command: 
 /home/ffan/Code_Saturne/4.0.0-rc2/code_saturne-4.0.0-rc2/arch/Linux_x86_64/libexec/code_saturne/cs_solver --param fluid_3disks_alone.xml

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

                                  (R)
                      Code_Saturne

                      Version 4.0.0-rc2


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

  revision 4.0.0-rc2
  build Mon 20 Apr 2015 05:53:07 AM EDT
  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:                Mon 20 Apr 2015 10:52:37 AM EDT
  System:              Linux 3.2.0-70-generic
  Machine:             caelinux2013
  Processor:           model name	: Intel(R) Core(TM) i7-4800MQ CPU @ 2.70GHz
  Memory:              16047 MB
  User:                ffan (Fa-Gung Fan)
  Directory:           /home/ffan/Saturne/4-2Ddisks/case1/RESU/20150420-1052
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              7 (Nb variables                )
       NSCAL  =              1 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              1 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )


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


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

       GX     =    0.00000E+00 (Gravity x component         )
       GY     =   -0.98100E+01 (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  =             21 (Turbulence model            )
       IDEUCH =              1 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - Linear production k-epsilon (ITURB = 21)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )
       RELAXV =    0.10000E+01 for k        (Relaxation)
       RELAXV =    0.10000E+01 for epsilon  (Relaxation)

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

 --- Constants

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

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


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.50000E-01 (Minimum time step           )
       DTMAX  =    0.50000E+03 (Maximum time step           )
       DTREF  =    0.50000E+00 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  0.1000E+01
 k                     1  0.1000E+01
 epsilon               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
 epsilon               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-06  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 k                   100      1  0.1000E-04  0.1000E-06  0.0000E+00
 epsilon             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
 epsilon               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                )


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-07      1
 k                 0.1000E-07      1
 epsilon           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 -0.2731E+03  0.1000E+13
-------------------------------------------------------

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

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

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

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

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


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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =            100 (Final time step required    )

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


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


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

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

 --- Post-processed variables


Velocity
Pressure
k
epsilon
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 epsilon                       -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 epsilon                        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 =              0 (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)


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


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: every 25 time steps and at calculation end


 Reading file:        mesh_input
 Finished reading:    mesh_input

 Number of cells:                                      3866

 ----------------------------------------------------------
 Number of cells + halo cells:                         3866


 ----------------------------------------------------------
 Number of interior faces:                             6183

 ----------------------------------------------------------
 Number of boundary faces:                             8116

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

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                  4

      1 : [          3 ;          4 ] =       3866

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

 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

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

 Matrix bandwidth for volume mesh :          3656
 Matrix profile/lines for volume mesh :      984

 Mesh coordinates:               minimum    and maximum
                       X : -3.0000001e-01  3.0000001e-01
                       Y : -1.7000000e+00 -1.1000000e+00
                       Z :  0.0000000e+00  9.9999998e-03
 Mesh
     Number of cells:          3866
     Number of interior faces: 6183
     Number of boundary faces: 8116
     Number of vertices:       5398

 Groups:
    "1"
       cells:                  3866
       boundary faces:          384
    "2"
       boundary faces:         3866
    "3"
       boundary faces:         3866

 --- Information on the volumes
       Minimum control volume      =  1.4004559e-07
       Maximum control volume      =  1.0120791e-06
       Total volume for the domain =  1.8852644e-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: 0 -->   0 %

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

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

 Computing geometric quantities (0.00496 s)
                                                             
       ALMAX  =    0.12379E+00 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  k                 0.6000E-03  0.6000E-03
  epsilon           0.1068E-04  0.1068E-04
  TempC             0.2000E+02  0.2000E+02
 ---------------------------------

                dt  0.5000E+00  0.5000E+00
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.500000000E+00   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1205E+01  0.1205E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.3654E-02  0.3654E-02
 -----------------------------------------

 --- 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           0
Smooth wall               5         384
Rough wall                6           0
Symmetry                  4        7732
Free outlet               3           0
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           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.67956E-02 0.74159E-02
   Dimensionless distance   yplus :  0.90471E+00 0.12143E+01
   Friction thermal sca.    tstar : -0.14814E+02-0.11038E+02
   Rough dim-less th. sca.  tplus :  0.67502E+00 0.90597E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          1
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80862E-05    2394   0.54443E+00   0.14111E-03 0.20000E+01 
c  Velocity[X]                                      0.35981E-04 
c  Velocity[Y]                                      0.10513E-03 
c  Velocity[Z]                                      0.17842E-29 
c  Pressure     0.32824E-04     493   0.16870E+00   0.99810E+00 0.20000E+01 
c  k            0.45275E-07    1561   0.28578E+00   0.32515E-06 0.32775E+01 
c  epsilon      0.80627E-09    1938   0.10494E-07   0.64510E-13 0.34192E-01 
c  TempC        0.18276E+01    2419   0.14991E-01   0.14697E+01 0.82414E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.013567        0.013621      1.7925e-05      3.1054e-06
v  Velocity[Y]          -0.014711        0.028814      0.00063412     -0.00042739
v  Velocity[Z]        -5.6259e-15      4.3214e-15      3.2492e-18      4.1512e-18
v  ǁVelocityǁ          4.4032e-05        0.028837       0.0072524       0.0069488
v  Pressure             -0.058078        0.055799       9.714e-05     -3.9313e-19
v  k                   1.7708e-05      0.00043682      0.00020556      0.00021497
v  epsilon             1.0505e-05      1.0505e-05      1.0505e-05      1.0505e-05
v  TempC                   20.308          21.598           20.83          20.801
v  Density                 1.2049          1.2049          1.2049          1.2049
v  TurbVisc             0.0036538       0.0036538       0.0036538       0.0036538
v  CourantNb                    0               0               0               0
v  FourierNb                 81.7          529.39          171.77          161.79
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.2049          1.2049          1.2049          1.2049


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            81.7          529.39          171.77          161.79


 TIME FOR THE TIME STEP                1:        0.46286E+00

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


 INSTANT    0.100000000E+01   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44755E-03 0.15130E-01
   Friction velocity        uk    :  0.93694E-03 0.14392E-01
   Dimensionless distance   yplus :  0.12419E+00 0.19060E+01
   Friction thermal sca.    tstar : -0.94020E+02-0.59202E+01
   Rough dim-less th. sca.  tplus :  0.92663E-01 0.14221E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          2
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72619E-05     975   0.71909E-01   0.11361E-03 0.13406E+01 
c  Velocity[X]                                      0.53317E-04 
c  Velocity[Y]                                      0.60289E-04 
c  Velocity[Z]                                      0.41325E-30 
c  Pressure     0.11528E-03     470   0.57636E-01   0.99922E+00 0.20000E+01 
c  k            0.21725E-07     770   0.65620E-01   0.34633E-08 0.34582E+00 
c  epsilon      0.97654E-09     663   0.31318E-01   0.70808E-11 0.31860E+00 
c  TempC        0.18827E+01     696   0.26072E-02   0.19445E+01 0.92377E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.033364        0.033403      3.0076e-05      6.5099e-06
v  Velocity[Y]          -0.023614        0.049105     -0.00046373      -0.0015301
v  Velocity[Z]        -6.5817e-15      6.1741e-15      5.3603e-18      2.6185e-18
v  ǁVelocityǁ          3.2055e-05        0.049892        0.009196       0.0087202
v  Pressure             -0.064087        0.064066      9.0901e-05     -7.9468e-18
v  k                   2.2401e-05      0.00042384      0.00020819      0.00021508
v  epsilon             7.7731e-06      1.6246e-05      1.1791e-05      1.1724e-05
v  TempC                   20.442           25.19          21.402          21.323
v  Density                 1.1984          1.2037          1.2015          1.2017
v  TurbVisc            3.2195e-06       0.0019677      0.00058151      0.00062378
v  CourantNb             0.016666          2.5316         0.60115         0.56421
v  FourierNb              0.85001          159.89          27.545          27.638
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1984          1.2037          1.2015          1.2015


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88069          160.19          28.146          28.202


 TIME FOR THE TIME STEP                2:        0.21943E+00

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


 INSTANT    0.150000000E+01   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25475E-01
   Friction velocity        uet   :  0.52705E-03 0.19804E-01
   Friction velocity        uk    :  0.10138E-02 0.18582E-01
   Dimensionless distance   yplus :  0.15593E+00 0.24381E+01
   Friction thermal sca.    tstar : -0.48491E+02-0.28359E+01
   Rough dim-less th. sca.  tplus :  0.11634E+00 0.18191E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        372
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14876E-05     591   0.15018E+00   0.29487E-04 0.68445E+00 
c  Velocity[X]                                      0.88926E-05 
c  Velocity[Y]                                      0.20594E-04 
c  Velocity[Z]                                      0.26400E-29 
c  Pressure     0.21103E-04     362   0.12327E-02   0.20026E+00 0.49055E-01 
c  k            0.26573E-07     668   0.63863E-01   0.10815E-07 0.54682E+00 
c  epsilon      0.18415E-06     530   0.72347E-01   0.20359E-05 0.19967E+01 
c  TempC        0.19333E+01     611   0.29980E-02   0.55119E+00 0.48164E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.025313         0.02532      3.5422e-05      2.3923e-06
v  Velocity[Y]          -0.017818        0.045205      0.00015362     -0.00090759
v  Velocity[Z]          -1.27e-15      1.4356e-15      4.4907e-18      3.7677e-18
v  ǁVelocityǁ          0.00011712        0.046392       0.0095108       0.0090628
v  Pressure              -0.06251        0.062823      8.4259e-05     -1.0249e-18
v  k                   1.3156e-05      0.00061166      0.00023178      0.00023545
v  epsilon             6.8859e-06        0.022592      0.00017427      0.00013462
v  TempC                   20.564          26.721          21.862          21.762
v  Density                  1.184          1.2031          1.1992          1.1995
v  TurbVisc            4.4381e-06       0.0015035      0.00049047      0.00051914
v  CourantNb            0.0083607          2.8672         0.70897         0.66277
v  FourierNb              0.88727          138.36          23.699          23.423
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density           1.184          1.2031          1.1987          1.1985


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90091           138.5          24.408          24.086


 TIME FOR THE TIME STEP                3:        0.16094E+00

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


 INSTANT    0.200000000E+01   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.101908651E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72776E-03 0.20198E-01
   Friction velocity        uk    :  0.95319E-03 0.17492E-01
   Dimensionless distance   yplus :  0.15309E+00 0.22918E+01
   Friction thermal sca.    tstar : -0.37671E+02-0.21228E+01
   Rough dim-less th. sca.  tplus :  0.11422E+00 0.17100E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17686E-05     527   0.10531E+00   0.44976E-04 0.66871E+00 
c  Velocity[X]                                      0.10142E-04 
c  Velocity[Y]                                      0.34833E-04 
c  Velocity[Z]                                      0.48330E-31 
c  Pressure     0.22116E-04     403   0.52593E-02   0.24724E+00 0.18455E+00 
c  k            0.33487E-07     511   0.33396E-01   0.16424E-07 0.57156E+00 
c  epsilon      0.69329E-07     358   0.10290E-01   0.18713E-05 0.25527E+02 
c  TempC        0.19650E+01     451   0.21087E-02   0.44868E+00 0.42702E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.02658        0.026532      4.5889e-05      1.3073e-06
v  Velocity[Y]          -0.021742         0.05101      0.00062342     -0.00061561
v  Velocity[Z]        -9.6172e-16      9.2617e-16      6.0313e-18      5.6858e-18
v  ǁVelocityǁ          5.7046e-05          0.0518        0.011848        0.011403
v  Pressure             -0.057029        0.057866      6.6146e-05      4.3104e-18
v  k                     6.79e-06      0.00076186      0.00025565      0.00026072
v  epsilon             5.8758e-06      0.00069097      5.2061e-05      4.8175e-05
v  TempC                   20.637          27.349           22.25          22.134
v  Density                 1.1779          1.2026          1.1974          1.1978
v  TurbVisc             6.895e-07       0.0011694      0.00030333      0.00032214
v  CourantNb             0.010071          2.6919         0.77632         0.73165
v  FourierNb              0.53565          104.89           14.82          14.741
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1779          1.2026          1.1967          1.1965


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55338          105.84          15.596          15.473


 TIME FOR THE TIME STEP                4:        0.14819E+00

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


 INSTANT    0.250000000E+01   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24746E-01
   Friction velocity        uet   :  0.73989E-03 0.19159E-01
   Friction velocity        uk    :  0.13621E-02 0.19276E-01
   Dimensionless distance   yplus :  0.21795E+00 0.25085E+01
   Friction thermal sca.    tstar : -0.19499E+02-0.16664E+01
   Rough dim-less th. sca.  tplus :  0.16261E+00 0.18717E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        368
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21553E-05     456   0.63772E-01   0.74788E-04 0.64143E+00 
c  Velocity[X]                                      0.15249E-04 
c  Velocity[Y]                                      0.59538E-04 
c  Velocity[Z]                                      0.64622E-32 
c  Pressure     0.21915E-04     406   0.56925E-02   0.28526E+00 0.17040E+00 
c  k            0.37288E-07     456   0.22424E-01   0.10262E-07 0.38250E+00 
c  epsilon      0.99558E-07     308   0.22166E-02   0.42339E-07 0.17198E+01 
c  TempC        0.19917E+01     389   0.20779E-02   0.29681E+00 0.34217E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.032556        0.032463      5.6268e-05      8.8335e-07
v  Velocity[Y]          -0.025666         0.09121       0.0011428     -0.00037102
v  Velocity[Z]          -1.19e-15      1.3393e-15      5.1633e-18      5.0816e-18
v  ǁVelocityǁ          0.00025245        0.092012         0.01557        0.015081
v  Pressure             -0.052232        0.053525      5.0421e-05      3.0117e-18
v  k                   3.3494e-06      0.00089699      0.00029337      0.00029913
v  epsilon             3.8997e-06       0.0050172      7.0627e-05      6.4766e-05
v  TempC                   20.679          27.848          22.581          22.458
v  Density                 1.1755          1.2023          1.1958          1.1963
v  TurbVisc            8.6823e-08       0.0010161      0.00025732      0.00027354
v  CourantNb            0.0039976          3.4343         0.98569         0.93665
v  FourierNb              0.46565          83.036          12.692           12.64
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1755          1.2023          1.1951          1.1949


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49593          84.505          13.678          13.577


 TIME FOR THE TIME STEP                5:        0.13501E+00

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


 INSTANT    0.300000000E+01   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.696486076E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.30715E-01
   Friction velocity        uet   :  0.89489E-03 0.19927E-01
   Friction velocity        uk    :  0.16951E-02 0.25186E-01
   Dimensionless distance   yplus :  0.23161E+00 0.32711E+01
   Friction thermal sca.    tstar : -0.13060E+02-0.98413E+00
   Rough dim-less th. sca.  tplus :  0.17281E+00 0.24406E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        295
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26125E-05     404   0.61813E-01   0.10611E-03 0.57649E+00 
c  Velocity[X]                                      0.24553E-04 
c  Velocity[Y]                                      0.81560E-04 
c  Velocity[Z]                                      0.51563E-32 
c  Pressure     0.21654E-04     407   0.62938E-02   0.30944E+00 0.17525E+00 
c  k            0.42968E-07     410   0.12794E-01   0.11174E-07 0.34674E+00 
c  epsilon      0.30905E-06     255   0.21583E-02   0.20473E-05 0.19546E+01 
c  TempC        0.20147E+01     348   0.23889E-02   0.24294E+00 0.30553E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.050483        0.050488      6.4321e-05      8.4131e-07
v  Velocity[Y]          -0.036317         0.12085       0.0016179     -0.00015295
v  Velocity[Z]        -1.3449e-15      1.8924e-15      3.7546e-18      3.9404e-18
v  ǁVelocityǁ          0.00012134         0.12099        0.020042        0.019574
v  Pressure             -0.047207        0.049513      4.5644e-05     -6.0444e-18
v  k                   1.9083e-06      0.00099342      0.00034129      0.00034723
v  epsilon             2.5807e-06        0.011784      0.00029562      0.00027271
v  TempC                   20.735          28.312          22.873          22.749
v  Density                 1.1735          1.2022          1.1945           1.195
v  TurbVisc            8.8654e-08      0.00091289      0.00022998      0.00024445
v  CourantNb            0.0090774          5.4681          1.3042          1.2454
v  FourierNb              0.44247          69.011          11.446            11.4
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1735          1.2022          1.1937          1.1935


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48925          71.045           12.75          12.645


 TIME FOR THE TIME STEP                6:        0.12389E+00

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


 INSTANT    0.350000000E+01   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.163554287E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32602E-01
   Friction velocity        uet   :  0.11183E-02 0.20806E-01
   Friction velocity        uk    :  0.17125E-02 0.28163E-01
   Dimensionless distance   yplus :  0.22182E+00 0.36552E+01
   Friction thermal sca.    tstar : -0.11243E+02-0.75034E+00
   Rough dim-less th. sca.  tplus :  0.16550E+00 0.27272E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        263
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31174E-05     363   0.65560E-01   0.10431E-03 0.46011E+00 
c  Velocity[X]                                      0.30594E-04 
c  Velocity[Y]                                      0.73721E-04 
c  Velocity[Z]                                      0.10013E-31 
c  Pressure     0.21467E-04     412   0.64854E-02   0.30895E+00 0.15668E+00 
c  k            0.49042E-07     372   0.92784E-02   0.97091E-08 0.29284E+00 
c  epsilon      0.52442E-06     224   0.55379E-03   0.14928E-05 0.32305E+01 
c  TempC        0.20348E+01     320   0.34615E-02   0.23128E+00 0.29465E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.06456        0.064536      7.5271e-05      8.3455e-07
v  Velocity[Y]          -0.049602         0.13382       0.0019988      3.6108e-05
v  Velocity[Z]        -1.6011e-15       2.416e-15      3.3989e-18       3.979e-18
v  ǁVelocityǁ          0.00030314         0.13382        0.024514        0.024094
v  Pressure              -0.04252        0.046201      3.9348e-05      3.0187e-18
v  k                   1.4148e-06       0.0010649      0.00037108      0.00037813
v  epsilon             2.1327e-06       0.0098476      0.00020944      0.00018676
v  TempC                    20.81          28.755          23.133           23.01
v  Density                 1.1717          1.2019          1.1933          1.1938
v  TurbVisc            6.8215e-08      0.00083444      0.00020244      0.00021476
v  CourantNb             0.029135          7.0848          1.6761          1.6105
v  FourierNb              0.42184           62.23          10.228          10.155
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1717          1.2019          1.1925          1.1923


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49287          64.817          11.904          11.765


 TIME FOR THE TIME STEP                7:        0.11805E+00

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


 INSTANT    0.400000000E+01   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.161465656E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32145E-01
   Friction velocity        uet   :  0.95784E-03 0.20807E-01
   Friction velocity        uk    :  0.98724E-03 0.29518E-01
   Dimensionless distance   yplus :  0.12807E+00 0.39972E+01
   Friction thermal sca.    tstar : -0.24227E+02-0.60443E+00
   Rough dim-less th. sca.  tplus :  0.95558E-01 0.29823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        247
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36057E-05     331   0.74647E-01   0.75590E-04 0.34042E+00 
c  Velocity[X]                                      0.27730E-04 
c  Velocity[Y]                                      0.47860E-04 
c  Velocity[Z]                                      0.71674E-32 
c  Pressure     0.20506E-04     412   0.56873E-02   0.27644E+00 0.13992E+00 
c  k            0.53956E-07     340   0.74710E-02   0.69254E-08 0.22749E+00 
c  epsilon      0.65479E-06     203   0.32603E-03   0.28746E-06 0.12613E+01 
c  TempC        0.20529E+01     299   0.48146E-02   0.22336E+00 0.28648E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.079232        0.079118      9.0903e-05      1.4376e-06
v  Velocity[Y]          -0.059538         0.13972       0.0022612       0.0001972
v  Velocity[Z]        -1.7141e-15       2.399e-15      2.9953e-18      4.1729e-18
v  ǁVelocityǁ          0.00033235         0.13981        0.028057        0.027682
v  Pressure             -0.038186        0.043533      1.9611e-05      3.7418e-18
v  k                   1.3236e-06       0.0011196      0.00040591      0.00041357
v  epsilon              2.086e-06       0.0057551      0.00026201      0.00023786
v  TempC                   20.923          29.163          23.373          23.254
v  Density                   1.17          1.2016          1.1922          1.1927
v  TurbVisc            5.2661e-08      0.00076989      0.00018984      0.00020073
v  CourantNb             0.022273          7.9342          2.0402          1.9701
v  FourierNb              0.42217          57.816           9.685          9.5861
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density            1.17          1.2016          1.1915          1.1912


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49307          60.932          11.725          11.556


 TIME FOR THE TIME STEP                8:        0.11202E+00

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


 INSTANT    0.450000000E+01   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.468018791E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32481E-01
   Friction velocity        uet   :  0.10772E-02 0.21121E-01
   Friction velocity        uk    :  0.10678E-02 0.29963E-01
   Dimensionless distance   yplus :  0.13807E+00 0.42152E+01
   Friction thermal sca.    tstar : -0.12983E+02-0.44983E+00
   Rough dim-less th. sca.  tplus :  0.10302E+00 0.31450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        241
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39631E-05     309   0.86073E-01   0.54221E-04 0.26579E+00 
c  Velocity[X]                                      0.25387E-04 
c  Velocity[Y]                                      0.28834E-04 
c  Velocity[Z]                                      0.54800E-32 
c  Pressure     0.17443E-04     405   0.50226E-02   0.21669E+00 0.13674E+00 
c  k            0.58861E-07     309   0.66201E-02   0.61117E-08 0.20015E+00 
c  epsilon      0.76966E-06     185   0.24853E-03   0.31730E-07 0.39497E+00 
c  TempC        0.20690E+01     283   0.58185E-02   0.21370E+00 0.27744E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.091378        0.091134      0.00011247      3.8597e-06
v  Velocity[Y]          -0.067724         0.13786        0.002425      0.00031614
v  Velocity[Z]        -1.6363e-15      1.7774e-15      2.3118e-18      3.8465e-18
v  ǁVelocityǁ           0.0004284         0.14627        0.030554        0.030178
v  Pressure             -0.035819        0.041184     -1.0957e-05      3.1205e-18
v  k                   1.5147e-06         0.00116      0.00043574      0.00044387
v  epsilon             2.3982e-06       0.0053705      0.00029306       0.0002687
v  TempC                   21.046          29.425          23.602          23.485
v  Density                 1.1684          1.2012          1.1913          1.1918
v  TurbVisc             8.497e-08      0.00071537      0.00018109      0.00019104
v  CourantNb              0.02138          9.1136          2.3303          2.2562
v  FourierNb              0.42464          54.215          9.3002          9.1886
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1684          1.2012          1.1905          1.1903


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4944          57.875          11.631          11.445


 TIME FOR THE TIME STEP                9:        0.10813E+00

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


 INSTANT    0.500000000E+01   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.379345029E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32607E-01
   Friction velocity        uet   :  0.35976E-03 0.19730E-01
   Friction velocity        uk    :  0.40216E-03 0.29735E-01
   Dimensionless distance   yplus :  0.51954E-01 0.43712E+01
   Friction thermal sca.    tstar : -0.27120E+02-0.33512E+00
   Rough dim-less th. sca.  tplus :  0.38764E-01 0.32614E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        233
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41682E-05     292   0.98193E-01   0.44973E-04 0.23295E+00 
c  Velocity[X]                                      0.23610E-04 
c  Velocity[Y]                                      0.21363E-04 
c  Velocity[Z]                                      0.52669E-32 
c  Pressure     0.14033E-04     397   0.47146E-02   0.16375E+00 0.14565E+00 
c  k            0.62800E-07     275   0.62135E-02   0.53375E-08 0.17772E+00 
c  epsilon      0.83619E-06     171   0.20079E-03   0.26769E-07 0.33156E+00 
c  TempC        0.20839E+01     269   0.61005E-02   0.19911E+00 0.26528E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.098137        0.097919      0.00013137      2.6821e-06
v  Velocity[Y]          -0.069414         0.13271       0.0025315      0.00039345
v  Velocity[Z]        -1.4924e-15      1.6285e-15      1.0769e-18      2.6645e-18
v  ǁVelocityǁ          8.4598e-05         0.15133        0.032128        0.031685
v  Pressure              -0.03451        0.038913     -4.5602e-05      2.3588e-18
v  k                   1.9326e-06       0.0011874      0.00046191       0.0004699
v  epsilon             3.0239e-06       0.0052893      0.00033316       0.0003071
v  TempC                   21.163          29.563          23.823          23.709
v  Density                 1.1674          1.2007          1.1904          1.1908
v  TurbVisc            1.0069e-07      0.00066739      0.00017375      0.00018292
v  CourantNb             0.025464          10.823          2.5357          2.4568
v  FourierNb              0.42576           51.03          8.9776           8.856
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1674          1.2007          1.1896          1.1894


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5038          55.272          11.513          11.313


 TIME FOR THE TIME STEP               10:        0.10327E+00

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


 INSTANT    0.550000000E+01   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.533035187E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32778E-01
   Friction velocity        uet   :  0.10111E-02 0.19087E-01
   Friction velocity        uk    :  0.17214E-02 0.28992E-01
   Dimensionless distance   yplus :  0.22234E+00 0.44157E+01
   Friction thermal sca.    tstar : -0.70030E+01-0.27191E+00
   Rough dim-less th. sca.  tplus :  0.16589E+00 0.32946E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        225
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42358E-05     278   0.10139E+00   0.43052E-04 0.22548E+00 
c  Velocity[X]                                      0.21767E-04 
c  Velocity[Y]                                      0.21285E-04 
c  Velocity[Z]                                      0.49489E-32 
c  Pressure     0.11715E-04     393   0.46386E-02   0.13234E+00 0.16111E+00 
c  k            0.66139E-07     232   0.55384E-02   0.47912E-08 0.16211E+00 
c  epsilon      0.86608E-06     158   0.44089E-03   0.11913E-06 0.63024E+00 
c  TempC        0.20978E+01     256   0.65178E-02   0.17946E+00 0.24957E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.10035         0.10023      0.00015234      3.0991e-06
v  Velocity[Y]          -0.069849         0.12878       0.0025975      0.00043358
v  Velocity[Z]        -1.3903e-15      1.4819e-15     -1.8583e-19      1.3529e-18
v  ǁVelocityǁ          0.00046928         0.15071        0.033022        0.032468
v  Pressure             -0.032994        0.036592     -7.5812e-05      1.4163e-18
v  k                   2.5264e-06       0.0012027      0.00048263      0.00049013
v  epsilon             3.9748e-06       0.0057387      0.00037709      0.00035343
v  TempC                    21.29          29.637           24.04          23.927
v  Density                 1.1669          1.2002          1.1895          1.1899
v  TurbVisc            1.2994e-07       0.0006232       0.0001661      0.00017449
v  CourantNb             0.046166          12.211          2.6688          2.5821
v  FourierNb              0.42898          48.064          8.6357          8.5056
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1669          1.2002          1.1888          1.1885


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51874          52.877          11.305          11.088


 TIME FOR THE TIME STEP               11:        0.10099E+00

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


 INSTANT    0.600000000E+01   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.268151275E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32986E-01
   Friction velocity        uet   :  0.13205E-03 0.19905E-01
   Friction velocity        uk    :  0.98530E-03 0.28175E-01
   Dimensionless distance   yplus :  0.12763E+00 0.43888E+01
   Friction thermal sca.    tstar : -0.19502E+02-0.25023E+00
   Rough dim-less th. sca.  tplus :  0.95227E-01 0.32745E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        208
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42205E-05     265   0.99811E-01   0.42889E-04 0.22560E+00 
c  Velocity[X]                                      0.19550E-04 
c  Velocity[Y]                                      0.23339E-04 
c  Velocity[Z]                                      0.41750E-32 
c  Pressure     0.11108E-04     394   0.48652E-02   0.12467E+00 0.18249E+00 
c  k            0.68495E-07     245   0.53301E-02   0.50310E-08 0.16303E+00 
c  epsilon      0.86566E-06     146   0.57112E-03   0.22279E-06 0.79711E+00 
c  TempC        0.21112E+01     243   0.65426E-02   0.15874E+00 0.23269E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.10003         0.10028      0.00016747      1.9731e-06
v  Velocity[Y]          -0.065805         0.12198       0.0026349      0.00045131
v  Velocity[Z]        -1.2402e-15      1.1045e-15     -1.5031e-18     -1.1261e-19
v  ǁVelocityǁ          0.00042139         0.14608        0.033591        0.032927
v  Pressure             -0.031071        0.034188     -9.4898e-05      1.3733e-18
v  k                   3.2473e-06       0.0012107      0.00049463      0.00050073
v  epsilon             5.1856e-06       0.0062847      0.00041975       0.0003976
v  TempC                   21.436          29.655          24.248          24.138
v  Density                 1.1666          1.1997          1.1886          1.1891
v  TurbVisc             1.689e-07      0.00058282      0.00015656      0.00016395
v  CourantNb            0.0042806          13.125          2.7539           2.657
v  FourierNb              0.42929          45.161          8.2184          8.0721
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1666          1.1997          1.1879          1.1877


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54018          50.811          10.972          10.729


 TIME FOR THE TIME STEP               12:        0.98669E-01

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


 INSTANT    0.650000000E+01   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.529726464E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.33096E-01
   Friction velocity        uet   :  0.15071E-02 0.20793E-01
   Friction velocity        uk    :  0.21029E-02 0.27575E-01
   Dimensionless distance   yplus :  0.27232E+00 0.43130E+01
   Friction thermal sca.    tstar : -0.87072E+01-0.27222E+00
   Rough dim-less th. sca.  tplus :  0.20318E+00 0.32180E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        199
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41695E-05     250   0.10316E+00   0.41585E-04 0.22402E+00 
c  Velocity[X]                                      0.17102E-04 
c  Velocity[Y]                                      0.24483E-04 
c  Velocity[Z]                                      0.29741E-32 
c  Pressure     0.11413E-04     394   0.50742E-02   0.12893E+00 0.19905E+00 
c  k            0.69276E-07     236   0.50554E-02   0.52675E-08 0.16692E+00 
c  epsilon      0.84206E-06     134   0.43385E-03   0.14572E-06 0.66596E+00 
c  TempC        0.21243E+01     229   0.62581E-02   0.13944E+00 0.21630E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.095355        0.094883      0.00017733      1.1921e-07
v  Velocity[Y]          -0.061419         0.11889       0.0026529      0.00045437
v  Velocity[Z]        -1.0749e-15      9.7092e-16     -2.8424e-18     -1.6966e-18
v  ǁVelocityǁ          0.00045683         0.13901         0.03402        0.033274
v  Pressure             -0.028808        0.031891     -0.00010019      3.4908e-18
v  k                   3.8324e-06       0.0012315      0.00049686      0.00050079
v  epsilon             6.3678e-06       0.0057306      0.00043701      0.00040977
v  TempC                   21.601          29.673          24.448           24.34
v  Density                 1.1665          1.1991          1.1878          1.1882
v  TurbVisc            2.1386e-07      0.00054046      0.00014553      0.00015187
v  CourantNb             0.061572          13.262          2.8141          2.7058
v  FourierNb              0.42888          42.202          7.7276          7.5659
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1665          1.1991          1.1871          1.1869


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56159          48.642          10.542          10.272


 TIME FOR THE TIME STEP               13:        0.98569E-01

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


 INSTANT    0.700000000E+01   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.882932586E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.33227E-01
   Friction velocity        uet   :  0.50183E-03 0.20625E-01
   Friction velocity        uk    :  0.19591E-02 0.28107E-01
   Dimensionless distance   yplus :  0.25373E+00 0.42076E+01
   Friction thermal sca.    tstar : -0.95258E+01-0.30489E+00
   Rough dim-less th. sca.  tplus :  0.18931E+00 0.31393E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        190
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41096E-05     236   0.88744E-01   0.37154E-04 0.21360E+00 
c  Velocity[X]                                      0.14630E-04 
c  Velocity[Y]                                      0.22524E-04 
c  Velocity[Z]                                      0.24694E-32 
c  Pressure     0.10973E-04     391   0.50611E-02   0.12535E+00 0.21586E+00 
c  k            0.69191E-07     222   0.43578E-02   0.38488E-08 0.14414E+00 
c  epsilon      0.81091E-06     122   0.30909E-03   0.80858E-07 0.49400E+00 
c  TempC        0.21369E+01     214   0.54141E-02   0.12287E+00 0.20146E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.090153        0.089854      0.00017825     -3.5391e-06
v  Velocity[Y]          -0.055029         0.12257        0.002653      0.00045699
v  Velocity[Z]        -8.9062e-16      8.6886e-16     -4.2175e-18     -3.3124e-18
v  ǁVelocityǁ          0.00041946         0.12997        0.034338        0.033555
v  Pressure             -0.026354        0.029691     -9.4498e-05      7.5028e-19
v  k                    4.001e-06       0.0012401      0.00049374      0.00049598
v  epsilon             6.2163e-06       0.0068316       0.0004558      0.00042432
v  TempC                   21.781          29.662          24.639          24.533
v  Density                 1.1664          1.1984           1.187          1.1874
v  TurbVisc             1.796e-07      0.00049779       0.0001346      0.00014009
v  CourantNb             0.030768          12.653          2.8713          2.7538
v  FourierNb              0.42778          39.128          7.2288          7.0631
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1664          1.1984          1.1863          1.1862


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57728          46.128            10.1          9.8169


 TIME FOR THE TIME STEP               14:        0.96232E-01

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


 INSTANT    0.750000000E+01   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.347271101E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.33382E-01
   Friction velocity        uet   :  0.15564E-02 0.20357E-01
   Friction velocity        uk    :  0.18745E-02 0.28636E-01
   Dimensionless distance   yplus :  0.24165E+00 0.40742E+01
   Friction thermal sca.    tstar : -0.62320E+01-0.31349E+00
   Rough dim-less th. sca.  tplus :  0.18029E+00 0.30398E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        186
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40548E-05     221   0.91175E-01   0.31425E-04 0.19794E+00 
c  Velocity[X]                                      0.12982E-04 
c  Velocity[Y]                                      0.18443E-04 
c  Velocity[Z]                                      0.19381E-32 
c  Pressure     0.10284E-04     390   0.48810E-02   0.11869E+00 0.22934E+00 
c  k            0.68418E-07     206   0.40670E-02   0.31592E-08 0.13337E+00 
c  epsilon      0.78085E-06     112   0.26126E-03   0.26766E-07 0.29209E+00 
c  TempC        0.21490E+01     200   0.45344E-02   0.11012E+00 0.18931E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.081807         0.08261      0.00017114     -4.8968e-06
v  Velocity[Y]          -0.050055         0.12621       0.0026308      0.00045675
v  Velocity[Z]        -7.4519e-16       8.425e-16     -5.6921e-18     -4.9611e-18
v  ǁVelocityǁ          0.00025046         0.13206        0.034505         0.03373
v  Pressure             -0.023877        0.027585     -8.1091e-05     -4.5807e-19
v  k                   3.7142e-06       0.0012297      0.00048423      0.00048559
v  epsilon             4.9489e-06        0.006197      0.00045983      0.00042786
v  TempC                   21.968          29.694          24.821          24.718
v  Density                 1.1665          1.1977          1.1862          1.1866
v  TurbVisc            1.4432e-07      0.00045531      0.00012392      0.00012871
v  CourantNb             0.065451           11.45          2.9188          2.7963
v  FourierNb              0.42635          35.966          6.7383          6.5734
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1665          1.1977          1.1856          1.1854


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58161          43.211           9.657          9.3698


 TIME FOR THE TIME STEP               15:        0.91992E-01

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


 INSTANT    0.800000000E+01   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.168703486E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.33266E-01
   Friction velocity        uet   :  0.18590E-02 0.20020E-01
   Friction velocity        uk    :  0.24509E-02 0.29028E-01
   Dimensionless distance   yplus :  0.31601E+00 0.39368E+01
   Friction thermal sca.    tstar : -0.55563E+01-0.31569E+00
   Rough dim-less th. sca.  tplus :  0.23578E+00 0.29373E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        177
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39975E-05     208   0.88973E-01   0.26461E-04 0.18277E+00 
c  Velocity[X]                                      0.11993E-04 
c  Velocity[Y]                                      0.14469E-04 
c  Velocity[Z]                                      0.15492E-32 
c  Pressure     0.92435E-05     391   0.45068E-02   0.10782E+00 0.24038E+00 
c  k            0.67388E-07     194   0.39256E-02   0.29687E-08 0.13308E+00 
c  epsilon      0.75885E-06     111   0.49061E-03   0.10706E-06 0.55930E+00 
c  TempC        0.21607E+01     189   0.40937E-02   0.99935E-01 0.17908E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.073715        0.073516      0.00015956     -3.2848e-06
v  Velocity[Y]          -0.049339         0.12896       0.0025915      0.00045986
v  Velocity[Z]        -7.5008e-16      7.8494e-16     -7.2019e-18     -6.5811e-18
v  ǁVelocityǁ           0.0007476         0.13426        0.034551        0.033822
v  Pressure             -0.021402        0.025525     -6.4452e-05       4.664e-18
v  k                   3.1013e-06       0.0012421      0.00047048      0.00047159
v  epsilon              3.794e-06       0.0061646      0.00047612      0.00044664
v  TempC                   22.147          29.716          24.995          24.896
v  Density                 1.1664          1.1969          1.1855          1.1859
v  TurbVisc            1.2246e-07      0.00043202       0.0001139      0.00011803
v  CourantNb             0.050755          10.219          2.9452          2.8217
v  FourierNb              0.42535          32.737          6.2758          6.1128
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1664          1.1969          1.1849          1.1847


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57698          39.884           9.221          8.9346


 TIME FOR THE TIME STEP               16:        0.90197E-01

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


 INSTANT    0.850000000E+01   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.482287656E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.33146E-01
   Friction velocity        uet   :  0.12312E-03 0.20342E-01
   Friction velocity        uk    :  0.21606E-02 0.29256E-01
   Dimensionless distance   yplus :  0.27860E+00 0.37994E+01
   Friction thermal sca.    tstar : -0.65481E+01-0.31992E+00
   Rough dim-less th. sca.  tplus :  0.20786E+00 0.28348E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        176
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39402E-05     188   0.88286E-01   0.23203E-04 0.17221E+00 
c  Velocity[X]                                      0.11434E-04 
c  Velocity[Y]                                      0.11769E-04 
c  Velocity[Z]                                      0.13805E-32 
c  Pressure     0.85624E-05     391   0.41061E-02   0.10087E+00 0.24510E+00 
c  k            0.65126E-07     187   0.38169E-02   0.36486E-08 0.15460E+00 
c  epsilon      0.74049E-06     100   0.32708E-03   0.47596E-07 0.39807E+00 
c  TempC        0.21718E+01     177   0.44612E-02   0.91108E-01 0.16985E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.070944        0.070888      0.00014457     -2.4368e-06
v  Velocity[Y]          -0.047086         0.12989       0.0025407      0.00046464
v  Velocity[Z]        -7.7721e-16      7.2999e-16     -8.1064e-18      -7.462e-18
v  ǁVelocityǁ          0.00015636         0.13458        0.034432         0.03377
v  Pressure             -0.019069        0.023544     -4.9294e-05      1.1969e-18
v  k                    2.487e-06       0.0012547      0.00044878      0.00044954
v  epsilon             2.8656e-06       0.0060924      0.00045979      0.00043082
v  TempC                   22.347          29.732          25.161          25.065
v  Density                 1.1663          1.1962          1.1848          1.1852
v  TurbVisc            1.1525e-07      0.00041061      0.00010307      0.00010643
v  CourantNb              0.07755           10.27          2.9482          2.8276
v  FourierNb              0.42423          29.581          5.7822          5.6144
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1663          1.1962          1.1842          1.1841


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56405          36.306          8.7305          8.4421


 TIME FOR THE TIME STEP               17:        0.86270E-01

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


 INSTANT    0.900000000E+01   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.810885154E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.33080E-01
   Friction velocity        uet   :  0.62561E-03 0.20614E-01
   Friction velocity        uk    :  0.18675E-02 0.29277E-01
   Dimensionless distance   yplus :  0.29637E+00 0.37949E+01
   Friction thermal sca.    tstar : -0.60113E+01-0.31369E+00
   Rough dim-less th. sca.  tplus :  0.22113E+00 0.28314E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        170
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38877E-05     181   0.82949E-01   0.22117E-04 0.16926E+00 
c  Velocity[X]                                      0.11193E-04 
c  Velocity[Y]                                      0.10925E-04 
c  Velocity[Z]                                      0.12096E-32 
c  Pressure     0.79662E-05     391   0.38000E-02   0.94657E-01 0.25008E+00 
c  k            0.62526E-07     181   0.35981E-02   0.33814E-08 0.15642E+00 
c  epsilon      0.72610E-06      99   0.27843E-03   0.28901E-07 0.31283E+00 
c  TempC        0.21825E+01     169   0.38299E-02   0.82137E-01 0.16026E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.07343        0.073549      0.00013228     -1.3631e-06
v  Velocity[Y]          -0.046716         0.12929       0.0024917      0.00047677
v  Velocity[Z]        -8.2605e-16       6.414e-16     -8.7427e-18     -8.0749e-18
v  ǁVelocityǁ           0.0007986         0.13238        0.034144        0.033555
v  Pressure             -0.016959        0.021609     -3.8198e-05      2.5703e-18
v  k                   1.8864e-06       0.0012652      0.00042572      0.00042666
v  epsilon             2.1602e-06       0.0060024      0.00045232      0.00042582
v  TempC                   22.563          29.755          25.319          25.226
v  Density                 1.1662          1.1954          1.1841          1.1845
v  TurbVisc            8.9771e-08      0.00038985      9.4014e-05      9.6846e-05
v  CourantNb             0.050637          10.116          2.9257          2.8115
v  FourierNb              0.42359          26.578          5.3638          5.1966
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1662          1.1954          1.1836          1.1834


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54852          32.614          8.2896          8.0082


 TIME FOR THE TIME STEP               18:        0.85442E-01

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


 INSTANT    0.950000000E+01   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.691026684E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32971E-01
   Friction velocity        uet   :  0.13250E-02 0.20296E-01
   Friction velocity        uk    :  0.14379E-02 0.29038E-01
   Dimensionless distance   yplus :  0.22802E+00 0.37634E+01
   Friction thermal sca.    tstar : -0.56203E+01-0.28610E+00
   Rough dim-less th. sca.  tplus :  0.17013E+00 0.28079E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        164
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38386E-05     177   0.79658E-01   0.22076E-04 0.17012E+00 
c  Velocity[X]                                      0.10556E-04 
c  Velocity[Y]                                      0.11520E-04 
c  Velocity[Z]                                      0.10710E-32 
c  Pressure     0.77516E-05     386   0.35808E-02   0.93028E-01 0.25234E+00 
c  k            0.60067E-07     174   0.33750E-02   0.34613E-08 0.16715E+00 
c  epsilon      0.71870E-06      99   0.23757E-03   0.37736E-07 0.36088E+00 
c  TempC        0.21927E+01     161   0.36675E-02   0.73725E-01 0.15093E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.075362        0.075543       0.0001206     -2.7988e-07
v  Velocity[Y]          -0.046499         0.12685       0.0024476      0.00049567
v  Velocity[Z]        -8.7106e-16      6.3402e-16     -8.9361e-18     -8.1964e-18
v  ǁVelocityǁ          0.00015717         0.12966        0.033764        0.033235
v  Pressure             -0.014973        0.019734     -3.1737e-05      1.9656e-19
v  k                   1.4023e-06       0.0012698        0.000401      0.00040212
v  epsilon             1.6281e-06       0.0057474      0.00044214      0.00041776
v  TempC                    22.76          29.775           25.47           25.38
v  Density                 1.1661          1.1945          1.1835          1.1839
v  TurbVisc            6.9838e-08      0.00037014      8.5436e-05      8.7788e-05
v  CourantNb             0.075533          9.7016          2.8801          2.7751
v  FourierNb              0.42339          23.846          4.9679          4.8027
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1661          1.1945           1.183          1.1828


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53146          28.985           7.848          7.5778


 TIME FOR THE TIME STEP               19:        0.84762E-01

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


 INSTANT    0.100000000E+02   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.103232140E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32915E-01
   Friction velocity        uet   :  0.58403E-03 0.20513E-01
   Friction velocity        uk    :  0.10177E-02 0.28750E-01
   Dimensionless distance   yplus :  0.13115E+00 0.37464E+01
   Friction thermal sca.    tstar : -0.62854E+01-0.27189E+00
   Rough dim-less th. sca.  tplus :  0.97851E-01 0.27952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        160
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37930E-05     172   0.76059E-01   0.23554E-04 0.17657E+00 
c  Velocity[X]                                      0.10073E-04 
c  Velocity[Y]                                      0.13481E-04 
c  Velocity[Z]                                      0.92486E-33 
c  Pressure     0.77316E-05     385   0.33690E-02   0.93606E-01 0.25333E+00 
c  k            0.57643E-07     167   0.31878E-02   0.33369E-08 0.17365E+00 
c  epsilon      0.71510E-06      98   0.20296E-03   0.26355E-07 0.30784E+00 
c  TempC        0.22024E+01     153   0.35085E-02   0.66258E-01 0.14228E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.077632        0.077617      0.00010732      8.0645e-08
v  Velocity[Y]          -0.045567         0.12578       0.0024117      0.00052051
v  Velocity[Z]          -9.31e-16      6.6003e-16     -8.6506e-18     -7.8575e-18
v  ǁVelocityǁ          0.00035087          0.1274        0.033381        0.032882
v  Pressure              -0.01313        0.017936     -3.0713e-05      5.7653e-19
v  k                   1.0333e-06       0.0012715      0.00037618       0.0003775
v  epsilon             1.2241e-06       0.0055376      0.00042693      0.00040541
v  TempC                   22.927          29.789          25.614          25.526
v  Density                  1.166          1.1937          1.1829          1.1833
v  TurbVisc            6.0908e-08      0.00034875      7.7598e-05       7.955e-05
v  CourantNb             0.011336          9.0915          2.8226          2.7263
v  FourierNb              0.42365          21.497          4.6078           4.445
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density           1.166          1.1937          1.1824          1.1822


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51708          25.577          7.4304          7.1713


 TIME FOR THE TIME STEP               20:        0.89619E-01

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


 INSTANT    0.105000000E+02   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.479764755E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32739E-01
   Friction velocity        uet   :  0.34594E-03 0.20673E-01
   Friction velocity        uk    :  0.11455E-02 0.28531E-01
   Dimensionless distance   yplus :  0.17357E+00 0.37649E+01
   Friction thermal sca.    tstar : -0.63092E+01-0.25201E+00
   Rough dim-less th. sca.  tplus :  0.12950E+00 0.28091E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        154
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37619E-05     167   0.78130E-01   0.25341E-04 0.18321E+00 
c  Velocity[X]                                      0.95202E-05 
c  Velocity[Y]                                      0.15821E-04 
c  Velocity[Z]                                      0.83648E-33 
c  Pressure     0.77892E-05     373   0.32420E-02   0.94984E-01 0.25762E+00 
c  k            0.55456E-07     160   0.30787E-02   0.30845E-08 0.17633E+00 
c  epsilon      0.71291E-06      95   0.21997E-03   0.35263E-07 0.35647E+00 
c  TempC        0.22116E+01     146   0.35767E-02   0.60777E-01 0.13554E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.079302        0.079414       9.523e-05      8.7564e-07
v  Velocity[Y]          -0.044046         0.12389       0.0023814      0.00054629
v  Velocity[Z]        -1.0176e-15      6.8525e-16     -8.1308e-18     -7.2711e-18
v  ǁVelocityǁ          0.00048805         0.12517        0.033193        0.032688
v  Pressure              -0.01179        0.016235     -3.5056e-05      2.0973e-19
v  k                   7.6216e-07       0.0012659      0.00035292       0.0003544
v  epsilon              9.296e-07       0.0053711      0.00041563      0.00039669
v  TempC                   23.067          29.808          25.751          25.665
v  Density                  1.166           1.193          1.1823          1.1827
v  TurbVisc            4.4151e-08      0.00032637      7.0658e-05      7.2275e-05
v  CourantNb              0.03956           8.572          2.7684          2.6775
v  FourierNb              0.42403          19.581          4.2843          4.1235
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density           1.166           1.193          1.1818          1.1816


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50479          22.511          7.0528           6.801


 TIME FOR THE TIME STEP               21:        0.86439E-01

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


 INSTANT    0.110000000E+02   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.146245532E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32681E-01
   Friction velocity        uet   :  0.16281E-03 0.20020E-01
   Friction velocity        uk    :  0.48151E-03 0.28275E-01
   Dimensionless distance   yplus :  0.62086E-01 0.37660E+01
   Friction thermal sca.    tstar : -0.10223E+02-0.23239E+00
   Rough dim-less th. sca.  tplus :  0.46323E-01 0.28098E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        151
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37521E-05     162   0.67864E-01   0.25625E-04 0.18316E+00 
c  Velocity[X]                                      0.91883E-05 
c  Velocity[Y]                                      0.16437E-04 
c  Velocity[Z]                                      0.85333E-33 
c  Pressure     0.76157E-05     370   0.31231E-02   0.93115E-01 0.25594E+00 
c  k            0.53540E-07     152   0.31011E-02   0.29354E-08 0.18139E+00 
c  epsilon      0.71332E-06      94   0.14376E-03   0.25234E-07 0.30914E+00 
c  TempC        0.22203E+01     140   0.37278E-02   0.57827E-01 0.13155E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.08048        0.080748      9.1406e-05      2.5445e-06
v  Velocity[Y]           -0.04281         0.12124        0.002383      0.00057542
v  Velocity[Z]        -1.0962e-15      7.7417e-16     -7.6793e-18     -6.8144e-18
v  ǁVelocityǁ           0.0003772         0.12241        0.033347        0.032775
v  Pressure             -0.010804        0.014711     -4.4326e-05      3.1591e-19
v  k                   5.6781e-07       0.0012482      0.00033154      0.00033298
v  epsilon             7.2847e-07       0.0052318      0.00040201       0.0003824
v  TempC                   23.191          29.825          25.882          25.796
v  Density                 1.1659          1.1925          1.1818          1.1821
v  TurbVisc            3.1806e-08      0.00030086      6.4522e-05      6.5871e-05
v  CourantNb             0.023109          8.8319          2.7338          2.6439
v  FourierNb               0.4241           18.07          4.0001           3.842
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1659          1.1925          1.1813          1.1811


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49493          21.536          6.7339          6.4858


 TIME FOR THE TIME STEP               22:        0.10743E+00

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


 INSTANT    0.115000000E+02   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.510535874E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32506E-01
   Friction velocity        uet   :  0.32154E-04 0.20047E-01
   Friction velocity        uk    :  0.30186E-03 0.28005E-01
   Dimensionless distance   yplus :  0.38918E-01 0.37562E+01
   Friction thermal sca.    tstar : -0.15399E+02-0.19246E+00
   Rough dim-less th. sca.  tplus :  0.29037E-01 0.28025E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        152
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37681E-05     158   0.68369E-01   0.24395E-04 0.17667E+00 
c  Velocity[X]                                      0.88263E-05 
c  Velocity[Y]                                      0.15569E-04 
c  Velocity[Z]                                      0.75740E-33 
c  Pressure     0.74115E-05     364   0.30481E-02   0.90445E-01 0.26998E+00 
c  k            0.51996E-07     145   0.34772E-02   0.24758E-08 0.17422E+00 
c  epsilon      0.71601E-06      90   0.14173E-03   0.84352E-08 0.18135E+00 
c  TempC        0.22285E+01     136   0.36649E-02   0.56628E-01 0.12957E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.081443         0.08188      9.1656e-05       2.131e-06
v  Velocity[Y]          -0.046665          0.1195       0.0024265      0.00060554
v  Velocity[Z]        -1.1314e-15      8.5396e-16     -7.3566e-18     -6.4883e-18
v  ǁVelocityǁ          0.00049201          0.1206        0.033823        0.033114
v  Pressure            -0.0098791        0.013327     -5.8683e-05      4.5982e-19
v  k                    4.326e-07       0.0012204      0.00031322       0.0003148
v  epsilon             5.9071e-07       0.0050602      0.00038937      0.00037065
v  TempC                   23.305          29.838          26.006          25.921
v  Density                 1.1659           1.192          1.1813          1.1816
v  TurbVisc            2.3389e-08      0.00027597      5.9377e-05      6.0567e-05
v  CourantNb             0.012597          9.0906          2.7423          2.6459
v  FourierNb              0.42391          16.952          3.7572          3.6043
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1659           1.192          1.1808          1.1806


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48595          20.631          6.4995          6.2502


 TIME FOR THE TIME STEP               23:        0.90328E-01

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


 INSTANT    0.120000000E+02   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.120371323E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32467E-01
   Friction velocity        uet   :  0.11132E-04 0.20647E-01
   Friction velocity        uk    :  0.54214E-03 0.27841E-01
   Dimensionless distance   yplus :  0.69891E-01 0.37340E+01
   Friction thermal sca.    tstar : -0.80299E+01-0.16793E+00
   Rough dim-less th. sca.  tplus :  0.52147E-01 0.27860E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        153
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38032E-05     154   0.72706E-01   0.22155E-04 0.16558E+00 
c  Velocity[X]                                      0.80706E-05 
c  Velocity[Y]                                      0.14085E-04 
c  Velocity[Z]                                      0.67325E-33 
c  Pressure     0.71010E-05     364   0.30242E-02   0.86095E-01 0.29635E+00 
c  k            0.50962E-07     138   0.35961E-02   0.20135E-08 0.16325E+00 
c  epsilon      0.71894E-06      87   0.16290E-03   0.28772E-08 0.10642E+00 
c  TempC        0.22363E+01     134   0.34213E-02   0.56686E-01 0.12905E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.08255        0.082848       9.831e-05      3.0877e-06
v  Velocity[Y]          -0.050834         0.11809       0.0025186      0.00063339
v  Velocity[Z]        -1.0911e-15      9.2377e-16     -7.0387e-18     -6.2255e-18
v  ǁVelocityǁ          0.00035419         0.11911        0.034534        0.033641
v  Pressure            -0.0089946        0.012043     -7.7422e-05     -4.4929e-19
v  k                   3.4427e-07       0.0011986      0.00029782      0.00029951
v  epsilon             4.9209e-07       0.0049609      0.00038015      0.00036222
v  TempC                   23.413           29.85          26.126          26.041
v  Density                 1.1658          1.1915          1.1808          1.1811
v  TurbVisc            1.7894e-08      0.00025208      5.4986e-05      5.6051e-05
v  CourantNb             0.020432          9.3205          2.7896            2.68
v  FourierNb               0.4236          16.183          3.5482          3.3997
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1658          1.1915          1.1803          1.1801


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47847          19.939          6.3379          6.0796


 TIME FOR THE TIME STEP               24:        0.80084E-01

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


 INSTANT    0.125000000E+02   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.833136313E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32451E-01
   Friction velocity        uet   :  0.33513E-03 0.19957E-01
   Friction velocity        uk    :  0.34461E-03 0.27711E-01
   Dimensionless distance   yplus :  0.44434E-01 0.36962E+01
   Friction thermal sca.    tstar : -0.14163E+02-0.16259E+00
   Rough dim-less th. sca.  tplus :  0.33153E-01 0.27578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        155
   Total number of wall faces                   :        384
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         25, Physical time    0.12500E+02


   ** 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


 Time for restart files:    0.10141E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38498E-05     150   0.72807E-01   0.20432E-04 0.15586E+00 
c  Velocity[X]                                      0.72032E-05 
c  Velocity[Y]                                      0.13229E-04 
c  Velocity[Z]                                      0.75845E-33 
c  Pressure     0.69709E-05     370   0.30115E-02   0.83686E-01 0.33582E+00 
c  k            0.50133E-07     132   0.33652E-02   0.15902E-08 0.15031E+00 
c  epsilon      0.72098E-06      84   0.15981E-03   0.28079E-08 0.10567E+00 
c  TempC        0.22437E+01     132   0.38331E-02   0.56286E-01 0.12804E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.08308        0.083421      0.00010761      2.8544e-06
v  Velocity[Y]          -0.054662         0.11672       0.0026688      0.00065807
v  Velocity[Z]        -1.0597e-15      9.8298e-16     -6.5929e-18     -5.9136e-18
v  ǁVelocityǁ          0.00061268         0.11766         0.03538        0.034282
v  Pressure            -0.0081347        0.010856     -9.9666e-05      8.9507e-20
v  k                   2.9415e-07       0.0011878      0.00028467      0.00028632
v  epsilon             4.1893e-07       0.0048579      0.00037246      0.00035479
v  TempC                   23.513          29.859          26.242          26.157
v  Density                 1.1658          1.1911          1.1803          1.1806
v  TurbVisc            1.4687e-08      0.00023346      5.1171e-05      5.2118e-05
v  CourantNb             0.011456          9.5226           2.865          2.7374
v  FourierNb              0.42331          15.704          3.3708          3.2248
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1658          1.1911          1.1798          1.1797


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47013          19.435          6.2358          5.9622


 TIME FOR THE TIME STEP               25:        0.14169E+00

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


 INSTANT    0.130000000E+02   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.375209126E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32445E-01
   Friction velocity        uet   :  0.29604E-03 0.20681E-01
   Friction velocity        uk    :  0.30429E-03 0.27659E-01
   Dimensionless distance   yplus :  0.39232E-01 0.36480E+01
   Friction thermal sca.    tstar : -0.14890E+02-0.16538E+00
   Rough dim-less th. sca.  tplus :  0.29271E-01 0.27218E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        165
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39044E-05     147   0.76241E-01   0.20158E-04 0.15158E+00 
c  Velocity[X]                                      0.66721E-05 
c  Velocity[Y]                                      0.13486E-04 
c  Velocity[Z]                                      0.72980E-33 
c  Pressure     0.67196E-05     368   0.29546E-02   0.79720E-01 0.37606E+00 
c  k            0.49193E-07     127   0.31296E-02   0.13686E-08 0.14441E+00 
c  epsilon      0.71767E-06      82   0.15445E-03   0.10532E-07 0.20759E+00 
c  TempC        0.22508E+01     131   0.38411E-02   0.55218E-01 0.12629E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.082986        0.083493      0.00011836      1.6789e-06
v  Velocity[Y]          -0.057872         0.11544       0.0028667      0.00067619
v  Velocity[Z]        -1.0161e-15      1.0432e-15     -6.1566e-18     -5.5751e-18
v  ǁVelocityǁ          0.00022572          0.1164        0.036252        0.034961
v  Pressure            -0.0073054       0.0097512     -0.00012401      6.6516e-19
v  k                     2.76e-07       0.0011565      0.00027307      0.00027467
v  epsilon             3.7341e-07       0.0047401       0.0003612      0.00034463
v  TempC                   23.617          29.865          26.354          26.269
v  Density                 1.1657          1.1907          1.1798          1.1802
v  TurbVisc            1.3326e-08      0.00021498      4.7867e-05      4.8697e-05
v  CourantNb              0.02458          9.7303          2.9568          2.8096
v  FourierNb              0.42306          15.358          3.2177          3.0737
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1657          1.1907          1.1794          1.1793


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            0.46          18.755          6.1745          5.8834


 TIME FOR THE TIME STEP               26:        0.79353E-01

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


 INSTANT    0.135000000E+02   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.211758237E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32436E-01
   Friction velocity        uet   :  0.91915E-03 0.20661E-01
   Friction velocity        uk    :  0.10833E-02 0.27488E-01
   Dimensionless distance   yplus :  0.17168E+00 0.36283E+01
   Friction thermal sca.    tstar : -0.65151E+01-0.16480E+00
   Rough dim-less th. sca.  tplus :  0.12809E+00 0.27072E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        166
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39635E-05     144   0.75690E-01   0.20317E-04 0.14898E+00 
c  Velocity[X]                                      0.58327E-05 
c  Velocity[Y]                                      0.14484E-04 
c  Velocity[Z]                                      0.67069E-33 
c  Pressure     0.66146E-05     369   0.28384E-02   0.77456E-01 0.42170E+00 
c  k            0.48207E-07     123   0.29362E-02   0.12347E-08 0.14201E+00 
c  epsilon      0.71420E-06      80   0.15170E-03   0.25214E-08 0.10313E+00 
c  TempC        0.22576E+01     131   0.39389E-02   0.52204E-01 0.12230E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.082403        0.083324      0.00012989      1.1081e-06
v  Velocity[Y]          -0.060631         0.11525        0.003108      0.00068841
v  Velocity[Z]        -1.0724e-15      1.0731e-15     -5.7053e-18     -5.1781e-18
v  ǁVelocityǁ          0.00094197         0.11776        0.037136        0.035669
v  Pressure            -0.0065997       0.0087072     -0.00014892      4.3525e-19
v  k                   2.8488e-07       0.0011284       0.0002632      0.00026469
v  epsilon             3.5068e-07       0.0046073      0.00035324      0.00033681
v  TempC                    23.72           29.87          26.462          26.378
v  Density                 1.1657          1.1903          1.1794          1.1797
v  TurbVisc            1.3653e-08      0.00019756      4.5032e-05      4.5758e-05
v  CourantNb             0.018357          10.625          3.0574          2.8914
v  FourierNb              0.42284          15.175          3.0848          2.9424
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1657          1.1903          1.1789          1.1788


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45318          18.463          6.1422          5.8338


 TIME FOR THE TIME STEP               27:        0.78440E-01

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


 INSTANT    0.140000000E+02   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.263374307E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32388E-01
   Friction velocity        uet   :  0.13810E-03 0.20728E-01
   Friction velocity        uk    :  0.81105E-03 0.27349E-01
   Dimensionless distance   yplus :  0.12853E+00 0.36081E+01
   Friction thermal sca.    tstar : -0.61864E+01-0.17067E+00
   Rough dim-less th. sca.  tplus :  0.95901E-01 0.26920E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        173
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40195E-05     142   0.73584E-01   0.22127E-04 0.15258E+00 
c  Velocity[X]                                      0.60543E-05 
c  Velocity[Y]                                      0.16072E-04 
c  Velocity[Z]                                      0.63686E-33 
c  Pressure     0.65216E-05     367   0.26411E-02   0.75428E-01 0.44608E+00 
c  k            0.47061E-07     120   0.27702E-02   0.12094E-08 0.14542E+00 
c  epsilon      0.70668E-06      79   0.14814E-03   0.80254E-08 0.18825E+00 
c  TempC        0.22643E+01     130   0.45239E-02   0.48617E-01 0.11756E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.082031        0.083243      0.00013686     -1.2795e-06
v  Velocity[Y]          -0.062308         0.11842       0.0033731      0.00069725
v  Velocity[Z]         -1.134e-15      1.1022e-15     -5.3802e-18     -4.8773e-18
v  ǁVelocityǁ          0.00047239         0.12079        0.037956        0.036323
v  Pressure            -0.0060117        0.007763      -0.0001729      1.0881e-19
v  k                   3.2675e-07       0.0011021      0.00025437      0.00025584
v  epsilon             3.9007e-07        0.004514      0.00034347      0.00032719
v  TempC                   23.824          29.875          26.566          26.485
v  Density                 1.1657          1.1898           1.179          1.1793
v  TurbVisc            1.5631e-08      0.00018132      4.2605e-05      4.3249e-05
v  CourantNb             0.010865           11.33          3.1622          2.9793
v  FourierNb              0.42257          14.775          2.9705          2.8307
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1657          1.1898          1.1785          1.1784


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4451          19.048          6.1327            5.81


 TIME FOR THE TIME STEP               28:        0.77896E-01

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


 INSTANT    0.145000000E+02   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.725271961E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32317E-01
   Friction velocity        uet   :  0.78633E-03 0.20440E-01
   Friction velocity        uk    :  0.80694E-03 0.27319E-01
   Dimensionless distance   yplus :  0.12788E+00 0.35759E+01
   Friction thermal sca.    tstar : -0.55871E+01-0.16733E+00
   Rough dim-less th. sca.  tplus :  0.95410E-01 0.26680E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        175
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40721E-05     142   0.85074E-01   0.22874E-04 0.15271E+00 
c  Velocity[X]                                      0.61823E-05 
c  Velocity[Y]                                      0.16692E-04 
c  Velocity[Z]                                      0.61288E-33 
c  Pressure     0.63352E-05     366   0.24467E-02   0.72509E-01 0.45702E+00 
c  k            0.45887E-07     117   0.26369E-02   0.11361E-08 0.14552E+00 
c  epsilon      0.69551E-06      78   0.14324E-03   0.39519E-08 0.13569E+00 
c  TempC        0.22709E+01     129   0.50994E-02   0.45036E-01 0.11271E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.081184        0.082539      0.00014319     -2.1806e-06
v  Velocity[Y]          -0.064142         0.12052       0.0036316      0.00070269
v  Velocity[Z]        -1.1954e-15        1.14e-15     -5.0979e-18     -4.6242e-18
v  ǁVelocityǁ          0.00029146         0.12278        0.038641        0.036873
v  Pressure            -0.0062228       0.0084956      -0.0001942      6.8096e-19
v  k                   4.3306e-07       0.0010686      0.00024663      0.00024818
v  epsilon             5.4222e-07       0.0044645      0.00033381      0.00031798
v  TempC                   23.926          29.878          26.666          26.589
v  Density                 1.1657          1.1894          1.1786          1.1789
v  TurbVisc            1.9128e-08      0.00016522      4.0549e-05       4.114e-05
v  CourantNb             0.012775          11.561          3.2624          3.0639
v  FourierNb              0.42227          14.025          2.8709          2.7338
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1657          1.1894          1.1781           1.178


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44635          19.452          6.1334          5.7977


 TIME FOR THE TIME STEP               29:        0.78022E-01

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


 INSTANT    0.150000000E+02   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.469838588E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32261E-01
   Friction velocity        uet   :  0.79181E-03 0.20254E-01
   Friction velocity        uk    :  0.97714E-03 0.27324E-01
   Dimensionless distance   yplus :  0.15484E+00 0.35383E+01
   Friction thermal sca.    tstar : -0.67546E+01-0.17016E+00
   Rough dim-less th. sca.  tplus :  0.11553E+00 0.26399E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        178
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41098E-05     143   0.87918E-01   0.22471E-04 0.14956E+00 
c  Velocity[X]                                      0.63895E-05 
c  Velocity[Y]                                      0.16081E-04 
c  Velocity[Z]                                      0.65875E-33 
c  Pressure     0.63482E-05     367   0.23389E-02   0.72119E-01 0.44983E+00 
c  k            0.44710E-07     115   0.25473E-02   0.10519E-08 0.14417E+00 
c  epsilon      0.68038E-06      77   0.13404E-03   0.59729E-08 0.17168E+00 
c  TempC        0.22774E+01     128   0.40804E-02   0.42219E-01 0.10873E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.079854        0.081324      0.00014747     -3.0392e-06
v  Velocity[Y]          -0.066038         0.12174       0.0038609      0.00070562
v  Velocity[Z]         -1.298e-15      1.2012e-15     -4.7568e-18     -4.3215e-18
v  ǁVelocityǁ          0.00043531         0.12381        0.039135        0.037267
v  Pressure            -0.0070871       0.0099492     -0.00021339     -2.1061e-20
v  k                   6.3641e-07       0.0010425      0.00023967      0.00024144
v  epsilon             7.5052e-07       0.0044306      0.00032421      0.00030873
v  TempC                   24.033           29.88          26.762           26.69
v  Density                 1.1656           1.189          1.1782          1.1785
v  TurbVisc            2.6124e-08      0.00015207      3.8821e-05      3.9388e-05
v  CourantNb            0.0076814          11.727          3.3438          3.1329
v  FourierNb              0.42202          13.079          2.7859          2.6526
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656           1.189          1.1778          1.1777


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44359          19.631          6.1297          5.7855


 TIME FOR THE TIME STEP               30:        0.78506E-01

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


 INSTANT    0.155000000E+02   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.956220788E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32195E-01
   Friction velocity        uet   :  0.46159E-03 0.20774E-01
   Friction velocity        uk    :  0.53113E-03 0.27631E-01
   Dimensionless distance   yplus :  0.84167E-01 0.35672E+01
   Friction thermal sca.    tstar : -0.67467E+01-0.17241E+00
   Rough dim-less th. sca.  tplus :  0.62798E-01 0.26616E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        181
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41325E-05     142   0.88812E-01   0.20270E-04 0.14095E+00 
c  Velocity[X]                                      0.61284E-05 
c  Velocity[Y]                                      0.14141E-04 
c  Velocity[Z]                                      0.67481E-33 
c  Pressure     0.61556E-05     367   0.22548E-02   0.69690E-01 0.42773E+00 
c  k            0.43585E-07     114   0.24644E-02   0.94301E-09 0.14011E+00 
c  epsilon      0.66409E-06      76   0.12091E-03   0.68830E-08 0.18958E+00 
c  TempC        0.22838E+01     127   0.44801E-02   0.39339E-01 0.10457E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.078089        0.079312       0.0001504     -3.2248e-06
v  Velocity[Y]           -0.06758         0.12247       0.0040423      0.00070954
v  Velocity[Z]        -1.3324e-15      1.2222e-15     -4.4118e-18     -4.0231e-18
v  ǁVelocityǁ          0.00044389         0.12328        0.039429          0.0375
v  Pressure            -0.0078913        0.011286     -0.00023058      5.6512e-19
v  k                   5.1196e-07       0.0010199      0.00023341      0.00023552
v  epsilon             5.4912e-07       0.0045436      0.00031449      0.00029954
v  TempC                   24.139          29.882          26.854          26.788
v  Density                 1.1656          1.1886          1.1778          1.1781
v  TurbVisc            2.4074e-08      0.00014318      3.7391e-05      3.7961e-05
v  CourantNb             0.019098          12.249           3.406          3.1866
v  FourierNb              0.42189          12.453          2.7141          2.5855
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656          1.1886          1.1774          1.1773


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45755          19.629          6.1201           5.772


 TIME FOR THE TIME STEP               31:        0.77113E-01

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


 INSTANT    0.160000000E+02   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.459250676E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32161E-01
   Friction velocity        uet   :  0.14361E-03 0.20236E-01
   Friction velocity        uk    :  0.16793E-03 0.27902E-01
   Dimensionless distance   yplus :  0.26600E-01 0.36024E+01
   Friction thermal sca.    tstar : -0.70111E+01-0.17830E+00
   Rough dim-less th. sca.  tplus :  0.19847E-01 0.26878E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        184
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41359E-05     142   0.91231E-01   0.16750E-04 0.12782E+00 
c  Velocity[X]                                      0.55903E-05 
c  Velocity[Y]                                      0.11159E-04 
c  Velocity[Z]                                      0.74526E-33 
c  Pressure     0.62164E-05     367   0.22678E-02   0.70426E-01 0.39259E+00 
c  k            0.42564E-07     113   0.22948E-02   0.79531E-09 0.13167E+00 
c  epsilon      0.64814E-06      75   0.10343E-03   0.42374E-08 0.15289E+00 
c  TempC        0.22900E+01     126   0.40736E-02   0.36962E-01 0.10102E-01 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.075548        0.076934      0.00014919     -2.3753e-06
v  Velocity[Y]          -0.068407         0.12402       0.0041572      0.00071238
v  Velocity[Z]        -1.3514e-15      1.2437e-15     -4.0535e-18     -3.6991e-18
v  ǁVelocityǁ          0.00049144         0.12467        0.039479         0.03753
v  Pressure            -0.0085353        0.012514     -0.00024425     -2.6677e-19
v  k                   4.4719e-07       0.0010047      0.00022776      0.00023027
v  epsilon             5.1492e-07       0.0045904      0.00030468      0.00029041
v  TempC                   24.246          29.885          26.943          26.883
v  Density                 1.1656          1.1882          1.1774          1.1777
v  TurbVisc            2.0428e-08       0.0001357      3.6234e-05      3.6826e-05
v  CourantNb             0.025245          12.714          3.4493          3.2251
v  FourierNb              0.42176          12.168          2.6582          2.5342
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656          1.1882           1.177          1.1769


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44998          19.484          6.1074          5.7593


 TIME FOR THE TIME STEP               32:        0.78065E-01

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


 INSTANT    0.165000000E+02   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.895340295E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32154E-01
   Friction velocity        uet   :  0.10774E-03 0.20565E-01
   Friction velocity        uk    :  0.98205E-03 0.27785E-01
   Dimensionless distance   yplus :  0.15561E+00 0.35872E+01
   Friction thermal sca.    tstar : -0.64130E+01-0.17278E+00
   Rough dim-less th. sca.  tplus :  0.11611E+00 0.26764E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        189
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41128E-05     141   0.91738E-01   0.13357E-04 0.11453E+00 
c  Velocity[X]                                      0.48829E-05 
c  Velocity[Y]                                      0.84742E-05 
c  Velocity[Z]                                      0.72323E-33 
c  Pressure     0.61480E-05     367   0.22887E-02   0.69973E-01 0.35666E+00 
c  k            0.41594E-07     112   0.20729E-02   0.65357E-09 0.12182E+00 
c  epsilon      0.63015E-06      74   0.87000E-04   0.43991E-08 0.16019E+00 
c  TempC        0.22962E+01     125   0.33350E-02   0.34291E-01 0.96971E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.072927        0.074145       0.0001411     -2.4625e-06
v  Velocity[Y]          -0.068815         0.12421       0.0042055       0.0007167
v  Velocity[Z]        -1.3508e-15      1.2454e-15     -3.7138e-18     -3.3917e-18
v  ǁVelocityǁ          0.00022345         0.12476         0.03928        0.037352
v  Pressure            -0.0090601        0.013591      -0.0002554     -5.4231e-19
v  k                   4.5138e-07      0.00099711      0.00022259      0.00022555
v  epsilon              4.876e-07        0.004566      0.00029449      0.00028123
v  TempC                   24.354          29.887          27.029          26.975
v  Density                 1.1656          1.1877          1.1771          1.1773
v  TurbVisc            2.0487e-08      0.00013174      3.5315e-05      3.5943e-05
v  CourantNb             0.011392          13.167          3.4699          3.2453
v  FourierNb              0.42165          11.905          2.6115          2.4918
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656          1.1877          1.1767          1.1766


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44618           19.25          6.0814          5.7371


 TIME FOR THE TIME STEP               33:        0.77245E-01

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


 INSTANT    0.170000000E+02   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.406972861E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32144E-01
   Friction velocity        uet   :  0.17402E-03 0.20449E-01
   Friction velocity        uk    :  0.79144E-03 0.27830E-01
   Dimensionless distance   yplus :  0.12541E+00 0.35935E+01
   Friction thermal sca.    tstar : -0.64969E+01-0.17065E+00
   Rough dim-less th. sca.  tplus :  0.93570E-01 0.26811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        195
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40700E-05     141   0.86994E-01   0.10828E-04 0.10417E+00 
c  Velocity[X]                                      0.43295E-05 
c  Velocity[Y]                                      0.64983E-05 
c  Velocity[Z]                                      0.76292E-33 
c  Pressure     0.60478E-05     367   0.22732E-02   0.69362E-01 0.32362E+00 
c  k            0.40675E-07     110   0.18190E-02   0.51935E-09 0.11064E+00 
c  epsilon      0.61063E-06      73   0.72484E-04   0.54753E-08 0.18384E+00 
c  TempC        0.23021E+01     124   0.37115E-02   0.31302E-01 0.92350E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.070668        0.072697      0.00012996     -4.1334e-06
v  Velocity[Y]          -0.069062         0.12273        0.004188      0.00072264
v  Velocity[Z]        -1.3165e-15       1.273e-15     -3.5452e-18     -3.1979e-18
v  ǁVelocityǁ          0.00029161         0.12324        0.038828        0.036954
v  Pressure            -0.0094192        0.014539     -0.00026318     -1.3689e-18
v  k                   4.1003e-07      0.00098651      0.00021778      0.00022118
v  epsilon             5.3741e-07       0.0045935      0.00028394      0.00027199
v  TempC                   24.465          29.888          27.112          27.063
v  Density                 1.1656          1.1873          1.1767           1.177
v  TurbVisc            1.7649e-08       0.0001294      3.4605e-05      3.5275e-05
v  CourantNb            0.0049154          13.378           3.465          3.2434
v  FourierNb              0.42187            11.7          2.5772          2.4618
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656          1.1873          1.1764          1.1762


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47349           18.94          6.0422          5.7053


 TIME FOR THE TIME STEP               34:        0.76694E-01

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


 INSTANT    0.175000000E+02   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.122158033E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32122E-01
   Friction velocity        uet   :  0.46585E-04 0.20704E-01
   Friction velocity        uk    :  0.20380E-03 0.27694E-01
   Dimensionless distance   yplus :  0.32282E-01 0.35761E+01
   Friction thermal sca.    tstar : -0.67108E+01-0.17129E+00
   Rough dim-less th. sca.  tplus :  0.24086E-01 0.26681E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        202
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40011E-05     141   0.82189E-01   0.91918E-05 0.97607E-01 
c  Velocity[X]                                      0.38084E-05 
c  Velocity[Y]                                      0.53835E-05 
c  Velocity[Z]                                      0.84897E-33 
c  Pressure     0.58151E-05     367   0.22112E-02   0.67392E-01 0.29273E+00 
c  k            0.39758E-07     108   0.15396E-02   0.39930E-09 0.98750E-01 
c  epsilon      0.58797E-06      72   0.59695E-04   0.56382E-08 0.19255E+00 
c  TempC        0.23078E+01     122   0.30581E-02   0.28674E-01 0.88114E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.069707        0.071484      0.00012018     -3.7176e-06
v  Velocity[Y]          -0.069673         0.12002       0.0041169      0.00072916
v  Velocity[Z]        -1.2856e-15      1.2974e-15     -3.6071e-18     -3.2816e-18
v  ǁVelocityǁ          0.00025926         0.12032        0.038143        0.036348
v  Pressure            -0.0096713        0.015372      -0.0002677     -3.9137e-19
v  k                   4.4449e-07      0.00097481      0.00021323      0.00021698
v  epsilon             6.1539e-07       0.0045148      0.00027313      0.00026236
v  TempC                   24.565          29.889          27.193          27.149
v  Density                 1.1656          1.1869          1.1764          1.1766
v  TurbVisc            1.9228e-08      0.00012834       3.406e-05      3.4773e-05
v  CourantNb             0.011006          13.252          3.4324          3.2164
v  FourierNb              0.42195          11.551          2.5476           2.435
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656          1.1869          1.1761          1.1759


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45553           18.69            5.98          5.6514


 TIME FOR THE TIME STEP               35:        0.76062E-01

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


 INSTANT    0.180000000E+02   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.101246907E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32117E-01
   Friction velocity        uet   :  0.49531E-03 0.18845E-01
   Friction velocity        uk    :  0.49401E-03 0.27479E-01
   Dimensionless distance   yplus :  0.78253E-01 0.35485E+01
   Friction thermal sca.    tstar : -0.71994E+01-0.16317E+00
   Rough dim-less th. sca.  tplus :  0.58386E-01 0.26476E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        202
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39083E-05     140   0.81793E-01   0.86842E-05 0.97063E-01 
c  Velocity[X]                                      0.33733E-05 
c  Velocity[Y]                                      0.53109E-05 
c  Velocity[Z]                                      0.75285E-33 
c  Pressure     0.56932E-05     369   0.21283E-02   0.66797E-01 0.26869E+00 
c  k            0.38914E-07     106   0.13019E-02   0.29557E-09 0.86486E-01 
c  epsilon      0.56681E-06      71   0.51933E-04   0.11241E-08 0.88267E-01 
c  TempC        0.23133E+01     121   0.29481E-02   0.25544E-01 0.82917E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.06901        0.070103      0.00010929     -3.3423e-06
v  Velocity[Y]          -0.069666         0.11602       0.0040013      0.00073654
v  Velocity[Z]        -1.2581e-15      1.3169e-15     -3.7179e-18     -3.4024e-18
v  ǁVelocityǁ          0.00010428         0.11635        0.037271        0.035573
v  Pressure            -0.0097378        0.016118     -0.00026906      5.0721e-19
v  k                   4.8959e-07      0.00096347        0.000209      0.00021304
v  epsilon             6.8746e-07       0.0044277      0.00026486      0.00025497
v  TempC                    24.65           29.89          27.272          27.232
v  Density                 1.1656          1.1865          1.1761          1.1763
v  TurbVisc            2.0629e-08      0.00012664      3.3655e-05       3.441e-05
v  CourantNb             0.016027          12.943          3.3738           3.165
v  FourierNb              0.42206          11.436          2.5273          2.4176
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656          1.1865          1.1757          1.1756


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43997          18.385          5.9011          5.5826


 TIME FOR THE TIME STEP               36:        0.79070E-01

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


 INSTANT    0.185000000E+02   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.480426500E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32140E-01
   Friction velocity        uet   :  0.24210E-03 0.20602E-01
   Friction velocity        uk    :  0.42977E-03 0.27114E-01
   Dimensionless distance   yplus :  0.68074E-01 0.35015E+01
   Friction thermal sca.    tstar : -0.75854E+01-0.16045E+00
   Rough dim-less th. sca.  tplus :  0.50791E-01 0.26125E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        207
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37961E-05     139   0.76551E-01   0.99238E-05 0.10679E+00 
c  Velocity[X]                                      0.34156E-05 
c  Velocity[Y]                                      0.65082E-05 
c  Velocity[Z]                                      0.64599E-33 
c  Pressure     0.56353E-05     367   0.20070E-02   0.67033E-01 0.23818E+00 
c  k            0.37989E-07     104   0.11017E-02   0.24796E-09 0.80738E-01 
c  epsilon      0.54345E-06      70   0.48815E-04   0.41341E-08 0.17437E+00 
c  TempC        0.23185E+01     118   0.25728E-02   0.22808E-01 0.78125E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.068113        0.068687      0.00010068       -3.78e-06
v  Velocity[Y]          -0.069336         0.11141       0.0038474      0.00074647
v  Velocity[Z]        -1.2267e-15      1.3365e-15     -3.9854e-18     -3.6924e-18
v  ǁVelocityǁ          0.00016632         0.11153        0.036228        0.034652
v  Pressure             -0.009635        0.016746     -0.00026766     -8.5471e-19
v  k                   5.5375e-07      0.00094856      0.00020461      0.00020889
v  epsilon             7.8991e-07       0.0042828      0.00025524      0.00024664
v  TempC                   24.732            29.9          27.348          27.312
v  Density                 1.1656          1.1861          1.1758          1.1759
v  TurbVisc            2.4315e-08      0.00012523      3.3337e-05      3.4132e-05
v  CourantNb            0.0062653          12.465           3.294          3.0937
v  FourierNb              0.42221          11.333          2.5125          2.4051
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656          1.1861          1.1754          1.1753


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4315           18.05          5.8065          5.4989


 TIME FOR THE TIME STEP               37:        0.80583E-01

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


 INSTANT    0.190000000E+02   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.739830340E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32152E-01
   Friction velocity        uet   :  0.10333E-03 0.20410E-01
   Friction velocity        uk    :  0.78883E-03 0.26743E-01
   Dimensionless distance   yplus :  0.12494E+00 0.34537E+01
   Friction thermal sca.    tstar : -0.76531E+01-0.15123E+00
   Rough dim-less th. sca.  tplus :  0.93220E-01 0.25768E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        210
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36720E-05     137   0.75390E-01   0.12003E-04 0.12144E+00 
c  Velocity[X]                                      0.37225E-05 
c  Velocity[Y]                                      0.82809E-05 
c  Velocity[Z]                                      0.57417E-33 
c  Pressure     0.55646E-05     367   0.19680E-02   0.67137E-01 0.21647E+00 
c  k            0.37012E-07     102   0.10034E-02   0.21415E-09 0.76642E-01 
c  epsilon      0.51796E-06      69   0.50839E-04   0.34754E-08 0.16528E+00 
c  TempC        0.23236E+01     116   0.25443E-02   0.19996E-01 0.72947E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.066494        0.066981      9.5638e-05     -3.1869e-06
v  Velocity[Y]          -0.068634         0.10588       0.0036627      0.00075625
v  Velocity[Z]         -1.193e-15      1.3604e-15     -4.2969e-18     -3.9959e-18
v  ǁVelocityǁ          0.00050684         0.10597        0.035069        0.033636
v  Pressure            -0.0093615        0.017304     -0.00026363     -1.0425e-18
v  k                   5.3881e-07      0.00092882          0.0002      0.00020447
v  epsilon             8.5358e-07       0.0041187      0.00024552      0.00023819
v  TempC                   24.812          29.906          27.422          27.389
v  Density                 1.1656          1.1858          1.1755          1.1756
v  TurbVisc            2.3338e-08      0.00012399      3.3069e-05      3.3899e-05
v  CourantNb              0.01975          12.218          3.1958          3.0058
v  FourierNb              0.42237          11.238          2.4981          2.3925
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1656          1.1858          1.1752           1.175


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44483          17.604          5.6939          5.3983


 TIME FOR THE TIME STEP               38:        0.77515E-01

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


 INSTANT    0.195000000E+02   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.105217374E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32130E-01
   Friction velocity        uet   :  0.50996E-04 0.20349E-01
   Friction velocity        uk    :  0.12345E-02 0.26096E-01
   Dimensionless distance   yplus :  0.18101E+00 0.33702E+01
   Friction thermal sca.    tstar : -0.76255E+01-0.14037E+00
   Rough dim-less th. sca.  tplus :  0.13505E+00 0.25146E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        213
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35406E-05     135   0.77244E-01   0.14578E-04 0.13889E+00 
c  Velocity[X]                                      0.42499E-05 
c  Velocity[Y]                                      0.10328E-04 
c  Velocity[Z]                                      0.54159E-33 
c  Pressure     0.55202E-05     367   0.19612E-02   0.67530E-01 0.19493E+00 
c  k            0.35961E-07     100   0.97288E-03   0.20293E-09 0.76412E-01 
c  epsilon      0.49240E-06      68   0.57130E-04   0.37430E-08 0.17748E+00 
c  TempC        0.23284E+01     113   0.22269E-02   0.17439E-01 0.67941E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.065007        0.065063      9.4331e-05      -2.647e-06
v  Velocity[Y]           -0.06704         0.09965        0.003459      0.00076732
v  Velocity[Z]        -1.1606e-15      1.3847e-15     -4.6132e-18        -4.3e-18
v  ǁVelocityǁ          0.00020895        0.099727        0.033829        0.032561
v  Pressure             -0.009012        0.017819     -0.00025832      1.3202e-18
v  k                   5.7397e-07      0.00090115      0.00019511       0.0001997
v  epsilon             8.6675e-07       0.0039252      0.00023565      0.00022964
v  TempC                   24.913          29.912          27.495          27.463
v  Density                 1.1655          1.1855          1.1752          1.1753
v  TurbVisc            2.4739e-08      0.00012219      3.2814e-05      3.3673e-05
v  CourantNb             0.024909          12.007          3.0848          2.9068
v  FourierNb              0.42235           11.17          2.4856          2.3816
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1655          1.1855          1.1749          1.1747


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46215          17.144          5.5704          5.2885


 TIME FOR THE TIME STEP               39:        0.77008E-01

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


 INSTANT    0.200000000E+02   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.109717236E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.32005E-01
   Friction velocity        uet   :  0.32885E-03 0.20582E-01
   Friction velocity        uk    :  0.16621E-02 0.25469E-01
   Dimensionless distance   yplus :  0.21441E+00 0.32891E+01
   Friction thermal sca.    tstar : -0.70074E+01-0.13328E+00
   Rough dim-less th. sca.  tplus :  0.15997E+00 0.24540E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        217
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34081E-05     132   0.71224E-01   0.17457E-04 0.15811E+00 
c  Velocity[X]                                      0.49716E-05 
c  Velocity[Y]                                      0.12486E-04 
c  Velocity[Z]                                      0.51578E-33 
c  Pressure     0.54931E-05     366   0.19740E-02   0.68051E-01 0.17385E+00 
c  k            0.34843E-07      97   0.99527E-03   0.21636E-09 0.81062E-01 
c  epsilon      0.46686E-06      67   0.64777E-04   0.47997E-08 0.20864E+00 
c  TempC        0.23331E+01     109   0.19143E-02   0.15362E-01 0.63602E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.063202        0.062878      9.4509e-05     -3.3191e-06
v  Velocity[Y]          -0.065577        0.093006       0.0032399      0.00077811
v  Velocity[Z]        -1.1929e-15      1.4231e-15     -4.9635e-18     -4.6605e-18
v  ǁVelocityǁ          0.00016285        0.093065        0.032528        0.031445
v  Pressure            -0.0086083        0.018289     -0.00025165      1.1759e-19
v  k                   5.8727e-07      0.00087442      0.00018987      0.00019455
v  epsilon             8.7178e-07         0.00372      0.00022501      0.00022049
v  TempC                   24.999          29.916          27.565          27.535
v  Density                 1.1655          1.1851          1.1749           1.175
v  TurbVisc            2.6674e-08      0.00011989      3.2559e-05      3.3441e-05
v  CourantNb             0.055781          11.643          2.9649          2.8011
v  FourierNb               0.4225          11.194          2.4724          2.3693
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1655          1.1851          1.1746          1.1744


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48071          16.575          5.4373          5.1705


 TIME FOR THE TIME STEP               40:        0.76422E-01

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


 INSTANT    0.205000000E+02   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.118319915E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.31753E-01
   Friction velocity        uet   :  0.49630E-03 0.20578E-01
   Friction velocity        uk    :  0.11865E-02 0.24744E-01
   Dimensionless distance   yplus :  0.17011E+00 0.31953E+01
   Friction thermal sca.    tstar : -0.65132E+01-0.12094E+00
   Rough dim-less th. sca.  tplus :  0.12692E+00 0.23841E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        221
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32837E-05     129   0.76651E-01   0.19849E-04 0.17546E+00 
c  Velocity[X]                                      0.56917E-05 
c  Velocity[Y]                                      0.14157E-04 
c  Velocity[Z]                                      0.51427E-33 
c  Pressure     0.51941E-05     363   0.20166E-02   0.65015E-01 0.15535E+00 
c  k            0.33663E-07      94   0.10657E-02   0.24477E-09 0.88889E-01 
c  epsilon      0.44160E-06      66   0.69466E-04   0.51394E-08 0.22472E+00 
c  TempC        0.23376E+01     106   0.19615E-02   0.13863E-01 0.60270E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.061141        0.060581      9.6754e-05     -3.2646e-06
v  Velocity[Y]          -0.063687        0.086268       0.0030155      0.00079139
v  Velocity[Z]        -1.1476e-15      1.4469e-15     -5.3031e-18     -4.9557e-18
v  ǁVelocityǁ          0.00053686        0.086754        0.031203        0.030319
v  Pressure            -0.0081389        0.018738     -0.00024447      1.2987e-18
v  k                   6.4455e-07      0.00084352      0.00018432      0.00018902
v  epsilon             8.7093e-07       0.0034689      0.00021403        0.000211
v  TempC                     25.1          29.919          27.633          27.604
v  Density                 1.1655          1.1847          1.1746          1.1748
v  TurbVisc            2.9378e-08      0.00011718      3.2289e-05      3.3186e-05
v  CourantNb             0.062327          11.251          2.8378          2.6899
v  FourierNb              0.42271          11.245          2.4583          2.3557
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1655          1.1847          1.1743          1.1742


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48858           16.02           5.296          5.0456


 TIME FOR THE TIME STEP               41:        0.75971E-01

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


 INSTANT    0.210000000E+02   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.719978005E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.31353E-01
   Friction velocity        uet   :  0.80329E-03 0.20476E-01
   Friction velocity        uk    :  0.79795E-03 0.24016E-01
   Dimensionless distance   yplus :  0.12639E+00 0.31007E+01
   Friction thermal sca.    tstar : -0.66096E+01-0.10058E+00
   Rough dim-less th. sca.  tplus :  0.94302E-01 0.23135E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        225
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31679E-05     126   0.70359E-01   0.21786E-04 0.19115E+00 
c  Velocity[X]                                      0.63803E-05 
c  Velocity[Y]                                      0.15406E-04 
c  Velocity[Z]                                      0.56398E-33 
c  Pressure     0.50679E-05     359   0.20519E-02   0.63940E-01 0.14018E+00 
c  k            0.32432E-07      92   0.12422E-02   0.28427E-09 0.99121E-01 
c  epsilon      0.41763E-06      64   0.82118E-04   0.51201E-08 0.23379E+00 
c  TempC        0.23419E+01     102   0.16737E-02   0.12977E-01 0.58173E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.058878        0.058135      0.00010083     -3.1843e-06
v  Velocity[Y]          -0.061668        0.080873       0.0027894      0.00080309
v  Velocity[Z]        -1.1388e-15      1.4797e-15     -5.5987e-18     -5.1933e-18
v  ǁVelocityǁ          0.00012825        0.081263        0.029915         0.02924
v  Pressure            -0.0082166        0.019191     -0.00023739      7.1079e-20
v  k                   7.1266e-07      0.00080821       0.0001785      0.00018317
v  epsilon             8.6965e-07       0.0032464      0.00020299      0.00020139
v  TempC                    25.19          29.922            27.7          27.671
v  Density                 1.1655          1.1843          1.1744          1.1745
v  TurbVisc            3.0024e-08      0.00011402      3.1991e-05      3.2896e-05
v  CourantNb             0.057154          10.767           2.705          2.5741
v  FourierNb              0.42266          11.293          2.4455          2.3438
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1655          1.1843          1.1741          1.1739


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48258          15.398          5.1505           4.918


 TIME FOR THE TIME STEP               42:        0.73664E-01

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


 INSTANT    0.215000000E+02   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.645862622E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.30841E-01
   Friction velocity        uet   :  0.22670E-03 0.20320E-01
   Friction velocity        uk    :  0.42180E-03 0.23294E-01
   Dimensionless distance   yplus :  0.66809E-01 0.30751E+01
   Friction thermal sca.    tstar : -0.63682E+01-0.92481E-01
   Rough dim-less th. sca.  tplus :  0.49847E-01 0.22944E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        229
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30620E-05     122   0.63608E-01   0.22511E-04 0.20155E+00 
c  Velocity[X]                                      0.67849E-05 
c  Velocity[Y]                                      0.15726E-04 
c  Velocity[Z]                                      0.69638E-33 
c  Pressure     0.48478E-05     358   0.20563E-02   0.61515E-01 0.12796E+00 
c  k            0.31173E-07      89   0.14020E-02   0.33069E-09 0.11103E+00 
c  epsilon      0.39536E-06      63   0.87542E-04   0.51803E-08 0.24534E+00 
c  TempC        0.23460E+01      99   0.15876E-02   0.12419E-01 0.56776E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.056377        0.055504      0.00010608     -2.7348e-06
v  Velocity[Y]          -0.059375        0.075273        0.002568       0.0008137
v  Velocity[Z]        -1.1611e-15      1.5154e-15     -6.0131e-18      -5.497e-18
v  ǁVelocityǁ          3.0329e-05         0.07555        0.028718        0.028252
v  Pressure            -0.0087044        0.019661      -0.0002311     -8.2487e-19
v  k                   7.7484e-07      0.00077178      0.00017246      0.00017706
v  epsilon             8.6412e-07       0.0030216      0.00019202      0.00019177
v  TempC                   25.275          29.924          27.765          27.736
v  Density                 1.1655           1.184          1.1741          1.1742
v  TurbVisc            3.1615e-08      0.00011042      3.1654e-05      3.2562e-05
v  CourantNb             0.031649          10.187          2.5757          2.4631
v  FourierNb              0.42268          11.315          2.4305          2.3287
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1655           1.184          1.1738          1.1736


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47645          14.697          5.0062          4.7918


 TIME FOR THE TIME STEP               43:        0.72543E-01

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


 INSTANT    0.220000000E+02   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.608804931E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.30182E-01
   Friction velocity        uet   :  0.35504E-03 0.20244E-01
   Friction velocity        uk    :  0.12503E-02 0.22510E-01
   Dimensionless distance   yplus :  0.16116E+00 0.30975E+01
   Friction thermal sca.    tstar : -0.52357E+01-0.82387E-01
   Rough dim-less th. sca.  tplus :  0.12024E+00 0.23111E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        233
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29719E-05     118   0.57421E-01   0.22083E-04 0.20635E+00 
c  Velocity[X]                                      0.68907E-05 
c  Velocity[Y]                                      0.15192E-04 
c  Velocity[Z]                                      0.77154E-33 
c  Pressure     0.47084E-05     358   0.20392E-02   0.59978E-01 0.11773E+00 
c  k            0.29905E-07      87   0.15801E-02   0.37650E-09 0.12350E+00 
c  epsilon      0.37523E-06      61   0.93821E-04   0.50792E-08 0.25350E+00 
c  TempC        0.23500E+01      95   0.13507E-02   0.12204E-01 0.56158E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.053744        0.052776      0.00011003     -2.6327e-06
v  Velocity[Y]          -0.056438        0.071525        0.002356      0.00082254
v  Velocity[Z]        -1.2128e-15      1.5497e-15     -6.4164e-18     -5.7772e-18
v  ǁVelocityǁ          0.00019412        0.071546        0.027642        0.027377
v  Pressure            -0.0091741        0.020154     -0.00022589     -1.4655e-18
v  k                   8.2375e-07      0.00073531      0.00016625      0.00017075
v  epsilon             8.5084e-07       0.0027988      0.00018128      0.00018231
v  TempC                   25.356          29.926          27.827          27.799
v  Density                 1.1655          1.1836          1.1739           1.174
v  TurbVisc            3.3211e-08      0.00010657       3.127e-05      3.2175e-05
v  CourantNb             0.041885          9.6551          2.4558          2.3618
v  FourierNb              0.42274          11.304          2.4128          2.3113
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1655          1.1836          1.1736          1.1734


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47356          14.077          4.8686          4.6731


 TIME FOR THE TIME STEP               44:        0.73512E-01

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


 INSTANT    0.225000000E+02   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.432780896E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.29404E-01
   Friction velocity        uet   :  0.47758E-04 0.20751E-01
   Friction velocity        uk    :  0.12009E-02 0.21740E-01
   Dimensionless distance   yplus :  0.15503E+00 0.31205E+01
   Friction thermal sca.    tstar : -0.71393E+01-0.80284E-01
   Rough dim-less th. sca.  tplus :  0.11567E+00 0.23283E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        239
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28974E-05     114   0.56730E-01   0.20815E-04 0.20625E+00 
c  Velocity[X]                                      0.67297E-05 
c  Velocity[Y]                                      0.14085E-04 
c  Velocity[Z]                                      0.81639E-33 
c  Pressure     0.45077E-05     357   0.19904E-02   0.57560E-01 0.10884E+00 
c  k            0.28606E-07      86   0.17477E-02   0.42518E-09 0.13733E+00 
c  epsilon      0.35599E-06      60   0.99625E-04   0.72623E-08 0.31740E+00 
c  TempC        0.23538E+01      92   0.13960E-02   0.12054E-01 0.55691E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.051099        0.049959      0.00011272     -2.5783e-06
v  Velocity[Y]          -0.054433        0.072084       0.0021557      0.00083013
v  Velocity[Z]        -1.2673e-15      1.5893e-15     -6.9214e-18     -6.0975e-18
v  ǁVelocityǁ          0.00028426         0.07238        0.026725        0.026648
v  Pressure            -0.0096244        0.020657      -0.0002218     -7.5467e-19
v  k                    8.485e-07      0.00069813      0.00015984      0.00016425
v  epsilon              8.245e-07       0.0025886      0.00016991      0.00017239
v  TempC                   25.435          29.928          27.889           27.86
v  Density                 1.1655          1.1833          1.1736          1.1737
v  TurbVisc            3.4567e-08      0.00010237      3.0832e-05      3.1732e-05
v  CourantNb             0.026987          9.0845           2.347          2.2707
v  FourierNb              0.42258          11.153          2.3937          2.2922
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1655          1.1833          1.1733          1.1732


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48689          13.894          4.7407          4.5629


 TIME FOR THE TIME STEP               45:        0.74156E-01

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


 INSTANT    0.230000000E+02   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.152201233E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.28594E-01
   Friction velocity        uet   :  0.32337E-03 0.20651E-01
   Friction velocity        uk    :  0.55603E-03 0.21017E-01
   Dimensionless distance   yplus :  0.88064E-01 0.31336E+01
   Friction thermal sca.    tstar : -0.62381E+01-0.74854E-01
   Rough dim-less th. sca.  tplus :  0.65705E-01 0.23380E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        252
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28322E-05     111   0.54132E-01   0.19489E-04 0.20483E+00 
c  Velocity[X]                                      0.65884E-05 
c  Velocity[Y]                                      0.12900E-04 
c  Velocity[Z]                                      0.89519E-33 
c  Pressure     0.44517E-05     357   0.19293E-02   0.56920E-01 0.10060E+00 
c  k            0.27214E-07      85   0.18405E-02   0.47838E-09 0.15295E+00 
c  epsilon      0.33430E-06      59   0.98988E-04   0.14424E-07 0.47397E+00 
c  TempC        0.23574E+01      89   0.13699E-02   0.12058E-01 0.55586E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.048484         0.04721      0.00010977     -3.8869e-06
v  Velocity[Y]          -0.052439        0.072446        0.001965      0.00083505
v  Velocity[Z]        -1.2841e-15      1.6322e-15     -7.4479e-18     -6.4591e-18
v  ǁVelocityǁ          0.00027831        0.072933        0.025916        0.026011
v  Pressure             -0.010079        0.021145     -0.00021869     -7.3273e-19
v  k                   8.5148e-07      0.00066049      0.00015314      0.00015753
v  epsilon             7.8163e-07       0.0023989      0.00015573      0.00016056
v  TempC                   25.515          29.933          27.948          27.918
v  Density                 1.1655           1.183          1.1734          1.1735
v  TurbVisc            3.5623e-08      9.7697e-05      3.0341e-05      3.1236e-05
v  CourantNb             0.040272          8.5137          2.2562          2.1962
v  FourierNb              0.42245          10.819           2.371          2.2696
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1655           1.183          1.1731           1.173


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49047           13.98          4.6272          4.4658


 TIME FOR THE TIME STEP               46:        0.73524E-01

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


 INSTANT    0.235000000E+02   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.705419626E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.27987E-01
   Friction velocity        uet   :  0.10054E-03 0.20664E-01
   Friction velocity        uk    :  0.69228E-03 0.20586E-01
   Dimensionless distance   yplus :  0.89277E-01 0.31425E+01
   Friction thermal sca.    tstar : -0.77348E+01-0.72258E-01
   Rough dim-less th. sca.  tplus :  0.66611E-01 0.23447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        256
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27744E-05     107   0.51858E-01   0.16513E-04 0.19282E+00 
c  Velocity[X]                                      0.59327E-05 
c  Velocity[Y]                                      0.10580E-04 
c  Velocity[Z]                                      0.94510E-33 
c  Pressure     0.42630E-05     357   0.18234E-02   0.54523E-01 0.96014E-01 
c  k            0.26030E-07      86   0.18852E-02   0.46391E-09 0.15844E+00 
c  epsilon      0.32344E-06      59   0.97818E-04   0.42866E-08 0.26809E+00 
c  TempC        0.23610E+01      86   0.12116E-02   0.11930E-01 0.55179E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.045979        0.045009      0.00010738     -2.9788e-06
v  Velocity[Y]          -0.050199        0.072496       0.0018058       0.0008414
v  Velocity[Z]        -1.4386e-15      1.6761e-15     -8.0085e-18     -6.8541e-18
v  ǁVelocityǁ          0.00081756        0.073197        0.025215        0.025449
v  Pressure             -0.010523        0.021727      -0.0002172      1.8217e-18
v  k                   7.9927e-07      0.00062225      0.00014679      0.00015106
v  epsilon             7.2854e-07       0.0022461      0.00014615       0.0001519
v  TempC                   25.594          29.937          28.006          27.976
v  Density                 1.1654          1.1827          1.1731          1.1733
v  TurbVisc            3.7147e-08      9.2664e-05      2.9824e-05      3.0708e-05
v  CourantNb             0.017357          7.9644          2.1808          2.1349
v  FourierNb              0.42237          10.513          2.3439          2.2429
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1654          1.1827          1.1729          1.1727


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50885          14.168          4.5247          4.3778


 TIME FOR THE TIME STEP               47:        0.71774E-01

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


 INSTANT    0.240000000E+02   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.311019910E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.27725E-01
   Friction velocity        uet   :  0.48116E-03 0.20752E-01
   Friction velocity        uk    :  0.51202E-03 0.20372E-01
   Dimensionless distance   yplus :  0.66014E-01 0.31456E+01
   Friction thermal sca.    tstar : -0.89904E+01-0.71395E-01
   Rough dim-less th. sca.  tplus :  0.49254E-01 0.23470E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        261
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27246E-05     103   0.50674E-01   0.13777E-04 0.17969E+00 
c  Velocity[X]                                      0.52087E-05 
c  Velocity[Y]                                      0.85678E-05 
c  Velocity[Z]                                      0.11879E-32 
c  Pressure     0.41144E-05     354   0.16919E-02   0.52610E-01 0.88332E-01 
c  k            0.24877E-07      86   0.18969E-02   0.47051E-09 0.16800E+00 
c  epsilon      0.31203E-06      58   0.97338E-04   0.54887E-08 0.31568E+00 
c  TempC        0.23644E+01      85   0.12939E-02   0.11620E-01 0.54350E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.044496         0.04593      0.00010077      -4.054e-06
v  Velocity[Y]          -0.048283        0.072255       0.0016725      0.00084602
v  Velocity[Z]        -1.4359e-15      1.7263e-15     -8.5517e-18     -7.2716e-18
v  ǁVelocityǁ          0.00011094        0.073172        0.024607        0.024944
v  Pressure             -0.011147        0.022322     -0.00021592      1.2636e-18
v  k                   7.4343e-07        0.000584      0.00014056      0.00014471
v  epsilon             6.7059e-07       0.0022026      0.00013695      0.00014356
v  TempC                   25.668          29.941          28.063          28.031
v  Density                 1.1654          1.1824          1.1729           1.173
v  TurbVisc            3.7856e-08      9.3806e-05      2.9282e-05      3.0153e-05
v  CourantNb             0.023047          7.4377          2.1169          2.0818
v  FourierNb              0.42234          10.881          2.3184          2.2178
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1654          1.1824          1.1727          1.1725


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51815          15.141          4.4354          4.2995


 TIME FOR THE TIME STEP               48:        0.68804E-01

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


 INSTANT    0.245000000E+02   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.236904527E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.27396E-01
   Friction velocity        uet   :  0.75575E-03 0.20301E-01
   Friction velocity        uk    :  0.10134E-02 0.20118E-01
   Dimensionless distance   yplus :  0.13064E+00 0.31429E+01
   Friction thermal sca.    tstar : -0.43947E+01-0.70363E-01
   Rough dim-less th. sca.  tplus :  0.97470E-01 0.23450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        265
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26769E-05     101   0.50977E-01   0.11195E-04 0.16509E+00 
c  Velocity[X]                                      0.44554E-05 
c  Velocity[Y]                                      0.67392E-05 
c  Velocity[Z]                                      0.11623E-32 
c  Pressure     0.39289E-05     355   0.16158E-02   0.50199E-01 0.82557E-01 
c  k            0.23812E-07      85   0.18665E-02   0.44501E-09 0.17197E+00 
c  epsilon      0.30199E-06      58   0.94163E-04   0.45154E-08 0.29723E+00 
c  TempC        0.23677E+01      83   0.14236E-02   0.11241E-01 0.53356E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.046063        0.046431      9.4082e-05      -3.655e-06
v  Velocity[Y]          -0.046635        0.071874       0.0015652      0.00084809
v  Velocity[Z]        -1.2834e-15      1.7641e-15     -9.1068e-18     -7.7504e-18
v  ǁVelocityǁ          0.00030662        0.072933         0.02406        0.024466
v  Pressure             -0.011952        0.022912     -0.00021439     -2.4571e-20
v  k                   6.9387e-07      0.00054607      0.00013447      0.00013849
v  epsilon             6.1113e-07        0.002134      0.00012865      0.00013589
v  TempC                   25.748          29.944          28.118          28.085
v  Density                 1.1654          1.1821          1.1727          1.1728
v  TurbVisc            3.4401e-08      9.8027e-05      2.8704e-05      2.9561e-05
v  CourantNb             0.025292          7.0411           2.065          2.0371
v  FourierNb              0.42232          11.488          2.2904          2.1904
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1654          1.1821          1.1724          1.1723


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52944          15.951          4.3553          4.2275


 TIME FOR THE TIME STEP               49:        0.69699E-01

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


 INSTANT    0.250000000E+02   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.491014412E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.26941E-01
   Friction velocity        uet   :  0.24292E-03 0.20709E-01
   Friction velocity        uk    :  0.68634E-03 0.19775E-01
   Dimensionless distance   yplus :  0.89087E-01 0.31354E+01
   Friction thermal sca.    tstar : -0.69246E+01-0.69888E-01
   Rough dim-less th. sca.  tplus :  0.66469E-01 0.23393E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        272
   Total number of wall faces                   :        384
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         50, Physical time    0.25000E+02


   ** 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


 Time for restart files:    0.92649E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26295E-05      99   0.50471E-01   0.92049E-05 0.15271E+00 
c  Velocity[X]                                      0.38222E-05 
c  Velocity[Y]                                      0.53828E-05 
c  Velocity[Z]                                      0.96799E-33 
c  Pressure     0.36823E-05     350   0.15012E-02   0.46990E-01 0.75354E-01 
c  k            0.22764E-07      85   0.18333E-02   0.41860E-09 0.17542E+00 
c  epsilon      0.28953E-06      57   0.90995E-04   0.65092E-08 0.37328E+00 
c  TempC        0.23710E+01      82   0.12904E-02   0.10539E-01 0.51567E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.045915         0.04648      8.7566e-05     -3.8844e-06
v  Velocity[Y]          -0.046364        0.071534       0.0014792      0.00084868
v  Velocity[Z]        -1.3702e-15       1.795e-15     -9.6277e-18      -8.227e-18
v  ǁVelocityǁ          0.00065841        0.072371        0.023531        0.023973
v  Pressure             -0.012726        0.023476     -0.00021182      5.5459e-18
v  k                   6.3101e-07      0.00050834      0.00012838      0.00013233
v  epsilon             5.5033e-07       0.0020502      0.00011947       0.0001277
v  TempC                   25.821          29.947          28.171          28.137
v  Density                 1.1654          1.1818          1.1725          1.1726
v  TurbVisc            3.1369e-08      0.00010087      2.8078e-05      2.8925e-05
v  CourantNb             0.014408          6.9905          2.0204           1.997
v  FourierNb              0.42215          11.934           2.257          2.1577
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1654          1.1818          1.1722          1.1721


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53765          16.545          4.2774          4.1548


 TIME FOR THE TIME STEP               50:        0.20424E+00

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


 INSTANT    0.255000000E+02   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.113820052E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.26335E-01
   Friction velocity        uet   :  0.36047E-03 0.20578E-01
   Friction velocity        uk    :  0.55888E-03 0.19714E-01
   Dimensionless distance   yplus :  0.72046E-01 0.31257E+01
   Friction thermal sca.    tstar : -0.74343E+01-0.69898E-01
   Rough dim-less th. sca.  tplus :  0.53754E-01 0.23321E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        275
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25770E-05      98   0.47957E-01   0.75279E-05 0.14106E+00 
c  Velocity[X]                                      0.32497E-05 
c  Velocity[Y]                                      0.42781E-05 
c  Velocity[Z]                                      0.98833E-33 
c  Pressure     0.34352E-05     350   0.14025E-02   0.43758E-01 0.71908E-01 
c  k            0.21844E-07      84   0.17796E-02   0.37239E-09 0.17372E+00 
c  epsilon      0.27955E-06      56   0.84785E-04   0.45609E-08 0.32419E+00 
c  TempC        0.23741E+01      80   0.11343E-02   0.96924E-02 0.49366E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.04626        0.047081      8.1341e-05      -3.256e-06
v  Velocity[Y]          -0.045385        0.070429        0.001417      0.00085069
v  Velocity[Z]        -1.3898e-15      1.8124e-15     -1.0038e-17     -8.6697e-18
v  ǁVelocityǁ          0.00041092        0.071673        0.023001        0.023451
v  Pressure             -0.013477        0.024022     -0.00020858     -2.0394e-18
v  k                      5.7e-07      0.00047556      0.00012253      0.00012639
v  epsilon             4.8094e-07       0.0019276       0.0001121      0.00012095
v  TempC                   25.895           29.95          28.222          28.188
v  Density                 1.1654          1.1815          1.1723          1.1724
v  TurbVisc            2.9115e-08      0.00010174      2.7406e-05      2.8245e-05
v  CourantNb             0.020367          6.8508          1.9789          1.9575
v  FourierNb              0.42205           12.22           2.224           2.127
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1654          1.1815           1.172          1.1719


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53346           16.94           4.203          4.0845


 TIME FOR THE TIME STEP               51:        0.71049E-01

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


 INSTANT    0.260000000E+02   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.244845461E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25739E-01
   Friction velocity        uet   :  0.92511E-03 0.20426E-01
   Friction velocity        uk    :  0.92985E-03 0.19596E-01
   Dimensionless distance   yplus :  0.11987E+00 0.31067E+01
   Friction thermal sca.    tstar : -0.46115E+01-0.71933E-01
   Rough dim-less th. sca.  tplus :  0.89439E-01 0.23180E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        280
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25204E-05      98   0.48039E-01   0.64608E-05 0.13377E+00 
c  Velocity[X]                                      0.28895E-05 
c  Velocity[Y]                                      0.35713E-05 
c  Velocity[Z]                                      0.10542E-32 
c  Pressure     0.32625E-05     349   0.13148E-02   0.41475E-01 0.66859E-01 
c  k            0.20953E-07      83   0.17207E-02   0.32975E-09 0.17134E+00 
c  epsilon      0.26755E-06      55   0.79323E-04   0.58738E-08 0.38413E+00 
c  TempC        0.23771E+01      79   0.10317E-02   0.87828E-02 0.46912E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.04574        0.046688      7.4775e-05     -2.8643e-06
v  Velocity[Y]          -0.044133        0.069428       0.0013743      0.00085203
v  Velocity[Z]        -1.3549e-15      1.8266e-15     -1.0317e-17      -9.036e-18
v  ǁVelocityǁ           0.0005094        0.070655        0.022434        0.022877
v  Pressure             -0.014202        0.024528     -0.00020417     -8.1785e-19
v  k                   5.1443e-07      0.00044284      0.00011682       0.0001206
v  epsilon              4.193e-07       0.0017567      0.00010427      0.00011395
v  TempC                   25.968          29.952          28.272          28.237
v  Density                 1.1654          1.1812          1.1721          1.1722
v  TurbVisc             2.685e-08      0.00010056      2.6706e-05      2.7535e-05
v  CourantNb             0.010442          6.9686          1.9362          1.9147
v  FourierNb              0.42198          12.341          2.1889          2.0935
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1654          1.1812          1.1718          1.1718


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54698           17.13          4.1251          4.0082


 TIME FOR THE TIME STEP               52:        0.70749E-01

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


 INSTANT    0.265000000E+02   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.299108509E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25654E-01
   Friction velocity        uet   :  0.35828E-03 0.19725E-01
   Friction velocity        uk    :  0.38394E-03 0.19456E-01
   Dimensionless distance   yplus :  0.60807E-01 0.30844E+01
   Friction thermal sca.    tstar : -0.31597E+01-0.72642E-01
   Rough dim-less th. sca.  tplus :  0.45369E-01 0.23013E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        287
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24607E-05      97   0.46616E-01   0.58438E-05 0.13055E+00 
c  Velocity[X]                                      0.27608E-05 
c  Velocity[Y]                                      0.30830E-05 
c  Velocity[Z]                                      0.93061E-33 
c  Pressure     0.31733E-05     350   0.13174E-02   0.40250E-01 0.62257E-01 
c  k            0.20100E-07      82   0.16775E-02   0.28060E-09 0.16536E+00 
c  epsilon      0.25589E-06      54   0.74226E-04   0.58065E-08 0.39926E+00 
c  TempC        0.23801E+01      78   0.96823E-03   0.79111E-02 0.44449E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.046135        0.046134      6.7204e-05     -2.4499e-06
v  Velocity[Y]          -0.042357        0.068683        0.001351      0.00085422
v  Velocity[Z]        -1.3487e-15      1.8411e-15     -1.0607e-17     -9.3786e-18
v  ǁVelocityǁ          0.00036223        0.069511        0.021817        0.022246
v  Pressure             -0.014895         0.02499     -0.00019907     -1.9095e-18
v  k                   4.5229e-07      0.00043273      0.00011132      0.00011499
v  epsilon             3.6214e-07       0.0016481      9.6493e-05      0.00010679
v  TempC                   26.036          29.953           28.32          28.284
v  Density                 1.1654          1.1809          1.1719           1.172
v  TurbVisc            2.3141e-08      9.8891e-05      2.5985e-05      2.6801e-05
v  CourantNb             0.041269          6.9377          1.8893           1.867
v  FourierNb              0.42184          12.312          2.1544          2.0607
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1654          1.1809          1.1716          1.1716


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54019          17.123          4.0437          3.9277


 TIME FOR THE TIME STEP               53:        0.70138E-01

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


 INSTANT    0.270000000E+02   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384        -0.105879118E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25553E-01
   Friction velocity        uet   :  0.45299E-03 0.17193E-01
   Friction velocity        uk    :  0.11125E-02 0.19348E-01
   Dimensionless distance   yplus :  0.14336E+00 0.30674E+01
   Friction thermal sca.    tstar : -0.43558E+01-0.72412E-01
   Rough dim-less th. sca.  tplus :  0.10697E+00 0.22886E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        288
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23951E-05      96   0.47478E-01   0.53446E-05 0.12837E+00 
c  Velocity[X]                                      0.26021E-05 
c  Velocity[Y]                                      0.27425E-05 
c  Velocity[Z]                                      0.82463E-33 
c  Pressure     0.30287E-05     353   0.13569E-02   0.38318E-01 0.59929E-01 
c  k            0.19418E-07      81   0.16602E-02   0.21655E-09 0.15166E+00 
c  epsilon      0.25031E-06      53   0.68145E-04   0.59285E-09 0.13094E+00 
c  TempC        0.23829E+01      76   0.83009E-03   0.71968E-02 0.42327E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.045322        0.046378      6.0239e-05     -1.9456e-06
v  Velocity[Y]          -0.040112        0.067098       0.0013491      0.00085915
v  Velocity[Z]        -1.4131e-15       1.858e-15     -1.0949e-17     -9.7364e-18
v  ǁVelocityǁ          0.00019013        0.068249        0.021181         0.02159
v  Pressure             -0.015572        0.025428     -0.00019415      -1.053e-19
v  k                   3.7365e-07      0.00042409      0.00010629      0.00010977
v  epsilon             3.1013e-07       0.0016167      9.1731e-05      0.00010176
v  TempC                   26.101          29.955          28.367           28.33
v  Density                 1.1654          1.1806          1.1717          1.1718
v  TurbVisc            2.0373e-08      9.8107e-05      2.5258e-05      2.6056e-05
v  CourantNb             0.031306          6.8319          1.8353          1.8124
v  FourierNb              0.42175          12.158          2.1164          2.0244
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1654          1.1806          1.1715          1.1714


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53111          16.938          3.9517          3.8368


 TIME FOR THE TIME STEP               54:        0.68790E-01

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


 INSTANT    0.275000000E+02   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384        -0.794093388E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25424E-01
   Friction velocity        uet   :  0.74469E-03 0.17835E-01
   Friction velocity        uk    :  0.94168E-03 0.19141E-01
   Dimensionless distance   yplus :  0.12134E+00 0.30344E+01
   Friction thermal sca.    tstar : -0.37471E+01-0.74038E-01
   Rough dim-less th. sca.  tplus :  0.90531E-01 0.22640E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        288
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23300E-05      95   0.46959E-01   0.53168E-05 0.13176E+00 
c  Velocity[X]                                      0.26162E-05 
c  Velocity[Y]                                      0.27006E-05 
c  Velocity[Z]                                      0.77210E-33 
c  Pressure     0.28384E-05     351   0.13545E-02   0.35817E-01 0.55809E-01 
c  k            0.18782E-07      79   0.16931E-02   0.17784E-09 0.14325E+00 
c  epsilon      0.24426E-06      51   0.65514E-04   0.15486E-09 0.68638E-01 
c  TempC        0.23857E+01      75   0.84341E-03   0.64746E-02 0.40086E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.044997        0.045566      5.3363e-05     -1.4351e-06
v  Velocity[Y]          -0.037887        0.065771       0.0013607      0.00086409
v  Velocity[Z]        -1.4487e-15      1.8833e-15     -1.1341e-17     -1.0067e-17
v  ǁVelocityǁ          0.00024791        0.066923        0.020553        0.020946
v  Pressure             -0.016218        0.025832     -0.00018916     -5.1247e-19
v  k                   3.1224e-07      0.00041114      0.00010159      0.00010488
v  epsilon             2.6299e-07        0.001582      8.7747e-05      9.7453e-05
v  TempC                   26.167          29.957          28.411          28.374
v  Density                 1.1653          1.1804          1.1715          1.1716
v  TurbVisc            1.7009e-08      9.5167e-05      2.4537e-05      2.5313e-05
v  CourantNb             0.024129          6.6125          1.7782          1.7549
v  FourierNb              0.42165          11.912          2.0807          1.9902
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1804          1.1713          1.1712


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51553          16.608          3.8589          3.7452


 TIME FOR THE TIME STEP               55:        0.68595E-01

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


 INSTANT    0.280000000E+02   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.164112634E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25284E-01
   Friction velocity        uet   :  0.52352E-03 0.18183E-01
   Friction velocity        uk    :  0.52165E-03 0.18960E-01
   Dimensionless distance   yplus :  0.67223E-01 0.30055E+01
   Friction thermal sca.    tstar : -0.59458E+01-0.74025E-01
   Rough dim-less th. sca.  tplus :  0.50156E-01 0.22424E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        290
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.22671E-05      93   0.45105E-01   0.57014E-05 0.14057E+00 
c  Velocity[X]                                      0.28061E-05 
c  Velocity[Y]                                      0.28953E-05 
c  Velocity[Z]                                      0.65598E-33 
c  Pressure     0.27664E-05     352   0.13076E-02   0.34826E-01 0.51248E-01 
c  k            0.18152E-07      77   0.17210E-02   0.15395E-09 0.13880E+00 
c  epsilon      0.23735E-06      50   0.64132E-04   0.78160E-09 0.15873E+00 
c  TempC        0.23884E+01      73   0.84710E-03   0.59206E-02 0.38275E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.045149        0.044815      4.5933e-05     -9.8331e-07
v  Velocity[Y]           -0.03577        0.064428       0.0013825      0.00086968
v  Velocity[Z]        -1.4761e-15      1.9172e-15     -1.1702e-17     -1.0366e-17
v  ǁVelocityǁ          0.00023119        0.065377        0.019937        0.020321
v  Pressure             -0.016817        0.026206     -0.00018416     -1.2812e-18
v  k                   2.6304e-07      0.00039873      9.7122e-05       0.0001002
v  epsilon             2.1947e-07       0.0015455      8.3732e-05      9.3008e-05
v  TempC                   26.227          29.958          28.454          28.417
v  Density                 1.1653          1.1801          1.1713          1.1715
v  TurbVisc            1.4294e-08      9.3466e-05       2.382e-05      2.4572e-05
v  CourantNb             0.014182          6.2945           1.722          1.6989
v  FourierNb              0.42156          11.596          2.0454          1.9563
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1801          1.1711          1.1711


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5103          16.169          3.7675          3.6552


 TIME FOR THE TIME STEP               56:        0.75644E-01

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


 INSTANT    0.285000000E+02   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.484396967E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25108E-01
   Friction velocity        uet   :  0.50480E-03 0.18441E-01
   Friction velocity        uk    :  0.78023E-03 0.18751E-01
   Dimensionless distance   yplus :  0.10057E+00 0.29725E+01
   Friction thermal sca.    tstar : -0.49654E+01-0.78798E-01
   Rough dim-less th. sca.  tplus :  0.75038E-01 0.22178E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        290
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.22057E-05      92   0.43375E-01   0.60391E-05 0.14895E+00 
c  Velocity[X]                                      0.29254E-05 
c  Velocity[Y]                                      0.31137E-05 
c  Velocity[Z]                                      0.61495E-33 
c  Pressure     0.26747E-05     349   0.12368E-02   0.33589E-01 0.48281E-01 
c  k            0.17571E-07      76   0.17130E-02   0.13166E-09 0.13354E+00 
c  epsilon      0.23042E-06      49   0.61970E-04   0.14514E-09 0.70317E-01 
c  TempC        0.23910E+01      71   0.74329E-03   0.54193E-02 0.36566E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.04375        0.043587      3.8675e-05     -5.6184e-07
v  Velocity[Y]          -0.034191         0.06329       0.0014085      0.00087441
v  Velocity[Z]        -1.5005e-15      1.9601e-15     -1.2137e-17     -1.0698e-17
v  ǁVelocityǁ          0.00044408        0.063971        0.019356        0.019739
v  Pressure             -0.017396        0.026555     -0.00017915     -2.6115e-18
v  k                   2.1492e-07      0.00037852      9.2927e-05      9.5807e-05
v  epsilon             1.7946e-07        0.001506      8.0247e-05      8.9164e-05
v  TempC                   26.288          29.959          28.496          28.458
v  Density                 1.1653          1.1799          1.1712          1.1713
v  TurbVisc            1.2012e-08      8.9658e-05      2.3111e-05      2.3837e-05
v  CourantNb             0.020538          5.8919          1.6665          1.6443
v  FourierNb              0.42149          11.237          2.0098          1.9216
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1799           1.171          1.1709


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.491          15.644          3.6763          3.5659


 TIME FOR THE TIME STEP               57:        0.71980E-01

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


 INSTANT    0.290000000E+02   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.269991752E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24954E-01
   Friction velocity        uet   :  0.15217E-03 0.18340E-01
   Friction velocity        uk    :  0.63967E-03 0.18592E-01
   Dimensionless distance   yplus :  0.82400E-01 0.29471E+01
   Friction thermal sca.    tstar : -0.49142E+01-0.76387E-01
   Rough dim-less th. sca.  tplus :  0.61480E-01 0.21989E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        291
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21503E-05      90   0.42175E-01   0.63934E-05 0.15759E+00 
c  Velocity[X]                                      0.30398E-05 
c  Velocity[Y]                                      0.33536E-05 
c  Velocity[Z]                                      0.65121E-33 
c  Pressure     0.26209E-05     349   0.11817E-02   0.32828E-01 0.45113E-01 
c  k            0.17008E-07      74   0.16877E-02   0.12280E-09 0.13413E+00 
c  epsilon      0.22330E-06      48   0.58909E-04   0.42651E-09 0.12394E+00 
c  TempC        0.23935E+01      70   0.65196E-03   0.50266E-02 0.35168E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.043236        0.043087      3.0781e-05      8.2263e-08
v  Velocity[Y]          -0.033244        0.061767       0.0014377       0.0008796
v  Velocity[Z]        -1.5458e-15      2.0092e-15     -1.2505e-17     -1.1001e-17
v  ǁVelocityǁ          0.00016403        0.062561        0.018815        0.019205
v  Pressure             -0.017935         0.02688     -0.00017409     -4.7737e-19
v  k                   1.7642e-07      0.00036312      8.8928e-05      9.1627e-05
v  epsilon             1.4614e-07       0.0014672      7.6905e-05      8.5469e-05
v  TempC                   26.347           29.96          28.536          28.498
v  Density                 1.1653          1.1796           1.171          1.1711
v  TurbVisc            9.7574e-09      8.6446e-05      2.2409e-05      2.3107e-05
v  CourantNb             0.037064          5.8026          1.6143          1.5941
v  FourierNb              0.42141          10.847          1.9759          1.8887
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1796          1.1708          1.1708


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47912          15.057          3.5902          3.4828


 TIME FOR THE TIME STEP               58:        0.66954E-01

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


 INSTANT    0.295000000E+02   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.457927187E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24764E-01
   Friction velocity        uet   :  0.36800E-03 0.18410E-01
   Friction velocity        uk    :  0.74694E-03 0.18374E-01
   Dimensionless distance   yplus :  0.96214E-01 0.29124E+01
   Friction thermal sca.    tstar : -0.38539E+01-0.76223E-01
   Rough dim-less th. sca.  tplus :  0.71786E-01 0.21730E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        292
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21002E-05      88   0.46190E-01   0.66075E-05 0.16431E+00 
c  Velocity[X]                                      0.30655E-05 
c  Velocity[Y]                                      0.35420E-05 
c  Velocity[Z]                                      0.64130E-33 
c  Pressure     0.25952E-05     348   0.11372E-02   0.32408E-01 0.42554E-01 
c  k            0.16461E-07      72   0.16494E-02   0.11463E-09 0.13474E+00 
c  epsilon      0.21596E-06      46   0.55927E-04   0.42042E-09 0.12679E+00 
c  TempC        0.23960E+01      68   0.54720E-03   0.46902E-02 0.33925E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.041321         0.04188       2.409e-05       3.684e-07
v  Velocity[Y]          -0.032593        0.060539       0.0014683      0.00088492
v  Velocity[Z]        -1.5904e-15       2.142e-15     -1.2874e-17     -1.1294e-17
v  ǁVelocityǁ          6.9226e-05        0.061355        0.018325        0.018729
v  Pressure             -0.018441         0.02719     -0.00016897      3.5347e-18
v  k                   1.4642e-07      0.00033966      8.5126e-05      8.7648e-05
v  epsilon             1.1882e-07       0.0014314      7.3626e-05      8.1838e-05
v  TempC                   26.404          29.961          28.574          28.537
v  Density                 1.1653          1.1794          1.1708           1.171
v  TurbVisc            8.0733e-09      8.2695e-05      2.1715e-05      2.2382e-05
v  CourantNb               0.0133          5.8881          1.5663           1.549
v  FourierNb              0.42136           10.44          1.9434          1.8572
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1794          1.1707          1.1706


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46839          14.414          3.5097          3.4062


 TIME FOR THE TIME STEP               59:        0.67180E-01

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


 INSTANT    0.300000000E+02   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.487043945E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24601E-01
   Friction velocity        uet   :  0.92339E-05 0.18378E-01
   Friction velocity        uk    :  0.55332E-03 0.18199E-01
   Dimensionless distance   yplus :  0.71269E-01 0.28846E+01
   Friction thermal sca.    tstar : -0.37559E+01-0.77371E-01
   Rough dim-less th. sca.  tplus :  0.53175E-01 0.21522E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        293
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20578E-05      86   0.44201E-01   0.66620E-05 0.16864E+00 
c  Velocity[X]                                      0.30078E-05 
c  Velocity[Y]                                      0.36542E-05 
c  Velocity[Z]                                      0.65992E-33 
c  Pressure     0.25611E-05     345   0.11045E-02   0.31876E-01 0.40096E-01 
c  k            0.15938E-07      70   0.15631E-02   0.10879E-09 0.13638E+00 
c  epsilon      0.20870E-06      45   0.52057E-04   0.41270E-09 0.12936E+00 
c  TempC        0.23983E+01      66   0.57509E-03   0.43990E-02 0.32813E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.03992        0.040332      1.6671e-05      1.2401e-07
v  Velocity[Y]          -0.032284        0.059604       0.0014999      0.00089085
v  Velocity[Z]        -1.6344e-15       2.141e-15     -1.3261e-17     -1.1565e-17
v  ǁVelocityǁ          0.00023046        0.060302        0.017895         0.01832
v  Pressure             -0.018908        0.027485     -0.00016383      3.8681e-18
v  k                   1.2357e-07      0.00033305      8.1547e-05       8.391e-05
v  epsilon             9.6708e-08       0.0014005      7.0553e-05      7.8451e-05
v  TempC                   26.458          29.961          28.612          28.575
v  Density                 1.1653          1.1792          1.1707          1.1708
v  TurbVisc            6.8135e-09      7.9579e-05      2.1035e-05      2.1667e-05
v  CourantNb             0.011249          5.8332          1.5229          1.5091
v  FourierNb              0.42131          10.032          1.9106          1.8248
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1792          1.1705          1.1705


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46031          13.733          3.4334          3.3339


 TIME FOR THE TIME STEP               60:        0.68026E-01

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


 INSTANT    0.305000000E+02   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.304402465E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24451E-01
   Friction velocity        uet   :  0.33210E-04 0.18313E-01
   Friction velocity        uk    :  0.56495E-03 0.18056E-01
   Dimensionless distance   yplus :  0.72767E-01 0.28617E+01
   Friction thermal sca.    tstar : -0.31725E+01-0.79449E-01
   Rough dim-less th. sca.  tplus :  0.54292E-01 0.21352E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        294
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20227E-05      83   0.39465E-01   0.65376E-05 0.17011E+00 
c  Velocity[X]                                      0.28605E-05 
c  Velocity[Y]                                      0.36771E-05 
c  Velocity[Z]                                      0.68450E-33 
c  Pressure     0.25646E-05     345   0.11015E-02   0.31795E-01 0.38081E-01 
c  k            0.15440E-07      68   0.14873E-02   0.10304E-09 0.13775E+00 
c  epsilon      0.20141E-06      44   0.48084E-04   0.40357E-09 0.13188E+00 
c  TempC        0.24006E+01      65   0.56009E-03   0.41896E-02 0.31982E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.039296        0.038916       1.236e-05      6.1407e-07
v  Velocity[Y]          -0.031913        0.058818       0.0015305      0.00089643
v  Velocity[Z]         -1.675e-15      2.2611e-15     -1.3585e-17     -1.1793e-17
v  ǁVelocityǁ          0.00016567        0.059394         0.01753        0.017978
v  Pressure             -0.019341        0.027769     -0.00015875     -1.4848e-18
v  k                   1.0124e-07      0.00033795      7.8206e-05      8.0427e-05
v  epsilon             7.8921e-08       0.0013728        6.76e-05      7.5207e-05
v  TempC                   26.513          29.962          28.648          28.611
v  Density                 1.1653           1.179          1.1705          1.1707
v  TurbVisc            5.6292e-09      7.6942e-05      2.0376e-05       2.097e-05
v  CourantNb              0.02619          5.6891          1.4847          1.4749
v  FourierNb              0.42126          9.6335          1.8792          1.7936
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653           1.179          1.1704          1.1703


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45439          13.017          3.3639          3.2685


 TIME FOR THE TIME STEP               61:        0.65696E-01

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


 INSTANT    0.310000000E+02   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.264697796E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24328E-01
   Friction velocity        uet   :  0.52320E-03 0.18274E-01
   Friction velocity        uk    :  0.63720E-03 0.17943E-01
   Dimensionless distance   yplus :  0.82145E-01 0.28437E+01
   Friction thermal sca.    tstar : -0.67475E+01-0.76143E-01
   Rough dim-less th. sca.  tplus :  0.61289E-01 0.21217E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        295
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19965E-05      81   0.40231E-01   0.62073E-05 0.16811E+00 
c  Velocity[X]                                      0.26362E-05 
c  Velocity[Y]                                      0.35712E-05 
c  Velocity[Z]                                      0.80356E-33 
c  Pressure     0.24712E-05     341   0.11098E-02   0.30505E-01 0.36085E-01 
c  k            0.14973E-07      67   0.14090E-02   0.97329E-10 0.13878E+00 
c  epsilon      0.19438E-06      43   0.45141E-04   0.39133E-09 0.13375E+00 
c  TempC        0.24028E+01      64   0.50989E-03   0.39960E-02 0.31196E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.036953        0.038152      7.5178e-06      4.1812e-07
v  Velocity[Y]           -0.03171        0.057619       0.0015601      0.00090222
v  Velocity[Z]        -1.7124e-15      2.3481e-15     -1.3966e-17     -1.1991e-17
v  ǁVelocityǁ          0.00024085        0.058279        0.017228        0.017703
v  Pressure             -0.019733        0.028045     -0.00015383     -5.3213e-18
v  k                   8.3809e-08      0.00034144      7.5105e-05      7.7204e-05
v  epsilon             6.4603e-08       0.0013457      6.4856e-05       7.221e-05
v  TempC                   26.576          29.963          28.684          28.646
v  Density                 1.1653          1.1787          1.1704          1.1706
v  TurbVisc             4.654e-09      7.4384e-05      1.9745e-05      2.0299e-05
v  CourantNb             0.027135          5.5165          1.4509          1.4456
v  FourierNb              0.42122          9.2521          1.8499          1.7642
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1787          1.1702          1.1702


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44839          12.272          3.3009          3.2098


 TIME FOR THE TIME STEP               62:        0.65831E-01

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


 INSTANT    0.315000000E+02   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.607481442E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24144E-01
   Friction velocity        uet   :  0.21122E-04 0.18025E-01
   Friction velocity        uk    :  0.42338E-03 0.17767E-01
   Dimensionless distance   yplus :  0.54534E-01 0.28157E+01
   Friction thermal sca.    tstar : -0.36984E+01-0.74039E-01
   Rough dim-less th. sca.  tplus :  0.40689E-01 0.21008E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        298
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19756E-05      80   0.41594E-01   0.57479E-05 0.16361E+00 
c  Velocity[X]                                      0.23984E-05 
c  Velocity[Y]                                      0.33495E-05 
c  Velocity[Z]                                      0.82171E-33 
c  Pressure     0.24380E-05     330   0.11143E-02   0.29955E-01 0.33901E-01 
c  k            0.14474E-07      67   0.13208E-02   0.94282E-10 0.14140E+00 
c  epsilon      0.18635E-06      43   0.42085E-04   0.97353E-09 0.21891E+00 
c  TempC        0.24050E+01      63   0.49475E-03   0.38516E-02 0.30592E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.036504        0.036185      6.3534e-06      1.6583e-06
v  Velocity[Y]          -0.031581        0.056734       0.0015891      0.00090859
v  Velocity[Z]        -1.7447e-15      2.3479e-15     -1.4264e-17      -1.216e-17
v  ǁVelocityǁ          0.00016995         0.05739        0.016965        0.017463
v  Pressure             -0.020106        0.028299      -0.0001493     -8.0732e-20
v  k                   7.0149e-08      0.00034262      7.2213e-05      7.4198e-05
v  epsilon             5.3081e-08       0.0013227      6.1846e-05      6.8874e-05
v  TempC                   26.638          29.964          28.718           28.68
v  Density                 1.1653          1.1785          1.1703          1.1704
v  TurbVisc            3.8965e-09       7.138e-05      1.9144e-05      1.9655e-05
v  CourantNb             0.022793          5.3055          1.4243          1.4235
v  FourierNb              0.42119          8.8949           1.822          1.7359
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1785          1.1701          1.1701


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44402          11.573          3.2462          3.1594


 TIME FOR THE TIME STEP               63:        0.65157E-01

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


 INSTANT    0.320000000E+02   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.599540508E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24004E-01
   Friction velocity        uet   :  0.39794E-03 0.17793E-01
   Friction velocity        uk    :  0.57411E-03 0.17634E-01
   Dimensionless distance   yplus :  0.90917E-01 0.27946E+01
   Friction thermal sca.    tstar : -0.46573E+01-0.75135E-01
   Rough dim-less th. sca.  tplus :  0.67834E-01 0.20851E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        299
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19587E-05      79   0.37029E-01   0.50662E-05 0.15488E+00 
c  Velocity[X]                                      0.20900E-05 
c  Velocity[Y]                                      0.29762E-05 
c  Velocity[Z]                                      0.78920E-33 
c  Pressure     0.23842E-05     326   0.11014E-02   0.29153E-01 0.32470E-01 
c  k            0.14057E-07      67   0.13455E-02   0.81688E-10 0.13597E+00 
c  epsilon      0.17960E-06      42   0.40799E-04   0.38571E-09 0.14204E+00 
c  TempC        0.24070E+01      63   0.46218E-03   0.37222E-02 0.30040E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.034876        0.035959      5.2081e-06      2.1351e-06
v  Velocity[Y]          -0.031448        0.056102       0.0016169      0.00091609
v  Velocity[Z]        -1.7791e-15      2.4435e-15     -1.4539e-17     -1.2323e-17
v  ǁVelocityǁ           0.0002494        0.056625        0.016743         0.01726
v  Pressure              -0.02045        0.028561     -0.00014528      2.2078e-18
v  k                    5.909e-08      0.00034159      6.9605e-05      7.1494e-05
v  epsilon             4.3846e-08       0.0013026      5.9355e-05      6.6154e-05
v  TempC                   26.701          29.965           28.75          28.713
v  Density                 1.1653          1.1783          1.1701          1.1703
v  TurbVisc            3.3017e-09      7.0061e-05      1.8579e-05      1.9046e-05
v  CourantNb             0.011406          5.4361          1.4006          1.4044
v  FourierNb              0.42116          8.5671          1.7967          1.7101
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1783            1.17          1.1699


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43732          11.074          3.1973          3.1145


 TIME FOR THE TIME STEP               64:        0.65957E-01

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


 INSTANT    0.325000000E+02   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.120437497E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.23894E-01
   Friction velocity        uet   :  0.32920E-03 0.17624E-01
   Friction velocity        uk    :  0.38208E-03 0.17536E-01
   Dimensionless distance   yplus :  0.60510E-01 0.27790E+01
   Friction thermal sca.    tstar : -0.36557E+01-0.78911E-01
   Rough dim-less th. sca.  tplus :  0.45147E-01 0.20734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        301
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19459E-05      78   0.37639E-01   0.43836E-05 0.14506E+00 
c  Velocity[X]                                      0.18271E-05 
c  Velocity[Y]                                      0.25565E-05 
c  Velocity[Z]                                      0.81190E-33 
c  Pressure     0.22587E-05     323   0.10513E-02   0.27479E-01 0.30517E-01 
c  k            0.13647E-07      68   0.13924E-02   0.74659E-10 0.13405E+00 
c  epsilon      0.17273E-06      42   0.41036E-04   0.67622E-09 0.19424E+00 
c  TempC        0.24090E+01      62   0.41431E-03   0.36023E-02 0.29520E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.034517         0.03421      3.8805e-06      2.0479e-06
v  Velocity[Y]          -0.031468        0.055287       0.0016423      0.00092289
v  Velocity[Z]        -1.8473e-15      2.5033e-15     -1.4755e-17     -1.2435e-17
v  ǁVelocityǁ          0.00017814        0.055826        0.016543        0.017071
v  Pressure             -0.020784        0.028815     -0.00014198     -4.2191e-18
v  k                   5.0002e-08      0.00033949      6.7246e-05      6.9028e-05
v  epsilon             3.6447e-08        0.001281      5.6906e-05      6.3455e-05
v  TempC                   26.769          29.965          28.782          28.744
v  Density                 1.1653           1.178            1.17          1.1702
v  TurbVisc             2.799e-09      6.8575e-05      1.8053e-05      1.8474e-05
v  CourantNb             0.011829          5.5064            1.38          1.3877
v  FourierNb              0.42114          8.2708          1.7738          1.6865
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653           1.178          1.1698          1.1698


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43312          11.519          3.1538          3.0741


 TIME FOR THE TIME STEP               65:        0.62846E-01

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


 INSTANT    0.330000000E+02   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.505572790E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.23746E-01
   Friction velocity        uet   :  0.75324E-04 0.17195E-01
   Friction velocity        uk    :  0.18123E-03 0.17422E-01
   Dimensionless distance   yplus :  0.28701E-01 0.27609E+01
   Friction thermal sca.    tstar : -0.31268E+01-0.78576E-01
   Rough dim-less th. sca.  tplus :  0.21414E-01 0.20600E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        305
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19319E-05      77   0.43309E-01   0.37943E-05 0.13596E+00 
c  Velocity[X]                                      0.16339E-05 
c  Velocity[Y]                                      0.21604E-05 
c  Velocity[Z]                                      0.89776E-33 
c  Pressure     0.22480E-05     321   0.98259E-03   0.27204E-01 0.28382E-01 
c  k            0.13189E-07      68   0.13405E-02   0.70950E-10 0.13458E+00 
c  epsilon      0.16464E-06      43   0.40868E-04   0.13094E-08 0.28183E+00 
c  TempC        0.24109E+01      63   0.39582E-03   0.34855E-02 0.29007E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.033339        0.033764      3.3141e-06      2.4051e-06
v  Velocity[Y]          -0.031728        0.054781       0.0016668      0.00093071
v  Velocity[Z]        -1.9049e-15      2.5533e-15     -1.4956e-17     -1.2531e-17
v  ǁVelocityǁ          0.00011377        0.054938        0.016341         0.01687
v  Pressure             -0.021095        0.029048     -0.00013946      3.0538e-19
v  k                   4.2615e-08       0.0003338      6.5101e-05      6.6749e-05
v  epsilon              3.052e-08       0.0012616      5.4164e-05       6.036e-05
v  TempC                   26.833          29.966          28.812          28.775
v  Density                 1.1653          1.1777          1.1699            1.17
v  TurbVisc            2.3909e-09      6.7099e-05      1.7578e-05      1.7946e-05
v  CourantNb            0.0052335          6.0718          1.3618          1.3722
v  FourierNb              0.42113          7.9979          1.7513          1.6624
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1777          1.1697          1.1697


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43389          11.866          3.1131          3.0346


 TIME FOR THE TIME STEP               66:        0.63032E-01

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


 INSTANT    0.335000000E+02   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.120437497E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.23604E-01
   Friction velocity        uet   :  0.18873E-03 0.16872E-01
   Friction velocity        uk    :  0.24961E-03 0.17283E-01
   Dimensionless distance   yplus :  0.39529E-01 0.27388E+01
   Friction thermal sca.    tstar : -0.27794E+01-0.81110E-01
   Rough dim-less th. sca.  tplus :  0.29493E-01 0.20435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        307
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19153E-05      77   0.36131E-01   0.32151E-05 0.12615E+00 
c  Velocity[X]                                      0.14216E-05 
c  Velocity[Y]                                      0.17936E-05 
c  Velocity[Z]                                      0.91292E-33 
c  Pressure     0.21707E-05     322   0.89890E-03   0.26132E-01 0.27144E-01 
c  k            0.12807E-07      68   0.12150E-02   0.58911E-10 0.12607E+00 
c  epsilon      0.15808E-06      44   0.38663E-04   0.69887E-09 0.21292E+00 
c  TempC        0.24128E+01      63   0.43310E-03   0.33692E-02 0.28490E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.032835        0.032996      2.6887e-06      2.6298e-06
v  Velocity[Y]          -0.032044        0.056203       0.0016875      0.00093748
v  Velocity[Z]        -2.0166e-15      2.6034e-15     -1.5108e-17     -1.2579e-17
v  ǁVelocityǁ          8.1139e-05        0.056221        0.016152        0.016675
v  Pressure             -0.021409        0.029283      -0.0001378     -1.5304e-18
v  k                   3.6564e-08      0.00032689       6.322e-05       6.472e-05
v  epsilon              2.576e-08       0.0012407       5.194e-05      5.7862e-05
v  TempC                   26.901          29.967          28.841          28.805
v  Density                 1.1653          1.1775          1.1698          1.1699
v  TurbVisc            2.0562e-09      6.6199e-05      1.7152e-05      1.7461e-05
v  CourantNb            0.0097101          6.6289          1.3442          1.3563
v  FourierNb              0.42111          7.7237          1.7338          1.6432
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1775          1.1696          1.1696


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4322          12.152          3.0779          2.9995


 TIME FOR THE TIME STEP               67:        0.63219E-01

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


 INSTANT    0.340000000E+02   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.250139417E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.23454E-01
   Friction velocity        uet   :  0.24409E-03 0.16980E-01
   Friction velocity        uk    :  0.35222E-03 0.17158E-01
   Dimensionless distance   yplus :  0.55779E-01 0.27189E+01
   Friction thermal sca.    tstar : -0.27237E+01-0.79560E-01
   Rough dim-less th. sca.  tplus :  0.41617E-01 0.20286E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        317
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18978E-05      77   0.37180E-01   0.31627E-05 0.12659E+00 
c  Velocity[X]                                      0.13749E-05 
c  Velocity[Y]                                      0.17877E-05 
c  Velocity[Z]                                      0.80923E-33 
c  Pressure     0.21712E-05     322   0.82797E-03   0.26004E-01 0.22424E-01 
c  k            0.12233E-07      68   0.11520E-02   0.72359E-10 0.14369E+00 
c  epsilon      0.14743E-06      45   0.40944E-04   0.32608E-08 0.49067E+00 
c  TempC        0.24146E+01      62   0.37652E-03   0.32534E-02 0.27969E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.031611        0.031873      1.0093e-07       2.315e-06
v  Velocity[Y]          -0.032364        0.056378       0.0017139      0.00094692
v  Velocity[Z]        -2.1251e-15      2.6566e-15     -1.5193e-17     -1.2467e-17
v  ǁVelocityǁ          6.5091e-05        0.056385        0.015983        0.016485
v  Pressure             -0.021688        0.029487     -0.00013693     -2.7519e-18
v  k                   3.1584e-08       0.0003176      6.1386e-05      6.2692e-05
v  epsilon             2.1973e-08       0.0012179      4.8331e-05      5.3632e-05
v  TempC                   26.973          29.967          28.869          28.833
v  Density                 1.1653          1.1772          1.1697          1.1698
v  TurbVisc             1.779e-09      6.4806e-05      1.6771e-05      1.7015e-05
v  CourantNb            0.0099016           7.012          1.3285          1.3418
v  FourierNb               0.4211          7.4457          1.7192          1.6266
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1772          1.1695          1.1695


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43129          12.336          3.0476          2.9685


 TIME FOR THE TIME STEP               68:        0.64054E-01

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


 INSTANT    0.345000000E+02   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384        -0.115143541E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.23286E-01
   Friction velocity        uet   :  0.39547E-03 0.16836E-01
   Friction velocity        uk    :  0.41467E-03 0.17025E-01
   Dimensionless distance   yplus :  0.53494E-01 0.26978E+01
   Friction thermal sca.    tstar : -0.38465E+01-0.76537E-01
   Rough dim-less th. sca.  tplus :  0.39912E-01 0.20129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        329
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18722E-05      76   0.34393E-01   0.32307E-05 0.12994E+00 
c  Velocity[X]                                      0.13441E-05 
c  Velocity[Y]                                      0.18865E-05 
c  Velocity[Z]                                      0.77513E-33 
c  Pressure     0.21763E-05     324   0.77881E-03   0.25931E-01 0.21348E-01 
c  k            0.11590E-07      69   0.11449E-02   0.72283E-10 0.14768E+00 
c  epsilon      0.13533E-06      46   0.46532E-04   0.40115E-08 0.58899E+00 
c  TempC        0.24164E+01      62   0.36091E-03   0.31224E-02 0.27374E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.031653        0.031897     -5.4244e-09      2.3477e-06
v  Velocity[Y]          -0.032615        0.055985       0.0017419      0.00095618
v  Velocity[Z]        -2.1542e-15      2.7138e-15     -1.5492e-17     -1.2619e-17
v  ǁVelocityǁ          0.00014765        0.055989        0.015817        0.016284
v  Pressure             -0.021968        0.029683     -0.00013685      4.0366e-18
v  k                   2.7497e-08      0.00030787      5.9647e-05      6.0738e-05
v  epsilon             1.8976e-08       0.0011928      4.4206e-05      4.8741e-05
v  TempC                   27.051          29.968          28.895           28.86
v  Density                 1.1653          1.1769          1.1695          1.1697
v  TurbVisc            1.5496e-09      6.4549e-05      1.6433e-05      1.6612e-05
v  CourantNb            0.0038955          7.2688          1.3161          1.3295
v  FourierNb              0.42109          7.1673          1.7053          1.6104
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1769          1.1694          1.1694


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43189          12.445          3.0214          2.9399


 TIME FOR THE TIME STEP               69:        0.63600E-01

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


 INSTANT    0.350000000E+02   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.174700545E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.23094E-01
   Friction velocity        uet   :  0.31275E-03 0.16929E-01
   Friction velocity        uk    :  0.32232E-03 0.16861E-01
   Dimensionless distance   yplus :  0.41511E-01 0.26717E+01
   Friction thermal sca.    tstar : -0.86583E+01-0.74822E-01
   Rough dim-less th. sca.  tplus :  0.30972E-01 0.19934E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        334
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18408E-05      76   0.37191E-01   0.27937E-05 0.12288E+00 
c  Velocity[X]                                      0.11811E-05 
c  Velocity[Y]                                      0.16126E-05 
c  Velocity[Z]                                      0.72646E-33 
c  Pressure     0.20758E-05     335   0.74482E-03   0.24605E-01 0.23486E-01 
c  k            0.11133E-07      69   0.11227E-02   0.48209E-10 0.12379E+00 
c  epsilon      0.12729E-06      47   0.46239E-04   0.16814E-08 0.40264E+00 
c  TempC        0.24181E+01      62   0.40506E-03   0.29676E-02 0.26663E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.03075        0.031437      3.9908e-07       2.207e-06
v  Velocity[Y]          -0.032513        0.055372       0.0017641      0.00096494
v  Velocity[Z]         -2.231e-15      2.7742e-15     -1.5861e-17     -1.2776e-17
v  ǁVelocityǁ          0.00010924        0.055373         0.01566        0.016087
v  Pressure             -0.022296        0.029894     -0.00013752     -2.9485e-18
v  k                   2.4187e-08      0.00029666      5.8184e-05      5.9093e-05
v  epsilon             1.6631e-08        0.001167      4.1513e-05      4.5581e-05
v  TempC                   27.126          29.969          28.921          28.887
v  Density                 1.1653          1.1766          1.1694          1.1696
v  TurbVisc            1.3623e-09      6.3859e-05       1.614e-05      1.6259e-05
v  CourantNb            0.0077345          7.4296          1.3047          1.3167
v  FourierNb              0.42108          6.9016          1.6928          1.5954
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1766          1.1693          1.1693


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42902          12.493          2.9976          2.9122


 TIME FOR THE TIME STEP               70:        0.64930E-01

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


 INSTANT    0.355000000E+02   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.979381845E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.22901E-01
   Friction velocity        uet   :  0.30793E-04 0.17009E-01
   Friction velocity        uk    :  0.10433E-03 0.16714E-01
   Dimensionless distance   yplus :  0.16521E-01 0.26484E+01
   Friction thermal sca.    tstar : -0.64031E+01-0.74958E-01
   Rough dim-less th. sca.  tplus :  0.12326E-01 0.19760E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        338
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18059E-05      75   0.37559E-01   0.25380E-05 0.11935E+00 
c  Velocity[X]                                      0.10840E-05 
c  Velocity[Y]                                      0.14540E-05 
c  Velocity[Z]                                      0.69700E-33 
c  Pressure     0.20616E-05     341   0.69888E-03   0.24323E-01 0.23050E-01 
c  k            0.10706E-07      69   0.10804E-02   0.40439E-10 0.11622E+00 
c  epsilon      0.11964E-06      47   0.42559E-04   0.12946E-08 0.37328E+00 
c  TempC        0.24198E+01      61   0.40117E-03   0.27806E-02 0.25786E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.029963        0.030082      4.3351e-07      1.9818e-06
v  Velocity[Y]          -0.032453        0.054859       0.0017812      0.00097266
v  Velocity[Z]        -2.3117e-15      2.8375e-15      -1.629e-17     -1.2993e-17
v  ǁVelocityǁ          0.00019794        0.054859        0.015487        0.015869
v  Pressure             -0.022627        0.030099     -0.00013858      5.3564e-18
v  k                   2.1549e-08      0.00028474      5.6906e-05      5.7653e-05
v  epsilon             1.4817e-08       0.0011373      3.9286e-05      4.2973e-05
v  TempC                   27.203          29.969          28.945          28.912
v  Density                 1.1653          1.1763          1.1693          1.1695
v  TurbVisc            1.2128e-09      6.2989e-05       1.589e-05      1.5956e-05
v  CourantNb             0.005934          7.4614          1.2946          1.3044
v  FourierNb              0.42108          6.9843          1.6836          1.5843
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1763          1.1692          1.1692


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42721          12.431          2.9782          2.8887


 TIME FOR THE TIME STEP               71:        0.65907E-01

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


 INSTANT    0.360000000E+02   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.661744490E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.22628E-01
   Friction velocity        uet   :  0.34805E-03 0.16959E-01
   Friction velocity        uk    :  0.36153E-03 0.16493E-01
   Dimensionless distance   yplus :  0.46588E-01 0.26133E+01
   Friction thermal sca.    tstar : -0.82537E+01-0.74038E-01
   Rough dim-less th. sca.  tplus :  0.34760E-01 0.19498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        341
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17708E-05      73   0.36084E-01   0.23737E-05 0.11780E+00 
c  Velocity[X]                                      0.97105E-06 
c  Velocity[Y]                                      0.14027E-05 
c  Velocity[Z]                                      0.72740E-33 
c  Pressure     0.19701E-05     341   0.64903E-03   0.23151E-01 0.21989E-01 
c  k            0.10317E-07      69   0.10298E-02   0.34437E-10 0.10977E+00 
c  epsilon      0.11259E-06      48   0.40362E-04   0.99839E-09 0.34551E+00 
c  TempC        0.24214E+01      60   0.35072E-03   0.25730E-02 0.24785E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.030135        0.030072      1.0835e-06       1.842e-06
v  Velocity[Y]          -0.032056        0.053031       0.0017935      0.00097946
v  Velocity[Z]        -2.3722e-15       2.902e-15     -1.6809e-17     -1.3295e-17
v  ǁVelocityǁ          0.00017246        0.053031        0.015293        0.015628
v  Pressure             -0.022962        0.030306     -0.00013994     -1.1864e-18
v  k                   1.9514e-08      0.00027282      5.5772e-05      5.6378e-05
v  epsilon             1.3449e-08       0.0011075      3.7378e-05      4.0739e-05
v  TempC                   27.281           29.97          28.969          28.937
v  Density                 1.1653           1.176          1.1693          1.1694
v  TurbVisc            1.0973e-09      6.2478e-05      1.5679e-05      1.5702e-05
v  CourantNb            0.0037889          7.3779          1.2826          1.2895
v  FourierNb              0.42108          6.9764           1.675          1.5739
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653           1.176          1.1691          1.1691


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42506          12.343          2.9576          2.8634


 TIME FOR THE TIME STEP               72:        0.69504E-01

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


 INSTANT    0.365000000E+02   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.358665514E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.22398E-01
   Friction velocity        uet   :  0.38720E-03 0.16967E-01
   Friction velocity        uk    :  0.38670E-03 0.16328E-01
   Dimensionless distance   yplus :  0.61234E-01 0.25872E+01
   Friction thermal sca.    tstar : -0.35648E+01-0.71738E-01
   Rough dim-less th. sca.  tplus :  0.45688E-01 0.19303E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        345
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17337E-05      72   0.40639E-01   0.23471E-05 0.11983E+00 
c  Velocity[X]                                      0.92624E-06 
c  Velocity[Y]                                      0.14209E-05 
c  Velocity[Z]                                      0.68390E-33 
c  Pressure     0.19243E-05     340   0.61467E-03   0.22538E-01 0.20703E-01 
c  k            0.98958E-08      69   0.98658E-03   0.32857E-10 0.10963E+00 
c  epsilon      0.10437E-06      48   0.40583E-04   0.12796E-08 0.41782E+00 
c  TempC        0.24230E+01      59   0.34766E-03   0.23533E-02 0.23683E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.029729        0.029565       1.866e-06       1.565e-06
v  Velocity[Y]          -0.031114        0.051736       0.0018033      0.00098639
v  Velocity[Z]        -2.3864e-15      2.9655e-15     -1.7331e-17     -1.3619e-17
v  ǁVelocityǁ          0.00010826        0.051739        0.015068        0.015354
v  Pressure              -0.02329        0.030504     -0.00014146       3.289e-18
v  k                    1.803e-08      0.00026335      5.4716e-05      5.5192e-05
v  epsilon             1.2459e-08       0.0010782      3.5363e-05      3.8363e-05
v  TempC                   27.362          29.971          28.991          28.961
v  Density                 1.1653          1.1757          1.1692          1.1693
v  TurbVisc            1.0135e-09      6.1751e-05      1.5501e-05      1.5492e-05
v  CourantNb            0.0016915          7.2093          1.2685          1.2721
v  FourierNb              0.42108          6.9248          1.6676          1.5652
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1757           1.169           1.169


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42297          12.234          2.9361          2.8373


 TIME FOR THE TIME STEP               73:        0.71393E-01

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


 INSTANT    0.370000000E+02   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.247492439E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.22038E-01
   Friction velocity        uet   :  0.29451E-03 0.16899E-01
   Friction velocity        uk    :  0.39607E-03 0.16055E-01
   Dimensionless distance   yplus :  0.51006E-01 0.25440E+01
   Friction thermal sca.    tstar : -0.27775E+01-0.69483E-01
   Rough dim-less th. sca.  tplus :  0.38056E-01 0.18981E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        348
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16948E-05      73   0.35799E-01   0.23154E-05 0.12192E+00 
c  Velocity[X]                                      0.88440E-06 
c  Velocity[Y]                                      0.14310E-05 
c  Velocity[Z]                                      0.67583E-33 
c  Pressure     0.18323E-05     340   0.58516E-03   0.21396E-01 0.20062E-01 
c  k            0.95203E-08      69   0.94861E-03   0.27149E-10 0.10173E+00 
c  epsilon      0.96870E-07      48   0.41112E-04   0.98236E-09 0.38994E+00 
c  TempC        0.24245E+01      59   0.37473E-03   0.21458E-02 0.22597E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.029477        0.028791      3.5134e-06       1.335e-06
v  Velocity[Y]          -0.030118        0.050066       0.0018085       0.0009919
v  Velocity[Z]        -2.3775e-15      3.0277e-15     -1.7912e-17     -1.3939e-17
v  ǁVelocityǁ          0.00029235         0.05007        0.014818        0.015053
v  Pressure             -0.023617        0.030706     -0.00014299      3.3627e-18
v  k                   1.7057e-08         0.00026      5.3747e-05      5.4116e-05
v  epsilon             1.1798e-08       0.0010512      3.3583e-05      3.6267e-05
v  TempC                   27.441          29.973          29.013          28.984
v  Density                 1.1653          1.1754          1.1691          1.1692
v  TurbVisc            9.5978e-10      6.0839e-05      1.5349e-05      1.5317e-05
v  CourantNb            0.0009289           7.029          1.2523          1.2522
v  FourierNb              0.42108          6.8723          1.6614          1.5582
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1754          1.1689          1.1689


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42221          12.026          2.9137          2.8104


 TIME FOR THE TIME STEP               74:        0.65568E-01

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


 INSTANT    0.375000000E+02   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.410281584E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.21697E-01
   Friction velocity        uet   :  0.22937E-03 0.16953E-01
   Friction velocity        uk    :  0.45894E-03 0.15811E-01
   Dimensionless distance   yplus :  0.72672E-01 0.25051E+01
   Friction thermal sca.    tstar : -0.42814E+01-0.68182E-01
   Rough dim-less th. sca.  tplus :  0.54221E-01 0.18691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        354
   Total number of wall faces                   :        384
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         75, Physical time    0.37500E+02


   ** 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


 Time for restart files:    0.13638E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16569E-05      74   0.38235E-01   0.24446E-05 0.12862E+00 
c  Velocity[X]                                      0.88082E-06 
c  Velocity[Y]                                      0.15638E-05 
c  Velocity[Z]                                      0.67727E-33 
c  Pressure     0.17859E-05     340   0.56016E-03   0.20803E-01 0.18680E-01 
c  k            0.90431E-08      68   0.91831E-03   0.32032E-10 0.11273E+00 
c  epsilon      0.86252E-07      47   0.43310E-04   0.20120E-08 0.61685E+00 
c  TempC        0.24259E+01      58   0.36896E-03   0.19300E-02 0.21414E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.028898        0.028269      5.1496e-06      1.0176e-06
v  Velocity[Y]           -0.02872        0.048182        0.001813      0.00099816
v  Velocity[Z]        -2.3767e-15      3.0714e-15     -1.8268e-17     -1.4102e-17
v  ǁVelocityǁ          0.00025729        0.048182        0.014537         0.01472
v  Pressure             -0.023933        0.030898     -0.00014437     -2.6501e-18
v  k                   1.6569e-08       0.0002563      5.2775e-05      5.3042e-05
v  epsilon              1.143e-08       0.0010234      3.1275e-05      3.3521e-05
v  TempC                   27.517          29.974          29.035          29.006
v  Density                 1.1653          1.1751           1.169          1.1691
v  TurbVisc            9.3525e-10       6.063e-05      1.5217e-05      1.5172e-05
v  CourantNb            0.0025907          6.8212          1.2332          1.2292
v  FourierNb              0.42108          6.8023          1.6563          1.5527
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1751          1.1689          1.1688


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42388          11.738          2.8894          2.7819


 TIME FOR THE TIME STEP               75:        0.20567E+00

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


 INSTANT    0.380000000E+02   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.449986253E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.21301E-01
   Friction velocity        uet   :  0.27274E-03 0.16872E-01
   Friction velocity        uk    :  0.27464E-03 0.15536E-01
   Dimensionless distance   yplus :  0.43488E-01 0.24617E+01
   Friction thermal sca.    tstar : -0.47854E+01-0.66420E-01
   Rough dim-less th. sca.  tplus :  0.32447E-01 0.18367E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        359
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16171E-05      75   0.35432E-01   0.25133E-05 0.13402E+00 
c  Velocity[X]                                      0.87775E-06 
c  Velocity[Y]                                      0.16355E-05 
c  Velocity[Z]                                      0.57333E-33 
c  Pressure     0.17002E-05     339   0.53409E-03   0.19762E-01 0.18486E-01 
c  k            0.86013E-08      67   0.89700E-03   0.27959E-10 0.10731E+00 
c  epsilon      0.75844E-07      47   0.46475E-04   0.18051E-08 0.65071E+00 
c  TempC        0.24274E+01      57   0.32744E-03   0.17381E-02 0.20307E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.028118        0.027244       7.996e-06      1.6264e-06
v  Velocity[Y]          -0.027313        0.046085        0.001814       0.0010043
v  Velocity[Z]        -2.3777e-15      3.1046e-15     -1.8556e-17      -1.414e-17
v  ǁVelocityǁ          0.00016052        0.046085        0.014238        0.014372
v  Pressure             -0.024248        0.031094     -0.00014557      -5.725e-18
v  k                   1.6548e-08      0.00025273      5.1853e-05      5.2039e-05
v  epsilon             1.1328e-08      0.00099098      2.9132e-05      3.0974e-05
v  TempC                   27.591          29.975          29.055          29.028
v  Density                 1.1653          1.1748          1.1689           1.169
v  TurbVisc            9.3963e-10      6.0164e-05      1.5101e-05       1.505e-05
v  CourantNb           0.00095654          6.5836          1.2112          1.2032
v  FourierNb              0.42108          6.7329          1.6501          1.5462
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1748          1.1688          1.1688


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42213          11.438          2.8613          2.7494


 TIME FOR THE TIME STEP               76:        0.64357E-01

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


 INSTANT    0.385000000E+02   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.254109884E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.20872E-01
   Friction velocity        uet   :  0.30234E-03 0.17012E-01
   Friction velocity        uk    :  0.31765E-03 0.15233E-01
   Dimensionless distance   yplus :  0.40927E-01 0.24135E+01
   Friction thermal sca.    tstar : -0.77607E+01-0.64287E-01
   Rough dim-less th. sca.  tplus :  0.30536E-01 0.18007E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        371
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15785E-05      75   0.34732E-01   0.29273E-05 0.14914E+00 
c  Velocity[X]                                      0.94284E-06 
c  Velocity[Y]                                      0.19845E-05 
c  Velocity[Z]                                      0.63370E-33 
c  Pressure     0.16677E-05     336   0.48876E-03   0.19351E-01 0.17057E-01 
c  k            0.78459E-08      66   0.91226E-03   0.46482E-10 0.14108E+00 
c  epsilon      0.53636E-07      47   0.62384E-04   0.43483E-08 0.13354E+01 
c  TempC        0.24288E+01      56   0.28393E-03   0.15679E-02 0.19273E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.027736        0.026383      1.1408e-05      2.0135e-06
v  Velocity[Y]          -0.026188        0.043397       0.0018156       0.0010116
v  Velocity[Z]        -2.3776e-15      3.1299e-15     -1.8556e-17     -1.3984e-17
v  ǁVelocityǁ          0.00015516        0.043397         0.01391        0.013989
v  Pressure             -0.024548        0.031268     -0.00014641     -4.5631e-19
v  k                   1.6981e-08      0.00024941      5.0829e-05      5.0923e-05
v  epsilon             1.1471e-08      0.00095786      2.5677e-05      2.6817e-05
v  TempC                   27.655          29.977          29.075          29.049
v  Density                 1.1653          1.1745          1.1688          1.1689
v  TurbVisc            9.6863e-10       5.983e-05      1.4995e-05      1.4946e-05
v  CourantNb           0.00089972           6.281          1.1873          1.1752
v  FourierNb              0.42108          6.6745          1.6436          1.5398
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1745          1.1687          1.1687


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42251           11.09          2.8309          2.7151


 TIME FOR THE TIME STEP               77:        0.65088E-01

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


 INSTANT    0.390000000E+02   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384        -0.423516474E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24270E-03 0.16820E-01
   Friction velocity        uk    :  0.24245E-03 0.14885E-01
   Dimensionless distance   yplus :  0.38391E-01 0.23581E+01
   Friction thermal sca.    tstar : -0.29459E+01-0.62819E-01
   Rough dim-less th. sca.  tplus :  0.28644E-01 0.17594E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15380E-05      76   0.27707E-01   0.32592E-05 0.16250E+00 
c  Velocity[X]                                      0.10009E-05 
c  Velocity[Y]                                      0.22584E-05 
c  Velocity[Z]                                      0.77089E-33 
c  Pressure     0.15616E-05     331   0.45991E-03   0.18099E-01 0.17261E-01 
c  k            0.70061E-08      66   0.95979E-03   0.51053E-10 0.15069E+00 
c  epsilon      0.10645E-07      52   0.30106E-03   0.48790E-08 0.27047E+01 
c  TempC        0.24301E+01      56   0.28468E-03   0.14134E-02 0.18286E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.026952        0.025442      1.3078e-05       1.261e-06
v  Velocity[Y]          -0.025202        0.041313       0.0018142       0.0010185
v  Velocity[Z]        -2.3753e-15       3.146e-15     -1.8138e-17     -1.3303e-17
v  ǁVelocityǁ          0.00020866        0.041314        0.013563        0.013588
v  Pressure             -0.024849        0.031443     -0.00014691     -5.7776e-18
v  k                   1.6899e-08      0.00024437      4.9783e-05      4.9794e-05
v  epsilon             1.1538e-08      0.00023651      2.1942e-05      2.2317e-05
v  TempC                   27.715          29.978          29.095           29.07
v  Density                 1.1653          1.1743          1.1687          1.1688
v  TurbVisc            9.6591e-10      5.9595e-05      1.4896e-05      1.4855e-05
v  CourantNb            0.0032103          5.9236          1.1606          1.1445
v  FourierNb              0.42109          6.6331          1.6388          1.5359
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1743          1.1686          1.1686


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42479          10.707          2.7995          2.6804


 TIME FOR THE TIME STEP               78:        0.64074E-01

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


 INSTANT    0.395000000E+02   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15618E-03 0.14332E-01
   Friction velocity        uk    :  0.15690E-03 0.13626E-01
   Dimensionless distance   yplus :  0.24845E-01 0.21299E+01
   Friction thermal sca.    tstar : -0.30473E+01-0.62169E-01
   Rough dim-less th. sca.  tplus :  0.18537E-01 0.15891E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14983E-05      75   0.27409E-01   0.25505E-05 0.14755E+00 
c  Velocity[X]                                      0.88327E-06 
c  Velocity[Y]                                      0.16672E-05 
c  Velocity[Z]                                      0.61605E-33 
c  Pressure     0.13938E-05     329   0.43024E-03   0.16135E-01 0.19144E-01 
c  k            0.68499E-08      64   0.92670E-03   0.10791E-10 0.70302E-01 
c  epsilon      0.54724E-08      54   0.54244E-03   0.13862E-09 0.48628E+00 
c  TempC        0.24314E+01      55   0.27313E-03   0.12888E-02 0.17450E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.025906        0.024422      1.5305e-05      1.2771e-06
v  Velocity[Y]           -0.02432        0.039149       0.0018018       0.0010225
v  Velocity[Z]        -2.3729e-15      3.1559e-15     -1.7948e-17      -1.288e-17
v  ǁVelocityǁ           7.172e-05        0.039149        0.013253        0.013239
v  Pressure             -0.025156        0.031648     -0.00014703     -4.2402e-18
v  k                    1.714e-08       0.0002402      4.9001e-05      4.9001e-05
v  epsilon             1.1535e-08      0.00023112      2.0866e-05      2.1079e-05
v  TempC                   27.771          29.979          29.114           29.09
v  Density                 1.1653           1.174          1.1687          1.1688
v  TurbVisc            9.8801e-10      5.9367e-05      1.4802e-05      1.4776e-05
v  CourantNb            0.0064147           5.551          1.1308          1.1106
v  FourierNb               0.4211          6.6136          1.6324          1.5303
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653           1.174          1.1685          1.1685


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4279          10.325          2.7632          2.6409


 TIME FOR THE TIME STEP               79:        0.63258E-01

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


 INSTANT    0.400000000E+02   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23252E-03 0.14199E-01
   Friction velocity        uk    :  0.23198E-03 0.13622E-01
   Dimensionless distance   yplus :  0.36734E-01 0.19606E+01
   Friction thermal sca.    tstar : -0.20212E+01-0.61687E-01
   Rough dim-less th. sca.  tplus :  0.27408E-01 0.14628E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14679E-05      75   0.26435E-01   0.22805E-05 0.14249E+00 
c  Velocity[X]                                      0.82165E-06 
c  Velocity[Y]                                      0.14588E-05 
c  Velocity[Z]                                      0.65868E-33 
c  Pressure     0.12652E-05     328   0.39197E-03   0.14628E-01 0.18341E-01 
c  k            0.67446E-08      63   0.91388E-03   0.79941E-11 0.61334E-01 
c  epsilon      0.51396E-08      53   0.53558E-03   0.90961E-11 0.12733E+00 
c  TempC        0.24327E+01      55   0.24919E-03   0.11947E-02 0.16789E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.024869        0.023423      1.7957e-05      8.7635e-07
v  Velocity[Y]          -0.023875        0.037384       0.0017843       0.0010259
v  Velocity[Z]        -2.3709e-15       3.162e-15     -1.7757e-17     -1.2574e-17
v  ǁVelocityǁ          9.3526e-05          0.0385        0.012994        0.012952
v  Pressure             -0.025451        0.031844     -0.00014667      2.5202e-18
v  k                   1.7748e-08      0.00023646      4.8294e-05      4.8313e-05
v  epsilon             1.1723e-08      0.00022566      2.0276e-05      2.0438e-05
v  TempC                   27.807           29.98          29.133          29.109
v  Density                 1.1653          1.1738          1.1686          1.1687
v  TurbVisc            1.0341e-09      5.9313e-05      1.4711e-05      1.4705e-05
v  CourantNb            0.0070011          5.1482          1.1033          1.0802
v  FourierNb              0.42111          6.6126          1.6269           1.526
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1738          1.1685          1.1684


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42819          9.9334          2.7302          2.6063


 TIME FOR THE TIME STEP               80:        0.65465E-01

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


 INSTANT    0.405000000E+02   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16923E-03 0.14147E-01
   Friction velocity        uk    :  0.22128E-03 0.13582E-01
   Dimensionless distance   yplus :  0.30985E-01 0.19141E+01
   Friction thermal sca.    tstar : -0.37758E+01-0.60062E-01
   Rough dim-less th. sca.  tplus :  0.23118E-01 0.14281E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14452E-05      74   0.27806E-01   0.21241E-05 0.13978E+00 
c  Velocity[X]                                      0.76227E-06 
c  Velocity[Y]                                      0.13619E-05 
c  Velocity[Z]                                      0.60816E-33 
c  Pressure     0.11887E-05     324   0.36891E-03   0.13727E-01 0.17950E-01 
c  k            0.66521E-08      62   0.96138E-03   0.74368E-11 0.59925E-01 
c  epsilon      0.50505E-08      52   0.51782E-03   0.27582E-11 0.71363E-01 
c  TempC        0.24339E+01      55   0.21600E-03   0.11265E-02 0.16292E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.023821        0.022514      2.0708e-05      5.5288e-07
v  Velocity[Y]          -0.023728        0.037215       0.0017646       0.0010292
v  Velocity[Z]        -2.3691e-15      3.1658e-15     -1.7675e-17     -1.2345e-17
v  ǁVelocityǁ          9.6374e-05        0.038513        0.012799        0.012738
v  Pressure             -0.025738        0.032033     -0.00014588      3.1591e-19
v  k                   1.8706e-08      0.00023293      4.7615e-05      4.7671e-05
v  epsilon             1.2088e-08       0.0002207      1.9817e-05      1.9958e-05
v  TempC                   27.834           29.98          29.151          29.128
v  Density                 1.1653          1.1737          1.1685          1.1686
v  TurbVisc            1.1033e-09      5.9487e-05      1.4621e-05       1.464e-05
v  CourantNb             0.005356          4.7452          1.0793          1.0539
v  FourierNb              0.42111          6.6237           1.621          1.5218
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1737          1.1684          1.1684


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4296          9.5649          2.7003          2.5757


 TIME FOR THE TIME STEP               81:        0.70876E-01

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


 INSTANT    0.410000000E+02   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18678E-03 0.14127E-01
   Friction velocity        uk    :  0.18685E-03 0.13559E-01
   Dimensionless distance   yplus :  0.24061E-01 0.18937E+01
   Friction thermal sca.    tstar : -0.44698E+01-0.58365E-01
   Rough dim-less th. sca.  tplus :  0.17952E-01 0.14129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14281E-05      74   0.25209E-01   0.20106E-05 0.13761E+00 
c  Velocity[X]                                      0.69994E-06 
c  Velocity[Y]                                      0.13107E-05 
c  Velocity[Z]                                      0.63550E-33 
c  Pressure     0.11565E-05     323   0.35652E-03   0.13340E-01 0.17785E-01 
c  k            0.65692E-08      61   0.10370E-02   0.74400E-11 0.60686E-01 
c  epsilon      0.49863E-08      51   0.50338E-03   0.19800E-11 0.61417E-01 
c  TempC        0.24351E+01      54   0.24452E-03   0.10890E-02 0.16009E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.022459        0.021726      2.4006e-05      4.5486e-07
v  Velocity[Y]          -0.023809        0.036863       0.0017436        0.001032
v  Velocity[Z]        -2.3662e-15      3.1681e-15      -1.765e-17     -1.2215e-17
v  ǁVelocityǁ          9.4775e-05        0.038227        0.012669        0.012596
v  Pressure             -0.026021        0.032217     -0.00014466      2.6255e-18
v  k                   1.9996e-08      0.00022962      4.6952e-05       4.706e-05
v  epsilon             1.2624e-08      0.00021629      1.9416e-05       1.955e-05
v  TempC                   27.858          29.981          29.168          29.146
v  Density                 1.1653          1.1736          1.1685          1.1685
v  TurbVisc            1.1946e-09      5.9801e-05      1.4526e-05      1.4574e-05
v  CourantNb            0.0078818          4.3451          1.0608          1.0337
v  FourierNb              0.42112           6.635          1.6148          1.5174
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1653          1.1736          1.1683          1.1683


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42909          9.2166          2.6756           2.551


 TIME FOR THE TIME STEP               82:        0.70109E-01

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


 INSTANT    0.415000000E+02   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37698E-03 0.14123E-01
   Friction velocity        uk    :  0.37596E-03 0.13554E-01
   Dimensionless distance   yplus :  0.59531E-01 0.18763E+01
   Friction thermal sca.    tstar : -0.19696E+01-0.56969E-01
   Rough dim-less th. sca.  tplus :  0.44417E-01 0.13999E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14167E-05      73   0.23850E-01   0.18727E-05 0.13381E+00 
c  Velocity[X]                                      0.62946E-06 
c  Velocity[Y]                                      0.12433E-05 
c  Velocity[Z]                                      0.65941E-33 
c  Pressure     0.10863E-05     322   0.34861E-03   0.12517E-01 0.17748E-01 
c  k            0.64947E-08      62   0.11476E-02   0.78450E-11 0.63067E-01 
c  epsilon      0.49344E-08      51   0.50321E-03   0.16787E-11 0.57340E-01 
c  TempC        0.24362E+01      55   0.25099E-03   0.10795E-02 0.15930E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.021512        0.022798      2.7117e-05      1.2546e-07
v  Velocity[Y]          -0.024225        0.036536       0.0017228       0.0010346
v  Velocity[Z]        -2.3637e-15      3.1689e-15     -1.7628e-17     -1.2126e-17
v  ǁVelocityǁ          0.00015645        0.038004        0.012601        0.012523
v  Pressure             -0.026298        0.032396     -0.00014306      2.2465e-19
v  k                   2.1286e-08      0.00022583      4.6299e-05      4.6473e-05
v  epsilon             1.3191e-08      0.00021233       1.905e-05      1.9187e-05
v  TempC                   27.881          29.982          29.186          29.164
v  Density                 1.1652          1.1735          1.1684          1.1685
v  TurbVisc            1.2693e-09      6.0199e-05      1.4426e-05      1.4505e-05
v  CourantNb            0.0075836          3.9606          1.0481          1.0193
v  FourierNb              0.42112          6.6599          1.6079          1.5127
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1735          1.1683          1.1682


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42882          9.3023           2.656           2.532


 TIME FOR THE TIME STEP               83:        0.72837E-01

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


 INSTANT    0.420000000E+02   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44844E-04 0.14118E-01
   Friction velocity        uk    :  0.45449E-04 0.13527E-01
   Dimensionless distance   yplus :  0.71966E-02 0.18638E+01
   Friction thermal sca.    tstar : -0.81342E+01-0.55864E-01
   Rough dim-less th. sca.  tplus :  0.53695E-02 0.13906E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14097E-05      72   0.23043E-01   0.17343E-05 0.12929E+00 
c  Velocity[X]                                      0.56748E-06 
c  Velocity[Y]                                      0.11668E-05 
c  Velocity[Z]                                      0.60815E-33 
c  Pressure     0.10955E-05     322   0.35359E-03   0.12611E-01 0.17780E-01 
c  k            0.64272E-08      62   0.12571E-02   0.84566E-11 0.66247E-01 
c  epsilon      0.48915E-08      51   0.50983E-03   0.15030E-11 0.54939E-01 
c  TempC        0.24373E+01      55   0.24417E-03   0.10816E-02 0.15936E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.022472         0.02377      3.0286e-05      1.5306e-07
v  Velocity[Y]          -0.024532        0.036099       0.0017027       0.0010366
v  Velocity[Z]        -2.3614e-15      3.1691e-15     -1.7685e-17     -1.2088e-17
v  ǁVelocityǁ          0.00011624        0.037568        0.012577        0.012499
v  Pressure             -0.026574        0.032571     -0.00014116      5.3353e-19
v  k                   2.2121e-08      0.00022288      4.5653e-05      4.5907e-05
v  epsilon             1.3615e-08      0.00020887      1.8708e-05      1.8856e-05
v  TempC                   27.903          29.983          29.203          29.181
v  Density                 1.1652          1.1734          1.1683          1.1684
v  TurbVisc            1.3128e-09       6.034e-05      1.4319e-05      1.4434e-05
v  CourantNb            0.0029774          3.8373          1.0401          1.0102
v  FourierNb              0.42113          6.7046          1.6006          1.5076
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1734          1.1682          1.1682


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43095          9.4093          2.6407          2.5178


 TIME FOR THE TIME STEP               84:        0.70563E-01

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


 INSTANT    0.425000000E+02   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19502E-03 0.13951E-01
   Friction velocity        uk    :  0.20142E-03 0.13367E-01
   Dimensionless distance   yplus :  0.31894E-01 0.18545E+01
   Friction thermal sca.    tstar : -0.24984E+01-0.55147E-01
   Rough dim-less th. sca.  tplus :  0.23797E-01 0.13836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14064E-05      71   0.21421E-01   0.15799E-05 0.12354E+00 
c  Velocity[X]                                      0.51250E-06 
c  Velocity[Y]                                      0.10674E-05 
c  Velocity[Z]                                      0.64462E-33 
c  Pressure     0.10957E-05     322   0.36512E-03   0.12603E-01 0.17695E-01 
c  k            0.63663E-08      63   0.13607E-02   0.92152E-11 0.69940E-01 
c  epsilon      0.48576E-08      51   0.52188E-03   0.14012E-11 0.53635E-01 
c  TempC        0.24384E+01      55   0.22086E-03   0.10908E-02 0.15995E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.023371        0.024675      3.3148e-05      2.9031e-07
v  Velocity[Y]          -0.024908        0.035516       0.0016835       0.0010382
v  Velocity[Z]        -2.3595e-15      3.1689e-15     -1.7713e-17     -1.2082e-17
v  ǁVelocityǁ          0.00012226        0.036833         0.01258        0.012507
v  Pressure             -0.026845        0.032743     -0.00013903     -1.3549e-18
v  k                    2.253e-08      0.00022012      4.5012e-05      4.5358e-05
v  epsilon             1.4059e-08      0.00020629      1.8384e-05      1.8552e-05
v  TempC                   27.924          29.983          29.219          29.198
v  Density                 1.1652          1.1733          1.1683          1.1683
v  TurbVisc            1.3464e-09      6.0764e-05      1.4206e-05      1.4359e-05
v  CourantNb            0.0084689          4.0749          1.0375          1.0069
v  FourierNb              0.42113          6.6934          1.5928          1.5023
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1733          1.1681          1.1681


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43169          9.6591          2.6303          2.5092


 TIME FOR THE TIME STEP               85:        0.70355E-01

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


 INSTANT    0.430000000E+02   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83796E-04 0.13848E-01
   Friction velocity        uk    :  0.38879E-03 0.13287E-01
   Dimensionless distance   yplus :  0.61036E-01 0.18648E+01
   Friction thermal sca.    tstar : -0.23173E+01-0.54658E-01
   Rough dim-less th. sca.  tplus :  0.45540E-01 0.13913E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14057E-05      69   0.22371E-01   0.14318E-05 0.11751E+00 
c  Velocity[X]                                      0.47088E-06 
c  Velocity[Y]                                      0.96097E-06 
c  Velocity[Z]                                      0.61642E-33 
c  Pressure     0.10946E-05     322   0.37345E-03   0.12582E-01 0.17488E-01 
c  k            0.63112E-08      64   0.14131E-02   0.98979E-11 0.73285E-01 
c  epsilon      0.48308E-08      52   0.51813E-03   0.13368E-11 0.52906E-01 
c  TempC        0.24394E+01      56   0.21583E-03   0.10863E-02 0.15953E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.024219        0.025493      3.5213e-05      3.4009e-08
v  Velocity[Y]           -0.02525        0.034834       0.0016653       0.0010396
v  Velocity[Z]        -2.3567e-15      3.1683e-15     -1.7766e-17     -1.2062e-17
v  ǁVelocityǁ          8.7423e-05        0.035924        0.012596        0.012532
v  Pressure             -0.027116        0.032911     -0.00013675     -4.4227e-18
v  k                   2.3133e-08       0.0002178      4.4373e-05      4.4823e-05
v  epsilon             1.4217e-08      0.00020398      1.8074e-05      1.8268e-05
v  TempC                   27.945          29.984          29.236          29.214
v  Density                 1.1652          1.1732          1.1682          1.1683
v  TurbVisc             1.392e-09      6.1263e-05      1.4087e-05       1.428e-05
v  CourantNb            0.0036759          4.2336          1.0378          1.0072
v  FourierNb              0.42114           6.577          1.5846          1.4968
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1732          1.1681          1.1681


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43152          9.9056          2.6224           2.504


 TIME FOR THE TIME STEP               86:        0.70888E-01

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


 INSTANT    0.435000000E+02   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41205E-03 0.13593E-01
   Friction velocity        uk    :  0.41087E-03 0.13036E-01
   Dimensionless distance   yplus :  0.65058E-01 0.18703E+01
   Friction thermal sca.    tstar : -0.23950E+01-0.54337E-01
   Rough dim-less th. sca.  tplus :  0.48541E-01 0.13955E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14063E-05      67   0.21658E-01   0.12908E-05 0.11137E+00 
c  Velocity[X]                                      0.44005E-06 
c  Velocity[Y]                                      0.85079E-06 
c  Velocity[Z]                                      0.61629E-33 
c  Pressure     0.11085E-05     322   0.38017E-03   0.12734E-01 0.17109E-01 
c  k            0.62614E-08      63   0.13880E-02   0.10365E-10 0.75797E-01 
c  epsilon      0.48097E-08      51   0.49942E-03   0.12853E-11 0.52325E-01 
c  TempC        0.24404E+01      56   0.23427E-03   0.10719E-02 0.15838E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.025        0.026094      3.6669e-05       4.475e-08
v  Velocity[Y]          -0.025372        0.033995       0.0016478       0.0010407
v  Velocity[Z]        -2.3542e-15      3.1673e-15     -1.7744e-17     -1.2011e-17
v  ǁVelocityǁ          0.00010764        0.034793        0.012614        0.012561
v  Pressure             -0.027384        0.033074     -0.00013439      3.7067e-18
v  k                   2.3922e-08      0.00021548      4.3736e-05      4.4299e-05
v  epsilon             1.4486e-08      0.00020335      1.7775e-05      1.8001e-05
v  TempC                   27.975          29.985          29.252           29.23
v  Density                 1.1652          1.1731          1.1681          1.1682
v  TurbVisc            1.4496e-09      6.1256e-05      1.3963e-05      1.4198e-05
v  CourantNb            0.0068323          4.2919           1.039           1.009
v  FourierNb              0.42114          6.3108           1.576           1.491
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1731           1.168           1.168


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43147          10.052           2.615             2.5


 TIME FOR THE TIME STEP               87:        0.68526E-01

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


 INSTANT    0.440000000E+02   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28349E-03 0.13382E-01
   Friction velocity        uk    :  0.28274E-03 0.12849E-01
   Dimensionless distance   yplus :  0.42679E-01 0.18760E+01
   Friction thermal sca.    tstar : -0.30986E+01-0.54006E-01
   Rough dim-less th. sca.  tplus :  0.31843E-01 0.13997E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14078E-05      64   0.22575E-01   0.11650E-05 0.10556E+00 
c  Velocity[X]                                      0.41813E-06 
c  Velocity[Y]                                      0.74690E-06 
c  Velocity[Z]                                      0.55683E-33 
c  Pressure     0.11004E-05     322   0.37919E-03   0.12634E-01 0.16575E-01 
c  k            0.62153E-08      62   0.13338E-02   0.10506E-10 0.77107E-01 
c  epsilon      0.47932E-08      51   0.47824E-03   0.12446E-11 0.51886E-01 
c  TempC        0.24414E+01      56   0.31468E-03   0.10385E-02 0.15581E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.025576        0.026764      3.7804e-05      2.7435e-07
v  Velocity[Y]          -0.025278        0.033025       0.0016313       0.0010419
v  Velocity[Z]         -2.353e-15      3.1658e-15     -1.7648e-17     -1.1902e-17
v  ǁVelocityǁ           0.0001203          0.0334        0.012629         0.01259
v  Pressure             -0.027652        0.033232     -0.00013206        3.84e-18
v  k                   2.4884e-08      0.00021428      4.3101e-05      4.3779e-05
v  epsilon             1.4853e-08      0.00020212      1.7483e-05      1.7745e-05
v  TempC                   28.002          29.985          29.267          29.246
v  Density                 1.1652           1.173          1.1681          1.1681
v  TurbVisc            1.5186e-09      6.1788e-05      1.3834e-05      1.4113e-05
v  CourantNb            0.0054965          4.2652          1.0399          1.0108
v  FourierNb              0.42114          5.9158          1.5672           1.485
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652           1.173           1.168          1.1679


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4316          10.095          2.6071          2.4957


 TIME FOR THE TIME STEP               88:        0.64274E-01

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


 INSTANT    0.445000000E+02   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11704E-03 0.13133E-01
   Friction velocity        uk    :  0.12005E-03 0.12633E-01
   Dimensionless distance   yplus :  0.15458E-01 0.18769E+01
   Friction thermal sca.    tstar : -0.50651E+01-0.52384E-01
   Rough dim-less th. sca.  tplus :  0.11533E-01 0.14003E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14087E-05      62   0.23988E-01   0.10572E-05 0.10036E+00 
c  Velocity[X]                                      0.39867E-06 
c  Velocity[Y]                                      0.65857E-06 
c  Velocity[Z]                                      0.49960E-33 
c  Pressure     0.10806E-05     322   0.37131E-03   0.12399E-01 0.15866E-01 
c  k            0.61724E-08      61   0.13112E-02   0.10372E-10 0.77403E-01 
c  epsilon      0.47817E-08      50   0.46181E-03   0.11926E-11 0.51122E-01 
c  TempC        0.24423E+01      55   0.28862E-03   0.99253E-03 0.15224E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.026226        0.027314      3.8379e-05      2.3197e-07
v  Velocity[Y]           -0.02494        0.032304       0.0016153       0.0010432
v  Velocity[Z]        -2.3515e-15      3.1639e-15     -1.7463e-17     -1.1728e-17
v  ǁVelocityǁ          0.00014267        0.032317        0.012632        0.012607
v  Pressure             -0.027909        0.033385     -0.00012979      1.2987e-18
v  k                   2.5064e-08      0.00021373      4.2468e-05      4.3259e-05
v  epsilon             1.5051e-08       0.0002023      1.7197e-05      1.7499e-05
v  TempC                   28.033          29.986          29.283          29.261
v  Density                 1.1652          1.1729           1.168          1.1681
v  TurbVisc            1.5073e-09      6.1851e-05      1.3701e-05      1.4022e-05
v  CourantNb             0.010406          4.1739            1.04          1.0119
v  FourierNb              0.42114          6.0014          1.5582          1.4788
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1729          1.1679          1.1679


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43165          10.034          2.5982          2.4906


 TIME FOR THE TIME STEP               89:        0.63668E-01

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


 INSTANT    0.450000000E+02   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39803E-03 0.12929E-01
   Friction velocity        uk    :  0.39673E-03 0.12381E-01
   Dimensionless distance   yplus :  0.62818E-01 0.18756E+01
   Friction thermal sca.    tstar : -0.19472E+01-0.51225E-01
   Rough dim-less th. sca.  tplus :  0.46869E-01 0.13994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14091E-05      63   0.23054E-01   0.96087E-06 0.95546E-01 
c  Velocity[X]                                      0.37926E-06 
c  Velocity[Y]                                      0.58161E-06 
c  Velocity[Z]                                      0.45889E-33 
c  Pressure     0.10400E-05     322   0.35363E-03   0.11925E-01 0.15089E-01 
c  k            0.61299E-08      60   0.13024E-02   0.99680E-11 0.76665E-01 
c  epsilon      0.47720E-08      49   0.44803E-03   0.11500E-11 0.50505E-01 
c  TempC        0.24432E+01      54   0.28836E-03   0.92571E-03 0.14695E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.026643        0.027644        3.86e-05      2.1758e-07
v  Velocity[Y]          -0.024536        0.032619       0.0015997       0.0010447
v  Velocity[Z]        -2.3512e-15      3.1618e-15       -1.72e-17      -1.151e-17
v  ǁVelocityǁ          0.00024905        0.032642        0.012622         0.01261
v  Pressure             -0.028169        0.033533     -0.00012764      2.3798e-18
v  k                   2.4755e-08      0.00021347      4.1833e-05      4.2731e-05
v  epsilon             1.4783e-08       0.0002016      1.6913e-05      1.7256e-05
v  TempC                   28.064          29.986          29.298          29.276
v  Density                 1.1652          1.1728          1.1679           1.168
v  TurbVisc            1.4908e-09      6.2213e-05      1.3565e-05      1.3925e-05
v  CourantNb             0.010461          4.0213           1.039          1.0121
v  FourierNb              0.42115          6.0086          1.5492          1.4724
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1728          1.1678          1.1678


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43172          9.8509          2.5882          2.4845


 TIME FOR THE TIME STEP               90:        0.64495E-01

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


 INSTANT    0.455000000E+02   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35275E-03 0.12942E-01
   Friction velocity        uk    :  0.42064E-03 0.12146E-01
   Dimensionless distance   yplus :  0.54177E-01 0.18759E+01
   Friction thermal sca.    tstar : -0.32420E+01-0.50230E-01
   Rough dim-less th. sca.  tplus :  0.40422E-01 0.13997E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14082E-05      64   0.23708E-01   0.88264E-06 0.91533E-01 
c  Velocity[X]                                      0.35763E-06 
c  Velocity[Y]                                      0.52501E-06 
c  Velocity[Z]                                      0.54874E-33 
c  Pressure     0.99466E-06     316   0.33636E-03   0.11395E-01 0.14306E-01 
c  k            0.60875E-08      59   0.12409E-02   0.92224E-11 0.74518E-01 
c  epsilon      0.47644E-08      48   0.42250E-03   0.10788E-11 0.49183E-01 
c  TempC        0.24441E+01      53   0.24068E-03   0.86108E-03 0.14166E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.027001        0.027951      3.8394e-05     -3.9327e-08
v  Velocity[Y]          -0.024503        0.032663       0.0015848        0.001046
v  Velocity[Z]        -2.3527e-15      3.1593e-15      -1.685e-17      -1.122e-17
v  ǁVelocityǁ          0.00023658        0.032696        0.012599          0.0126
v  Pressure             -0.028415        0.033676     -0.00012563     -5.8267e-19
v  k                   2.4534e-08      0.00021424      4.1195e-05      4.2191e-05
v  epsilon             1.4571e-08      0.00020202      1.6633e-05      1.7015e-05
v  TempC                   28.096          29.987          29.313          29.291
v  Density                 1.1652          1.1727          1.1679           1.168
v  TurbVisc            1.4799e-09      6.2379e-05      1.3425e-05      1.3819e-05
v  CourantNb             0.010579          3.8537          1.0371          1.0114
v  FourierNb              0.42115           5.919          1.5401          1.4658
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1727          1.1678          1.1678


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43185          9.5573          2.5772          2.4771


 TIME FOR THE TIME STEP               91:        0.65044E-01

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


 INSTANT    0.460000000E+02   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67954E-03 0.12885E-01
   Friction velocity        uk    :  0.67584E-03 0.11941E-01
   Dimensionless distance   yplus :  0.87025E-01 0.18656E+01
   Friction thermal sca.    tstar : -0.18389E+01-0.49524E-01
   Rough dim-less th. sca.  tplus :  0.64930E-01 0.13920E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14063E-05      64   0.25155E-01   0.81040E-06 0.87740E-01 
c  Velocity[X]                                      0.33532E-06 
c  Velocity[Y]                                      0.47509E-06 
c  Velocity[Z]                                      0.48719E-33 
c  Pressure     0.95479E-06     313   0.31307E-03   0.10928E-01 0.13406E-01 
c  k            0.60430E-08      58   0.11221E-02   0.83633E-11 0.71741E-01 
c  epsilon      0.47562E-08      47   0.38161E-03   0.99747E-12 0.47540E-01 
c  TempC        0.24450E+01      52   0.30727E-03   0.79372E-03 0.13594E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.02727        0.028109      3.8169e-05       5.571e-08
v  Velocity[Y]          -0.024488         0.03286       0.0015708       0.0010475
v  Velocity[Z]         -2.354e-15      3.1561e-15     -1.6477e-17     -1.0901e-17
v  ǁVelocityǁ          0.00015357         0.03291        0.012566        0.012577
v  Pressure             -0.028657        0.033812     -0.00012379     -1.9656e-19
v  k                   2.4418e-08        0.000216      4.0549e-05      4.1632e-05
v  epsilon             1.4417e-08      0.00020342      1.6355e-05      1.6775e-05
v  TempC                   28.124          29.987          29.327          29.305
v  Density                 1.1652          1.1725          1.1678          1.1679
v  TurbVisc             1.476e-09      6.2136e-05      1.3278e-05      1.3702e-05
v  CourantNb            0.0099608          3.8935          1.0338          1.0092
v  FourierNb              0.42115          5.9618          1.5309          1.4588
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1725          1.1677          1.1677


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43183          9.1842          2.5647          2.4681


 TIME FOR THE TIME STEP               92:        0.63218E-01

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


 INSTANT    0.465000000E+02   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28773E-03 0.12904E-01
   Friction velocity        uk    :  0.29091E-03 0.11775E-01
   Dimensionless distance   yplus :  0.37459E-01 0.18663E+01
   Friction thermal sca.    tstar : -0.18697E+01-0.48921E-01
   Rough dim-less th. sca.  tplus :  0.27949E-01 0.13925E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14028E-05      63   0.25083E-01   0.74630E-06 0.84328E-01 
c  Velocity[X]                                      0.31051E-06 
c  Velocity[Y]                                      0.43579E-06 
c  Velocity[Z]                                      0.46087E-33 
c  Pressure     0.90942E-06     310   0.29818E-03   0.10396E-01 0.12692E-01 
c  k            0.59957E-08      57   0.95931E-03   0.74638E-11 0.68545E-01 
c  epsilon      0.47471E-08      46   0.33251E-03   0.91364E-12 0.45730E-01 
c  TempC        0.24459E+01      51   0.33686E-03   0.73878E-03 0.13109E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.027352        0.028154      3.7462e-05      5.5374e-08
v  Velocity[Y]          -0.024464        0.032788       0.0015581        0.001049
v  Velocity[Z]        -2.3571e-15      3.1514e-15     -1.6115e-17     -1.0554e-17
v  ǁVelocityǁ           2.987e-05        0.032845        0.012524        0.012541
v  Pressure             -0.028889        0.033944     -0.00012213      2.6887e-18
v  k                   2.4411e-08      0.00021851      3.9897e-05      4.1055e-05
v  epsilon             1.4319e-08      0.00020562      1.6081e-05      1.6536e-05
v  TempC                   28.152          29.987          29.341          29.319
v  Density                 1.1652          1.1724          1.1678          1.1679
v  TurbVisc            1.4796e-09      6.0612e-05      1.3125e-05      1.3572e-05
v  CourantNb            0.0099825           3.882          1.0288          1.0055
v  FourierNb              0.42115          5.9791          1.5216          1.4516
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1724          1.1677          1.1677


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43121          8.8214          2.5505          2.4571


 TIME FOR THE TIME STEP               93:        0.62013E-01

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


 INSTANT    0.470000000E+02   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56102E-03 0.12978E-01
   Friction velocity        uk    :  0.55871E-03 0.11810E-01
   Dimensionless distance   yplus :  0.71941E-01 0.18720E+01
   Friction thermal sca.    tstar : -0.27584E+01-0.48476E-01
   Rough dim-less th. sca.  tplus :  0.53676E-01 0.13967E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13984E-05      63   0.25583E-01   0.68134E-06 0.80768E-01 
c  Velocity[X]                                      0.28309E-06 
c  Velocity[Y]                                      0.39825E-06 
c  Velocity[Z]                                      0.51286E-33 
c  Pressure     0.84382E-06     311   0.28823E-03   0.96346E-02 0.11958E-01 
c  k            0.59460E-08      56   0.80332E-03   0.66240E-11 0.65352E-01 
c  epsilon      0.47360E-08      45   0.28743E-03   0.82207E-12 0.43611E-01 
c  TempC        0.24468E+01      50   0.31670E-03   0.68948E-03 0.12658E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.027391        0.028105       3.646e-05     -9.5516e-08
v  Velocity[Y]          -0.024334        0.032569       0.0015474       0.0010504
v  Velocity[Z]        -2.3617e-15      3.1463e-15     -1.5711e-17       -1.02e-17
v  ǁVelocityǁ          9.2652e-05        0.033565        0.012475        0.012496
v  Pressure             -0.029116        0.034071     -0.00012062      4.9492e-18
v  k                   2.4509e-08      0.00022044      3.9234e-05      4.0455e-05
v  epsilon             1.4271e-08      0.00020732       1.581e-05      1.6294e-05
v  TempC                   28.185          29.988          29.355          29.333
v  Density                 1.1652          1.1723          1.1677          1.1678
v  TurbVisc            1.4906e-09      5.9872e-05      1.2963e-05       1.343e-05
v  CourantNb            0.0070598          3.8376           1.023          1.0007
v  FourierNb              0.42115          5.9228          1.5122          1.4439
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1723          1.1676          1.1676


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43073           8.458          2.5352          2.4446


 TIME FOR THE TIME STEP               94:        0.62230E-01

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


 INSTANT    0.475000000E+02   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50184E-03 0.13137E-01
   Friction velocity        uk    :  0.59951E-03 0.11941E-01
   Dimensionless distance   yplus :  0.77197E-01 0.18930E+01
   Friction thermal sca.    tstar : -0.29513E+01-0.48125E-01
   Rough dim-less th. sca.  tplus :  0.57597E-01 0.14124E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13921E-05      62   0.23328E-01   0.62303E-06 0.77502E-01 
c  Velocity[X]                                      0.25637E-06 
c  Velocity[Y]                                      0.36666E-06 
c  Velocity[Z]                                      0.49960E-33 
c  Pressure     0.82024E-06     307   0.27371E-03   0.93520E-02 0.11271E-01 
c  k            0.58922E-08      55   0.67607E-03   0.59411E-11 0.62683E-01 
c  epsilon      0.47212E-08      45   0.24777E-03   0.75018E-12 0.41903E-01 
c  TempC        0.24476E+01      49   0.25841E-03   0.64441E-03 0.12232E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.027333        0.027862      3.5077e-05     -1.8414e-07
v  Velocity[Y]          -0.024186        0.032267       0.0015388       0.0010521
v  Velocity[Z]        -2.3667e-15       3.141e-15     -1.5361e-17     -9.8618e-18
v  ǁVelocityǁ          0.00030567        0.034138        0.012421        0.012442
v  Pressure             -0.029333        0.034194     -0.00011931     -9.5474e-19
v  k                     2.47e-08      0.00022252      3.8559e-05      3.9831e-05
v  epsilon             1.4266e-08      0.00020931       1.554e-05       1.605e-05
v  TempC                   28.199          29.988          29.369          29.347
v  Density                 1.1652          1.1722          1.1677          1.1678
v  TurbVisc            1.5081e-09      5.8396e-05      1.2792e-05      1.3273e-05
v  CourantNb             0.007004          3.8709          1.0175         0.99576
v  FourierNb              0.42114           5.805          1.5024          1.4357
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1722          1.1676          1.1676


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43055          8.2188          2.5199          2.4315


 TIME FOR THE TIME STEP               95:        0.64503E-01

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


 INSTANT    0.480000000E+02   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43903E-03 0.13270E-01
   Friction velocity        uk    :  0.44509E-03 0.12063E-01
   Dimensionless distance   yplus :  0.57313E-01 0.19122E+01
   Friction thermal sca.    tstar : -0.17913E+01-0.47901E-01
   Rough dim-less th. sca.  tplus :  0.42762E-01 0.14268E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13852E-05      61   0.24722E-01   0.56758E-06 0.74292E-01 
c  Velocity[X]                                      0.23001E-06 
c  Velocity[Y]                                      0.33758E-06 
c  Velocity[Z]                                      0.58635E-33 
c  Pressure     0.78938E-06     306   0.26800E-03   0.89870E-02 0.10703E-01 
c  k            0.58336E-08      54   0.58982E-03   0.53605E-11 0.60352E-01 
c  epsilon      0.47011E-08      44   0.22032E-03   0.68130E-12 0.40197E-01 
c  TempC        0.24484E+01      48   0.33036E-03   0.60511E-03 0.11848E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.027324         0.02751      3.3639e-05     -9.3762e-08
v  Velocity[Y]          -0.024005        0.031906       0.0015327       0.0010536
v  Velocity[Z]        -2.3738e-15      3.1356e-15     -1.5017e-17     -9.5492e-18
v  ǁVelocityǁ          4.5205e-05        0.034843        0.012363         0.01238
v  Pressure             -0.029548        0.034313     -0.00011814       1.741e-18
v  k                   2.4371e-08      0.00022402      3.7868e-05       3.918e-05
v  epsilon             1.4296e-08      0.00021079       1.527e-05      1.5798e-05
v  TempC                   28.218          29.989          29.382           29.36
v  Density                 1.1652          1.1721          1.1676          1.1677
v  TurbVisc             1.469e-09      5.6444e-05      1.2609e-05      1.3102e-05
v  CourantNb            0.0093565          3.8703          1.0117         0.99037
v  FourierNb              0.42114          5.6694          1.4923          1.4271
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1721          1.1675          1.1675


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43061          8.1621           2.504          2.4175


 TIME FOR THE TIME STEP               96:        0.64190E-01

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


 INSTANT    0.485000000E+02   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56951E-03 0.13360E-01
   Friction velocity        uk    :  0.56823E-03 0.12140E-01
   Dimensionless distance   yplus :  0.73166E-01 0.19245E+01
   Friction thermal sca.    tstar : -0.15718E+01-0.46731E-01
   Rough dim-less th. sca.  tplus :  0.54590E-01 0.14359E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13768E-05      60   0.23028E-01   0.52389E-06 0.71750E-01 
c  Velocity[X]                                      0.20725E-06 
c  Velocity[Y]                                      0.31663E-06 
c  Velocity[Z]                                      0.55977E-33 
c  Pressure     0.77253E-06     306   0.25660E-03   0.87813E-02 0.10131E-01 
c  k            0.57709E-08      53   0.53019E-03   0.49017E-11 0.58538E-01 
c  epsilon      0.46769E-08      43   0.20286E-03   0.63574E-12 0.39112E-01 
c  TempC        0.24492E+01      47   0.26702E-03   0.57574E-03 0.11551E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.027313        0.027412       3.176e-05     -2.3396e-07
v  Velocity[Y]          -0.023761         0.03147       0.0015292       0.0010553
v  Velocity[Z]        -2.3816e-15      3.1307e-15     -1.4802e-17     -9.2704e-18
v  ǁVelocityǁ           6.693e-05         0.03482        0.012298        0.012308
v  Pressure             -0.029752        0.034428     -0.00011714     -9.3368e-19
v  k                   2.3264e-08      0.00022551      3.7164e-05      3.8505e-05
v  epsilon             1.4249e-08      0.00021243      1.4998e-05      1.5541e-05
v  TempC                   28.237          29.989          29.395          29.373
v  Density                 1.1652          1.1721          1.1676          1.1676
v  TurbVisc            1.4062e-09      5.3815e-05      1.2416e-05      1.2916e-05
v  CourantNb            0.0072836          3.8781          1.0056         0.98452
v  FourierNb              0.42114          5.5354          1.4819           1.418
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1721          1.1675          1.1675


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43071          8.1309          2.4875          2.4025


 TIME FOR THE TIME STEP               97:        0.65118E-01

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


 INSTANT    0.490000000E+02   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47805E-03 0.13407E-01
   Friction velocity        uk    :  0.47635E-03 0.12180E-01
   Dimensionless distance   yplus :  0.61334E-01 0.19309E+01
   Friction thermal sca.    tstar : -0.17661E+01-0.45483E-01
   Rough dim-less th. sca.  tplus :  0.45762E-01 0.14407E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13677E-05      58   0.23214E-01   0.48476E-06 0.69431E-01 
c  Velocity[X]                                      0.18500E-06 
c  Velocity[Y]                                      0.29976E-06 
c  Velocity[Z]                                      0.54122E-33 
c  Pressure     0.72139E-06     308   0.24836E-03   0.81871E-02 0.96274E-02 
c  k            0.57045E-08      52   0.48298E-03   0.44960E-11 0.56909E-01 
c  epsilon      0.46488E-08      43   0.18942E-03   0.59503E-12 0.38145E-01 
c  TempC        0.24500E+01      46   0.26644E-03   0.54489E-03 0.11233E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.026994        0.027306      2.9905e-05     -2.9981e-07
v  Velocity[Y]          -0.023552        0.030992       0.0015286       0.0010568
v  Velocity[Z]        -2.3907e-15      3.1262e-15     -1.4555e-17     -9.0401e-18
v  ǁVelocityǁ           0.0001216        0.034989        0.012228        0.012228
v  Pressure             -0.029956         0.03454     -0.00011624     -4.3876e-18
v  k                   2.2398e-08      0.00022638      3.6449e-05       3.781e-05
v  epsilon             1.3611e-08      0.00021356      1.4725e-05      1.5277e-05
v  TempC                   28.257          29.989          29.408          29.386
v  Density                 1.1652           1.172          1.1675          1.1676
v  TurbVisc            1.3591e-09      5.1997e-05      1.2214e-05      1.2719e-05
v  CourantNb            0.0096024          3.8655         0.99919          0.9781
v  FourierNb              0.42114          5.3719          1.4712          1.4084
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652           1.172          1.1674          1.1674


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43086          8.0981          2.4704          2.3865


 TIME FOR THE TIME STEP               98:        0.62684E-01

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


 INSTANT    0.495000000E+02   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17665E-03 0.13397E-01
   Friction velocity        uk    :  0.17687E-03 0.12170E-01
   Dimensionless distance   yplus :  0.22774E-01 0.19295E+01
   Friction thermal sca.    tstar : -0.24517E+01-0.44459E-01
   Rough dim-less th. sca.  tplus :  0.16992E-01 0.14396E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         99
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13571E-05      57   0.20710E-01   0.45748E-06 0.67907E-01 
c  Velocity[X]                                      0.16895E-06 
c  Velocity[Y]                                      0.28853E-06 
c  Velocity[Z]                                      0.51670E-33 
c  Pressure     0.70814E-06     308   0.23346E-03   0.80232E-02 0.91339E-02 
c  k            0.56348E-08      51   0.44701E-03   0.41220E-11 0.55345E-01 
c  epsilon      0.46171E-08      42   0.18402E-03   0.55506E-12 0.37166E-01 
c  TempC        0.24508E+01      45   0.21514E-03   0.51802E-03 0.10948E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.0266        0.027174      2.7684e-05     -3.9663e-07
v  Velocity[Y]          -0.023362        0.030474       0.0015313       0.0010586
v  Velocity[Z]           -2.4e-15       3.122e-15     -1.4445e-17     -8.8586e-18
v  ǁVelocityǁ          0.00016848        0.034586        0.012153        0.012141
v  Pressure             -0.030149        0.034648     -0.00011548     -2.1061e-20
v  k                   2.1735e-08      0.00022677      3.5726e-05      3.7098e-05
v  epsilon             1.3085e-08      0.00021427      1.4449e-05      1.5007e-05
v  TempC                   28.282           29.99           29.42          29.398
v  Density                 1.1652          1.1719          1.1675          1.1675
v  TurbVisc             1.325e-09      5.0012e-05      1.2004e-05      1.2513e-05
v  CourantNb            0.0099171          3.8347         0.99244         0.97119
v  FourierNb              0.42114          5.1961          1.4604          1.3986
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1719          1.1674          1.1674


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43118          8.0648          2.4528          2.3698


 TIME FOR THE TIME STEP               99:        0.60938E-01

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


 INSTANT    0.500000000E+02   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         384         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        7732         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32636E-03 0.13375E-01
   Friction velocity        uk    :  0.32530E-03 0.12168E-01
   Dimensionless distance   yplus :  0.51509E-01 0.19289E+01
   Friction thermal sca.    tstar : -0.20919E+01-0.43560E-01
   Rough dim-less th. sca.  tplus :  0.38431E-01 0.14392E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        384
   Total number of wall faces                   :        384
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step        100
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            



 Write final restart files
   checkpoint at iteration        100, Physical time    0.50000E+02


   ** 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


 Time for restart files:    0.10926E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13467E-05      56   0.21419E-01   0.44185E-06 0.67226E-01 
c  Velocity[X]                                      0.15489E-06 
c  Velocity[Y]                                      0.28696E-06 
c  Velocity[Z]                                      0.48868E-33 
c  Pressure     0.67493E-06     309   0.22512E-03   0.76339E-02 0.86907E-02 
c  k            0.55621E-08      50   0.41401E-03   0.37854E-11 0.53903E-01 
c  epsilon      0.45814E-08      41   0.17613E-03   0.52665E-12 0.36550E-01 
c  TempC        0.24515E+01      45   0.25065E-03   0.48794E-03 0.10621E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.026702         0.02715      2.5819e-05     -2.2013e-07
v  Velocity[Y]          -0.023213        0.030046       0.0015369       0.0010601
v  Velocity[Z]        -2.4101e-15      3.1181e-15     -1.4308e-17     -8.7052e-18
v  ǁVelocityǁ          0.00017902        0.034387        0.012078        0.012051
v  Pressure             -0.030333        0.034752     -0.00011481     -3.2223e-18
v  k                   2.1235e-08      0.00022705      3.4996e-05      3.6373e-05
v  epsilon             1.2651e-08        0.000215      1.4171e-05      1.4731e-05
v  TempC                   28.309           29.99          29.432           29.41
v  Density                 1.1652          1.1718          1.1674          1.1675
v  TurbVisc            1.3013e-09       4.795e-05       1.179e-05      1.2299e-05
v  CourantNb             0.003772          3.8129         0.98551         0.96376
v  FourierNb              0.42114          5.0202          1.4494          1.3885
v  total_pressure      1.0134e+05      1.0134e+05      1.0134e+05      1.0134e+05

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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Boundary Density          1.1652          1.1718          1.1673          1.1673


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43152          8.0509          2.4349          2.3522


 TIME FOR THE TIME STEP              100:        0.21447E+00

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.16000E-04
      -----------------------                                



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




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


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

 Destroying structures and ending computation

Time elapsed defining values using MEI:      0.15768


Calculation time summary:

  User CPU time:              8.509 s
  System CPU time:            0.264 s

  Elapsed time:               8.787 s
  CPU / elapsed time          0.998

Memory use summary:

  Total memory used:                             105.051 MiB
  Theoretical instrumented dynamic memory:         7.541 MiB
