02
   Friction velocity        uet   :  0.72922E-03 0.74677E+01
   Friction velocity        uk    :  0.10166E-01 0.52444E+01
   Dimensionless distance   yplus :  0.10735E+00 0.10910E+03
   Friction thermal sca.    tstar : -0.44551E+03 0.65623E+02
   Rough dim-less th. sca.  tplus :  0.80097E-01 0.15130E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123819
   Nb of faces within the viscous sub-layer     :      11055
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1376 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21627E+00      44   0.48955E-01   0.43083E+02 0.12458E+03 
c  Velocity[X]                                      0.32778E+02 
c  Velocity[Y]                                      0.17612E+01 
c  Velocity[Z]                                      0.85438E+01 
c  Pressure     0.16926E-03     104   0.27283E-02   0.81767E-01 0.73298E+02 
c  k            0.10744E-01      32   0.53650E-03   0.36287E+01 0.60678E+03 
c  omega        0.21139E+03      51   0.20870E-03   0.16947E+10 0.79800E+03 
c  TempC        0.42189E+04      84   0.18506E-01   0.12051E+06 0.18305E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.201           113.1          4.1932          4.3899
v  Velocity[Y]            -23.658          10.932      -0.0011948      0.00050214
v  Velocity[Z]            -30.842          26.661        -0.52008        -0.23051
v  ǁVelocityǁ           0.0038162          118.03          4.7203          4.5852
v  Pressure               -5248.3          539.29          5.4858          14.555
v  k                   2.3562e-10          99.242         0.14032         0.12097
v  omega                    1e-24      1.1475e+06          5206.4          1429.3
v  TempC                  -96.274          596.95          72.384          79.041
v  Density                0.41084           2.419          1.1268          1.1436
v  TurbVisc            1.5147e-15       0.0022895      0.00019759      0.00028508
v  CourantNb                    0          52.958         0.80961         0.58966
v  FourierNb            0.0025147          4.6712         0.18564         0.23989
v  total_pressure           96077      1.0186e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41225           2.419          1.0644          1.1131


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018821          53.361         0.99525         0.82955


 TIME FOR THE TIME STEP              371:        0.64532E+02

===============================================================


 INSTANT    0.351300000E-01   TIME STEP NUMBER             372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.404960032E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155861745E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47558E+02 0.70401E+02
   Friction velocity        uet   :  0.25529E-02 0.74802E+01
   Friction velocity        uk    :  0.11097E-01 0.54564E+01
   Dimensionless distance   yplus :  0.10548E+00 0.11279E+03
   Friction thermal sca.    tstar : -0.49937E+03 0.72232E+02
   Rough dim-less th. sca.  tplus :  0.78699E-01 0.15209E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123728
   Nb of faces within the viscous sub-layer     :      11085
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1377 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21634E+00      43   0.52277E-01   0.43475E+02 0.12503E+03 
c  Velocity[X]                                      0.33010E+02 
c  Velocity[Y]                                      0.17873E+01 
c  Velocity[Z]                                      0.86779E+01 
c  Pressure     0.17082E-03      93   0.27097E-02   0.80703E-01 0.68878E+02 
c  k            0.10981E-01      31   0.52221E-03   0.36054E+01 0.60260E+03 
c  omega        0.22389E+03      51   0.16078E-03   0.10888E+10 0.63928E+03 
c  TempC        0.42249E+04      84   0.18333E-01   0.12085E+06 0.18304E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.383          116.56          4.1948          4.3925
v  Velocity[Y]            -21.985          11.423      -0.0011393       0.0005018
v  Velocity[Z]            -31.353          26.925        -0.52187        -0.23106
v  ǁVelocityǁ           0.0031998          121.23          4.7234          4.5881
v  Pressure                 -5324          585.17          5.4602          14.547
v  k                   1.0673e-10          105.47         0.14088         0.12131
v  omega                    1e-24      5.9506e+05          5210.2          1429.8
v  TempC                  -113.59          610.18          72.595          79.268
v  Density                0.40591          1.9968          1.1264          1.1432
v  TurbVisc            1.2098e-15       0.0022899      0.00019818       0.0002859
v  CourantNb                    0          57.249         0.81017         0.59003
v  FourierNb            0.0025149          4.6712         0.18619         0.24059
v  total_pressure           96001      1.0191e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41394          1.9968          1.0639          1.1127


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021695          57.666         0.99635         0.83062


 TIME FOR THE TIME STEP              372:        0.63800E+02

===============================================================


 INSTANT    0.352300000E-01   TIME STEP NUMBER             373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.404423223E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155862549E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47629E+02 0.73237E+02
   Friction velocity        uet   :  0.29040E-02 0.76341E+01
   Friction velocity        uk    :  0.10924E-01 0.56249E+01
   Dimensionless distance   yplus :  0.11507E+00 0.11291E+03
   Friction thermal sca.    tstar : -0.47497E+03 0.74256E+02
   Rough dim-less th. sca.  tplus :  0.85853E-01 0.15212E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123579
   Nb of faces within the viscous sub-layer     :      11113
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1377 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21637E+00      43   0.49675E-01   0.43652E+02 0.12517E+03 
c  Velocity[X]                                      0.32841E+02 
c  Velocity[Y]                                      0.19000E+01 
c  Velocity[Z]                                      0.89107E+01 
c  Pressure     0.16991E-03      94   0.25409E-02   0.78457E-01 0.83188E+02 
c  k            0.11194E-01      32   0.50041E-03   0.35905E+01 0.59911E+03 
c  omega        0.24549E+03      51   0.16308E-03   0.29454E+10 0.10456E+04 
c  TempC        0.42308E+04      83   0.18294E-01   0.12177E+06 0.18347E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.099           119.6          4.1966          4.3952
v  Velocity[Y]            -21.262          11.237      -0.0011363       0.0004925
v  Velocity[Z]            -32.318          27.039        -0.52351        -0.23158
v  ǁVelocityǁ           0.0030159          124.11          4.7265           4.591
v  Pressure               -5403.1          655.57          5.3251          14.464
v  k                   2.7787e-11          111.07         0.14146         0.12164
v  omega                    1e-24      2.2819e+06          5217.6          1430.4
v  TempC                  -124.81          600.07          72.807          79.494
v  Density                0.39983          2.2134          1.1259          1.1428
v  TurbVisc            5.4794e-16       0.0022903      0.00019878      0.00028672
v  CourantNb                    0          54.226         0.81073          0.5904
v  FourierNb            0.0025151          4.6712         0.18673         0.24129
v  total_pressure           95922      1.0198e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41011          2.2134          1.0634          1.1123


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.020876          54.658         0.99746         0.83169


 TIME FOR THE TIME STEP              373:        0.63850E+02

===============================================================


 INSTANT    0.353300000E-01   TIME STEP NUMBER             374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.456204352E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155866552E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46370E+02 0.76642E+02
   Friction velocity        uet   :  0.14699E-02 0.77877E+01
   Friction velocity        uk    :  0.92079E-02 0.57723E+01
   Dimensionless distance   yplus :  0.96205E-01 0.11671E+03
   Friction thermal sca.    tstar : -0.40163E+03 0.73297E+02
   Rough dim-less th. sca.  tplus :  0.71780E-01 0.15291E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123548
   Nb of faces within the viscous sub-layer     :      11179
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1378 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21646E+00      44   0.54651E-01   0.42876E+02 0.12395E+03 
c  Velocity[X]                                      0.32722E+02 
c  Velocity[Y]                                      0.17704E+01 
c  Velocity[Z]                                      0.83830E+01 
c  Pressure     0.16918E-03     103   0.25088E-02   0.76332E-01 0.10210E+03 
c  k            0.11417E-01      32   0.50843E-03   0.35945E+01 0.59708E+03 
c  omega        0.20469E+03      51   0.15646E-03   0.22090E+10 0.90473E+03 
c  TempC        0.42366E+04      83   0.18394E-01   0.12180E+06 0.18322E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.559          120.12          4.1983          4.3978
v  Velocity[Y]            -25.737          11.728      -0.0011766      0.00047821
v  Velocity[Z]            -32.519          26.938        -0.52513        -0.23207
v  ǁVelocityǁ           0.0028696          125.66          4.7296          4.5939
v  Pressure               -5492.9          706.94          5.0685          14.235
v  k                   1.7274e-10          118.29         0.14204         0.12198
v  omega                    1e-24      1.3195e+06          5223.4            1431
v  TempC                  -117.57          599.12           73.02          79.721
v  Density                0.40446          2.3809          1.1255          1.1423
v  TurbVisc            1.4262e-16       0.0022902      0.00019937      0.00028754
v  CourantNb                    0          59.549         0.81129         0.59077
v  FourierNb            0.0025153          4.6712         0.18727         0.24198
v  total_pressure           95832      1.0203e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          0.4165          2.3809           1.063          1.1119


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017739          60.013         0.99856         0.83275


 TIME FOR THE TIME STEP              374:        0.64439E+02

===============================================================


 INSTANT    0.354300000E-01   TIME STEP NUMBER             375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.406058376E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867205E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46396E+02 0.79175E+02
   Friction velocity        uet   :  0.26039E-02 0.78649E+01
   Friction velocity        uk    :  0.73056E-02 0.59571E+01
   Dimensionless distance   yplus :  0.76385E-01 0.11395E+03
   Friction thermal sca.    tstar : -0.37025E+03 0.72204E+02
   Rough dim-less th. sca.  tplus :  0.56992E-01 0.15234E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123500
   Nb of faces within the viscous sub-layer     :      11203
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1378 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21653E+00      44   0.53933E-01   0.44338E+02 0.12593E+03 
c  Velocity[X]                                      0.33875E+02 
c  Velocity[Y]                                      0.17820E+01 
c  Velocity[Z]                                      0.86813E+01 
c  Pressure     0.17305E-03      93   0.25669E-02   0.76216E-01 0.13928E+03 
c  k            0.11736E-01      32   0.52820E-03   0.36523E+01 0.59907E+03 
c  omega        0.19921E+03      51   0.15896E-03   0.20374E+10 0.86749E+03 
c  TempC        0.42423E+04      81   0.18213E-01   0.12120E+06 0.18250E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.276          123.36          4.2001          4.4004
v  Velocity[Y]            -22.574          12.672      -0.0011711      0.00047776
v  Velocity[Z]            -34.323          27.272        -0.52674        -0.23255
v  ǁVelocityǁ           0.0025869          128.33          4.7327          4.5967
v  Pressure               -5565.3          795.15          4.6624          13.846
v  k                   1.3785e-10          128.37         0.14263         0.12232
v  omega                    1e-24      1.3511e+06          5228.5          1431.5
v  TempC                  -123.09          607.04          73.233          79.948
v  Density                 0.4049            2.27           1.125          1.1419
v  TurbVisc            8.8647e-16       0.0022901      0.00019994      0.00028835
v  CourantNb                    0          56.218         0.81185         0.59113
v  FourierNb            0.0025155          4.6712         0.18779         0.24267
v  total_pressure           95760      1.0212e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41856          2.1992          1.0625          1.1114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.014165          56.669         0.99964          0.8338


 TIME FOR THE TIME STEP              375:        0.63499E+02

===============================================================


 INSTANT    0.355300000E-01   TIME STEP NUMBER             376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.471162475E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155870710E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44920E+02 0.81546E+02
   Friction velocity        uet   :  0.17830E-02 0.79691E+01
   Friction velocity        uk    :  0.10798E-01 0.62056E+01
   Dimensionless distance   yplus :  0.12968E+00 0.12215E+03
   Friction thermal sca.    tstar : -0.47323E+03 0.76639E+02
   Rough dim-less th. sca.  tplus :  0.96757E-01 0.15399E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123415
   Nb of faces within the viscous sub-layer     :      11259
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1381 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21652E+00      44   0.49479E-01   0.44424E+02 0.12594E+03 
c  Velocity[X]                                      0.33908E+02 
c  Velocity[Y]                                      0.18812E+01 
c  Velocity[Z]                                      0.86347E+01 
c  Pressure     0.17405E-03      94   0.23943E-02   0.74934E-01 0.12026E+03 
c  k            0.12141E-01      32   0.55163E-03   0.36721E+01 0.59771E+03 
c  omega        0.21150E+03      52   0.12917E-03   0.10973E+10 0.63637E+03 
c  TempC        0.42481E+04      83   0.18237E-01   0.12202E+06 0.18285E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.511          123.28          4.2018           4.403
v  Velocity[Y]            -27.264          12.397      -0.0011116       0.0004748
v  Velocity[Z]             -35.21          28.148        -0.52825        -0.23298
v  ǁVelocityǁ           0.0023994          129.27          4.7357          4.5995
v  Pressure               -5646.1          844.16          4.3815          13.546
v  k                   6.4874e-10          140.03         0.14322         0.12266
v  omega                    1e-24      8.9247e+05          5232.7            1432
v  TempC                  -128.09          616.58          73.446          80.175
v  Density                0.40126          2.3537          1.1246          1.1415
v  TurbVisc            6.2444e-16       0.0022898      0.00020052      0.00028915
v  CourantNb                    0          60.549         0.81239          0.5915
v  FourierNb            0.0025157          4.6712         0.18832         0.24335
v  total_pressure           95679      1.0217e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41321          2.1191          1.0621           1.111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.012632          61.033          1.0007         0.83485


 TIME FOR THE TIME STEP              376:        0.63709E+02

===============================================================


 INSTANT    0.356300000E-01   TIME STEP NUMBER             377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.544863228E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155867766E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45028E+02 0.83227E+02
   Friction velocity        uet   :  0.16239E-02 0.80016E+01
   Friction velocity        uk    :  0.78430E-02 0.64813E+01
   Dimensionless distance   yplus :  0.10059E+00 0.12109E+03
   Friction thermal sca.    tstar : -0.51822E+03 0.87937E+02
   Rough dim-less th. sca.  tplus :  0.75049E-01 0.15379E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123280
   Nb of faces within the viscous sub-layer     :      11298
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1380 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21666E+00      44   0.55580E-01   0.44447E+02 0.12586E+03 
c  Velocity[X]                                      0.33994E+02 
c  Velocity[Y]                                      0.19028E+01 
c  Velocity[Z]                                      0.85511E+01 
c  Pressure     0.17288E-03     108   0.23707E-02   0.72627E-01 0.17077E+03 
c  k            0.12566E-01      32   0.51301E-03   0.36795E+01 0.59526E+03 
c  omega        0.19839E+03      51   0.12729E-03   0.85631E+09 0.56142E+03 
c  TempC        0.42537E+04      81   0.18237E-01   0.12227E+06 0.18277E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.236          127.63          4.2037          4.4057
v  Velocity[Y]            -25.596          13.281      -0.0011344      0.00045912
v  Velocity[Z]            -33.997          28.958        -0.52965         -0.2334
v  ǁVelocityǁ           0.0024852          133.35          4.7387          4.6023
v  Pressure               -5731.1          938.57          3.8597          13.065
v  k                   9.2835e-10          151.12         0.14381         0.12301
v  omega                    1e-24      8.8801e+05          5236.5          1432.4
v  TempC                  -132.32          642.99          73.658          80.401
v  Density                0.39696          2.4347          1.1242          1.1411
v  TurbVisc             3.328e-15       0.0022897      0.00020109      0.00028995
v  CourantNb                    0          57.922         0.81292         0.59185
v  FourierNb            0.0025159          4.6712         0.18884         0.24403
v  total_pressure           95594      1.0226e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41153          2.2812          1.0616          1.1106


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016182          58.416          1.0018         0.83588


 TIME FOR THE TIME STEP              377:        0.65473E+02

===============================================================


 INSTANT    0.357300000E-01   TIME STEP NUMBER             378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.482586163E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871375E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43797E+02 0.86344E+02
   Friction velocity        uet   :  0.96114E-03 0.81808E+01
   Friction velocity        uk    :  0.91749E-02 0.67332E+01
   Dimensionless distance   yplus :  0.91860E-01 0.12683E+03
   Friction thermal sca.    tstar : -0.56699E+03 0.10789E+03
   Rough dim-less th. sca.  tplus :  0.68538E-01 0.15489E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123198
   Nb of faces within the viscous sub-layer     :      11325
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1381 outlet faces on       1874

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21667E+00      44   0.54880E-01   0.44135E+02 0.12531E+03 
c  Velocity[X]                                      0.33475E+02 
c  Velocity[Y]                                      0.18708E+01 
c  Velocity[Z]                                      0.87894E+01 
c  Pressure     0.17271E-03      92   0.23131E-02   0.70872E-01 0.12746E+03 
c  k            0.13078E-01      32   0.57499E-03   0.37228E+01 0.59547E+03 
c  omega        0.19912E+03      51   0.14851E-03   0.14302E+10 0.72352E+03 
c  TempC        0.42594E+04      80   0.17854E-01   0.12181E+06 0.18217E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.492          127.81          4.2054          4.4083
v  Velocity[Y]            -29.977          13.785       -0.001134      0.00045537
v  Velocity[Z]            -34.609          30.209        -0.53102        -0.23379
v  ǁVelocityǁ            0.002385          134.59          4.7415          4.6051
v  Pressure               -5824.3          992.27          3.5084           12.72
v  k                   6.4535e-10          166.12         0.14439         0.12335
v  omega                    1e-24      1.1275e+06          5240.6          1432.9
v  TempC                  -136.41          601.51           73.87          80.628
v  Density                0.38551          2.5078          1.1237          1.1407
v  TurbVisc            4.5646e-15       0.0022895      0.00020168      0.00029076
v  CourantNb                    0          62.889         0.81342          0.5922
v  FourierNb            0.0025161          4.6712         0.18937         0.24471
v  total_pressure           95501      1.0232e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41758          1.9672          1.0612          1.1102


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017404          63.424          1.0028         0.83691


 TIME FOR THE TIME STEP              378:        0.65466E+02

===============================================================


 INSTANT    0.358300000E-01   TIME STEP NUMBER             379
 ============================================================= 



 Options set or changed by "control_file":
 -----------------------------------------

  max_time_step                             379 (current: 379)

 Finished reading "control_file".



   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         876        -0.155855450E-01
Smooth wall               5      225028        -0.432989691E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      154326         0.000000000E+00
Free outlet               3        1874         0.155871195E-01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43109E+02 0.88210E+02
   Friction velocity        uet   :  0.57472E-03 0.82226E+01
   Friction velocity        uk    :  0.11078E-01 0.70596E+01
   Dimensionless distance   yplus :  0.16696E+00 0.12496E+03
   Friction thermal sca.    tstar : -0.41205E+03 0.19373E+03
   Rough dim-less th. sca.  tplus :  0.12457E+00 0.15453E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :     123096
   Nb of faces within the viscous sub-layer     :      11310
   Total number of wall faces                   :     225028
------------------------------------------------------------


Incoming flow detained for       1381 outlet faces on       1874


 Write final restart files
   checkpoint at iteration        379, Physical time    0.35830E-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


 Time for restart files:    0.60815E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21676E+00      44   0.56540E-01   0.44464E+02 0.12567E+03 
c  Velocity[X]                                      0.33600E+02 
c  Velocity[Y]                                      0.18544E+01 
c  Velocity[Z]                                      0.90089E+01 
c  Pressure     0.17437E-03      94   0.22435E-02   0.69811E-01 0.16943E+03 
c  k            0.13746E-01      32   0.59775E-03   0.38580E+01 0.60243E+03 
c  omega        0.17010E+10       2   0.14052E-08   0.76032E+09 0.52770E+03 
c  TempC        0.42650E+04      79   0.17920E-01   0.12147E+06 0.18165E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     initial min     initial max  clips to min  clips to max
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega
a  TempC


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.123          130.68          4.2073          4.4109
v  Velocity[Y]            -27.349          13.299      -0.0011191      0.00044505
v  Velocity[Z]            -34.564           30.61        -0.53229        -0.23415
v  ǁVelocityǁ           0.0022056          136.97          4.7444          4.6078
v  Pressure               -5898.8          1096.2          2.9879          12.241
v  k                   8.2443e-10          184.03         0.14496         0.12369
v  omega                    1e-24      8.8537e+05          5241.7            1433
v  TempC                  -140.52          609.64          74.079          80.854
v  Density                 0.4038          2.5829          1.1233          1.1403
v  TurbVisc            3.6168e-15       0.0022896      0.00020227      0.00029157
v  CourantNb                    0          59.509         0.81392         0.59255
v  FourierNb            0.0025163          4.6712         0.18989         0.24539
v  total_pressure           95426      1.0242e+05      1.0133e+05      1.0134e+05

  ** Computed fields on boundary_faces
     ---------------------------------

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density         0.41871          2.1461          1.0607          1.1098


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.01616          60.035          1.0038         0.83794


 TIME FOR THE TIME STEP              379:        0.63537E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.10000E-04
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation

Time elapsed defining values using MEI:     70.70525

