command: 
 /usr/lib/code_saturne/cs_solver --param fluidcoupled

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

                                  (R)
                      Code_Saturne

                      Version 4.2.0


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

  build Min 07 Peb 2016 01:11:58  WIB
  MPI version 3.0 (Open MPI 1.10.2)


  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:                Sel 11 Okt 2016 10:25:41  WIB
  System:              Linux 4.4.0-31-generic
  Machine:             nur-Aspire-4930
  Processor:           model name	: Intel(R) Core(TM)2 Duo CPU     T5800  @ 2.00GHz
  Memory:              1930 MB
  User:                nur (Nur)
  Directory:           /home/nur/Documents/CFD_EXERCISE/HEAT_CONJUGATE/rev_3disks2D/fluid/RESU/20161011-1025
  OpenMP threads:      1
  Processors/node:     2
  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            )
       IWALLF =              3 (wall function               )
                               (0: disabled                 )
                               (1: one scale power law
                                   (forbidden for k-epsilon))
                               (2: one scale log law        )
                               (3: two scales log law       )
                               (4: scalable wall function   )
                               (5: two scales V. Driest     )
                               (6: two scales smooth/rough  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       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 -0.1000E+13  0.1000E+13
-------------------------------------------------------

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

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

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

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

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


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


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

 --- Restarted calculation
       ISUITE =              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
TempC
Density
Boundary Density
TurbVisc
CourantNb
FourierNb
total_pressure
Yplus
         --           --

 --- 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 =              1 (Force exerted by the
                                     fluid on the boundary)
       ipstft =              1 (Thermal flux   at boundary)
       ipstnu =              0 (Dimensionless thermal
                                          flux at boundary)


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


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

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


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


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: 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 (0.0175 s)
                                                             
       ALMAX  =    0.12354E+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           0.1071E-04  0.1071E-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  0.3646E-02  0.3646E-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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80862E-05    2390   0.54381E+00   0.14086E-03 0.20000E+01 
c  Velocity[X]                                      0.35916E-04 
c  Velocity[Y]                                      0.10495E-03 
c  Velocity[Z]                                      0.17857E-29 
c  Pressure     0.32854E-04     220   0.16861E+00   0.99810E+00 0.20000E+01 
c  k            0.45275E-07    1560   0.28545E+00   0.32484E-06 0.32726E+01 
c  epsilon      0.37143E-05    2373   0.13234E+00   0.58172E-03 0.19988E+01 
c  TempC        0.18276E+01    2415   0.14982E-01   0.14699E+01 0.82418E-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]          -0.013563        0.013617      1.7911e-05       3.112e-06
v  Velocity[Y]          -0.014696        0.028787      0.00063304     -0.00042771
v  Velocity[Z]        -5.6291e-15      4.3224e-15      3.2471e-18      4.1472e-18
v  ǁVelocityǁ           4.285e-05         0.02881       0.0072459       0.0069424
v  Pressure             -0.058095        0.055821      9.7166e-05      1.0629e-17
v  k                    1.774e-05      0.00043715      0.00020578       0.0002152
v  epsilon               0.004844        0.033472         0.01628        0.015659
v  TempC                   20.308          21.599           20.83          20.801
v  Density                 1.2049          1.2049          1.2049          1.2049
v  TurbVisc             0.0036461       0.0036461       0.0036461       0.0036461
v  CourantNb                    0               0               0               0
v  FourierNb                81.53          528.29          171.41          161.45
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  TempC                         20              30          20.473          20.909
v  Boundary Density          1.2049          1.2049          1.2049          1.2049
v  Yplus                          0          1.2143        0.048756        0.096289


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           81.53          528.29          171.41          161.45


 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   :  0.40488E-03 0.15123E-01
   Friction velocity        uk    :  0.91204E-03 0.14385E-01
   Dimensionless distance   yplus :  0.12089E+00 0.19050E+01
   Friction thermal sca.    tstar : -0.96580E+02-0.59227E+01
   Rough dim-less th. sca.  tplus :  0.90201E-01 0.14214E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72486E-05      49   0.13267E-01   0.16265E-03 0.13892E+01 
c  Velocity[X]                                      0.73382E-04 
c  Velocity[Y]                                      0.89273E-04 
c  Velocity[Z]                                      0.11569E-29 
c  Pressure     0.11903E-03     207   0.56510E-01   0.99930E+00 0.20000E+01 
c  k            0.19384E-07      13   0.30814E-02   0.10379E-06 0.21490E+02 
c  epsilon      0.12894E-05      10   0.25652E-02   0.57175E-03 0.13536E+03 
c  TempC        0.18827E+01      42   0.23114E-02   0.26247E+01 0.10755E+00 
-----------------------------------------------------------------------------
  
  

  ** 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]           -0.03764         0.03764      3.0861e-05       5.407e-06
v  Velocity[Y]          -0.024422         0.05858     -0.00030922      -0.0015642
v  Velocity[Z]         -9.318e-15      7.3317e-15       8.613e-18      4.0249e-18
v  ǁVelocityǁ          9.1684e-05        0.058914        0.010552        0.010039
v  Pressure             -0.064226        0.064506      9.0761e-05       -2.78e-18
v  k                    1.894e-08      6.8247e-05      1.2028e-05      1.3182e-05
v  epsilon             2.1669e-05      0.00045377      0.00021181      0.00022069
v  TempC                   20.312          25.507          21.357          21.268
v  Density                 1.1984          1.2037          1.2015          1.2017
v  TurbVisc            1.0192e-09      4.2738e-06      7.0757e-07      7.7842e-07
v  CourantNb             0.016467          2.5271         0.60056         0.56363
v  FourierNb              0.40904          2.6706         0.89024         0.84121
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  TempC                     20.308              30          21.264          21.637
v  Boundary Density          1.1984          1.2037          1.2015          1.2015
v  Yplus                          0           1.905        0.055932         0.10616


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42624          4.2099          1.4908          1.4048


 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 0.25283E-01
   Friction velocity        uet   :  0.37665E-03 0.18237E-01
   Friction velocity        uk    :  0.37579E-03 0.21169E-01
   Dimensionless distance   yplus :  0.49125E-01 0.27699E+01
   Friction thermal sca.    tstar : -0.12539E+03-0.23530E+01
   Rough dim-less th. sca.  tplus :  0.36653E-01 0.20667E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        332
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17370E-05      45   0.32225E-01   0.10026E-03 0.80346E+00 
c  Velocity[X]                                      0.20386E-04 
c  Velocity[Y]                                      0.79878E-04 
c  Velocity[Z]                                      0.81745E-30 
c  Pressure     0.22359E-04     151   0.99591E-03   0.20667E+00 0.22337E-01 
c  k            0.71928E-08      17   0.10020E-02   0.60350E-09 0.86965E+01 
c  epsilon      0.25905E-06      12   0.22740E-03   0.10793E-06 0.21809E+02 
c  TempC        0.19346E+01      47   0.24816E-02   0.75615E+00 0.56789E-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]          -0.036408        0.036483      4.0662e-05       4.596e-08
v  Velocity[Y]          -0.024788        0.084021      0.00073855      -0.0009258
v  Velocity[Z]         -8.258e-15       6.719e-15      1.0598e-17        1.95e-18
v  ǁVelocityǁ           7.991e-05        0.084059        0.014141        0.013508
v  Pressure             -0.063123        0.063961       8.669e-05      2.8081e-20
v  k                   4.1428e-11      1.6769e-05      1.7971e-06      2.0007e-06
v  epsilon              4.685e-08      7.9255e-05      1.3595e-05       1.418e-05
v  TempC                   20.314          27.381          21.707          21.585
v  Density                 1.1827          1.2037          1.1994          1.1998
v  TurbVisc             1.492e-12      1.1542e-06      1.1388e-07      1.2871e-07
v  CourantNb            0.0073444          3.4305         0.82036         0.76942
v  FourierNb              0.41328          2.6497         0.86475         0.81486
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  TempC                     20.312              30          21.766          22.061
v  Boundary Density          1.1827          1.2037          1.1987          1.1985
v  Yplus                          0          2.7699        0.080527         0.15031


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42777          4.2505          1.6851          1.5843


 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         0.106871735E-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 0.28085E-01
   Friction velocity        uet   :  0.12983E-02 0.18278E-01
   Friction velocity        uk    :  0.12981E-02 0.25045E-01
   Dimensionless distance   yplus :  0.20802E+00 0.32599E+01
   Friction thermal sca.    tstar : -0.23458E+02-0.13109E+01
   Rough dim-less th. sca.  tplus :  0.15521E+00 0.24322E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        243
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25705E-05      54   0.38512E-01   0.24597E-03 0.82029E+00 
c  Velocity[X]                                      0.44819E-04 
c  Velocity[Y]                                      0.20115E-03 
c  Velocity[Z]                                      0.26798E-30 
c  Pressure     0.37806E-04     171   0.39079E-02   0.41971E+00 0.10870E+00 
c  k            0.12614E-07      21   0.12379E-03   0.48302E-09 0.19828E+01 
c  epsilon      0.40183E-06      15   0.17113E-04   0.20982E-06 0.19715E+01 
c  TempC        0.19652E+01      56   0.37543E-02   0.36052E+00 0.38733E-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]          -0.049355        0.049365      5.6323e-05       7.329e-07
v  Velocity[Y]          -0.036517         0.11074       0.0018137     -0.00039179
v  Velocity[Z]        -7.6535e-15      6.2445e-15      1.1191e-17      6.0405e-19
v  ǁVelocityǁ          0.00025279         0.11103        0.021106        0.020449
v  Pressure             -0.058907        0.061212      7.1373e-05     -1.9095e-18
v  k                    4.045e-16      0.00019105      2.6813e-06      2.0602e-06
v  epsilon             1.3872e-09       0.0041801       4.745e-05      3.3481e-05
v  TempC                   20.317          28.466          21.971          21.829
v  Density                 1.1753          1.2037           1.198          1.1985
v  TurbVisc            1.5945e-17      4.7125e-07      3.4718e-08      3.9707e-08
v  CourantNb              0.01967          4.9717          1.1482           1.087
v  FourierNb              0.41554          2.6536         0.86708         0.81536
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  TempC                     20.314              30            22.1          22.349
v  Boundary Density          1.1753          1.2037          1.1971          1.1967
v  Yplus                          0          3.2599         0.09674         0.18453


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44459          6.6115          2.0153          1.9023


 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         0.956841174E-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 0.31910E-01
   Friction velocity        uet   :  0.15838E-02 0.18262E-01
   Friction velocity        uk    :  0.15838E-02 0.27016E-01
   Dimensionless distance   yplus :  0.25304E+00 0.38566E+01
   Friction thermal sca.    tstar : -0.14385E+02-0.80805E+00
   Rough dim-less th. sca.  tplus :  0.18879E+00 0.28775E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35654E-05      65   0.54968E-01   0.30368E-03 0.64813E+00 
c  Velocity[X]                                      0.83236E-04 
c  Velocity[Y]                                      0.22045E-03 
c  Velocity[Z]                                      0.17992E-30 
c  Pressure     0.37903E-04     175   0.48932E-02   0.44264E+00 0.68070E-01 
c  k            0.21413E-07      27   0.28264E-04   0.12552E-08 0.16845E+01 
c  epsilon      0.67441E-06      18   0.62775E-05   0.46944E-06 0.16482E+01 
c  TempC        0.19854E+01      66   0.53596E-02   0.29370E+00 0.34604E-01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.1909e-16                             6
a  epsilon
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.064316        0.064353      6.6983e-05      1.3988e-06
v  Velocity[Y]          -0.049105         0.12943       0.0027322      5.6859e-05
v  Velocity[Z]        -7.1914e-15      5.8824e-15      1.0598e-17     -1.6644e-18
v  ǁVelocityǁ          0.00036558         0.13017        0.029779        0.029169
v  Pressure             -0.055071        0.059825      4.5587e-05     -2.5694e-18
v  k                   5.1299e-21      0.00021464      6.5982e-06      5.7255e-06
v  epsilon             1.8621e-11       0.0050477      0.00012629      0.00010577
v  TempC                   20.322          29.113          22.191          22.039
v  Density                 1.1711          1.2036           1.197          1.1975
v  TurbVisc            3.9896e-25      9.4102e-07      2.7523e-08      2.6471e-08
v  CourantNb             0.016735          6.5721          1.7128          1.6415
v  FourierNb              0.41663          2.6604         0.87438         0.82227
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  TempC                     20.317              30          22.351          22.571
v  Boundary Density          1.1711          1.2036          1.1959          1.1955
v  Yplus                          0          3.8566         0.11722         0.22683


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45676          8.3028          2.5872          2.4638


 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         0.265111386E-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 0.32133E-01
   Friction velocity        uet   :  0.10808E-02 0.18123E-01
   Friction velocity        uk    :  0.10808E-02 0.29126E-01
   Dimensionless distance   yplus :  0.17238E+00 0.41650E+01
   Friction thermal sca.    tstar : -0.17118E+02-0.57066E+00
   Rough dim-less th. sca.  tplus :  0.12861E+00 0.31076E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        121
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45660E-05      77   0.67544E-01   0.28298E-03 0.49308E+00 
c  Velocity[X]                                      0.99430E-04 
c  Velocity[Y]                                      0.18355E-03 
c  Velocity[Z]                                      0.13906E-30 
c  Pressure     0.34321E-04     176   0.57374E-02   0.36246E+00 0.54003E-01 
c  k            0.29826E-07      34   0.51604E-04   0.12010E-08 0.12516E+01 
c  epsilon      0.96009E-06      21   0.21063E-04   0.43730E-06 0.12302E+01 
c  TempC        0.20008E+01      78   0.76788E-02   0.32446E+00 0.36038E-01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1745e-18                             4
a  epsilon     -2.0247e-09                             2
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.08223        0.082162      8.5453e-05      1.5017e-06
v  Velocity[Y]          -0.061419          0.1516        0.003428      0.00040635
v  Velocity[Z]        -6.8316e-15      5.5464e-15      8.3982e-18     -4.0755e-18
v  ǁVelocityǁ          0.00019552          0.1581        0.038215         0.03769
v  Pressure              -0.05139        0.059844      -2.667e-06     -8.9999e-18
v  k                    6.757e-23      0.00022094      1.1007e-05      9.9682e-06
v  epsilon             1.1403e-13       0.0051767        0.000208      0.00018094
v  TempC                   20.324          29.516          22.389          22.233
v  Density                 1.1686          1.2036          1.1961          1.1967
v  TurbVisc            2.7242e-32      1.0353e-06      4.5522e-08      4.2937e-08
v  CourantNb             0.027823          7.6809          2.3928          2.3087
v  FourierNb              0.41714          2.6695         0.88258         0.82943
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  TempC                     20.322              30          22.561          22.762
v  Boundary Density          1.1686          1.2036           1.195          1.1946
v  Yplus                          0           4.165          0.1319         0.25718


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44582          9.3868          3.2753          3.1381


 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         0.828049152E-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 0.32111E-01
   Friction velocity        uet   :  0.10277E-02 0.18487E-01
   Friction velocity        uk    :  0.10277E-02 0.29958E-01
   Dimensionless distance   yplus :  0.16365E+00 0.45731E+01
   Friction thermal sca.    tstar : -0.15298E+02-0.42585E+00
   Rough dim-less th. sca.  tplus :  0.12210E+00 0.34120E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        106
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54591E-05      89   0.84510E-01   0.25859E-03 0.39775E+00 
c  Velocity[X]                                      0.10097E-03 
c  Velocity[Y]                                      0.15763E-03 
c  Velocity[Z]                                      0.10367E-30 
c  Pressure     0.30971E-04     174   0.47373E-02   0.28139E+00 0.66905E-01 
c  k            0.36789E-07      42   0.37569E-04   0.42227E-09 0.64759E+00 
c  epsilon      0.12028E-05      29   0.15333E-04   0.17570E-06 0.67880E+00 
c  TempC        0.20138E+01      92   0.99182E-02   0.37616E+00 0.38466E-01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.0904e-11                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.10311         0.10293      0.00012575      1.3959e-06
v  Velocity[Y]          -0.074187         0.17005       0.0039725      0.00066539
v  Velocity[Z]        -6.6122e-15      5.2421e-15      4.4587e-18     -6.7848e-18
v  ǁVelocityǁ          0.00048011         0.17816        0.045897        0.045444
v  Pressure             -0.047664        0.060253     -7.7023e-05      6.6411e-18
v  k                   1.7146e-21      0.00023444      1.3136e-05      1.2066e-05
v  epsilon             1.7092e-15       0.0053041      0.00024829      0.00021899
v  TempC                   20.328          29.689          22.577           22.42
v  Density                  1.167          1.2036          1.1953          1.1959
v  TurbVisc            6.2531e-34      1.1077e-06      7.0909e-08      6.8033e-08
v  CourantNb             0.025389          9.5832          3.0711          2.9742
v  FourierNb              0.41732          2.6783         0.88517         0.83152
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  TempC                     20.324              30           22.75          22.939
v  Boundary Density           1.167          1.2036          1.1942          1.1939
v  Yplus                          0          4.5731         0.13967         0.27352


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44373          11.804          3.9562          3.8057


 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         0.871558852E-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 0.31995E-01
   Friction velocity        uet   :  0.12376E-02 0.19747E-01
   Friction velocity        uk    :  0.12376E-02 0.30520E-01
   Dimensionless distance   yplus :  0.15950E+00 0.47821E+01
   Friction thermal sca.    tstar : -0.17265E+02-0.31082E+00
   Rough dim-less th. sca.  tplus :  0.11900E+00 0.35680E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        105
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62406E-05     103   0.10114E+00   0.23813E-03 0.33732E+00 
c  Velocity[X]                                      0.91789E-04 
c  Velocity[Y]                                      0.14634E-03 
c  Velocity[Z]                                      0.81730E-31 
c  Pressure     0.29688E-04     174   0.47550E-02   0.23231E+00 0.85548E-01 
c  k            0.42796E-07      48   0.14783E-04   0.23677E-09 0.42821E+00 
c  epsilon      0.14166E-05      31   0.51360E-05   0.92938E-07 0.43536E+00 
c  TempC        0.20259E+01     107   0.11248E-01   0.40308E+00 0.39488E-01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.3611e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.11756         0.11716      0.00018496      1.0182e-06
v  Velocity[Y]          -0.086162         0.18343       0.0044852      0.00084474
v  Velocity[Z]        -6.6086e-15      4.9864e-15     -3.1969e-19     -9.6463e-18
v  ǁVelocityǁ           0.0005385         0.19121        0.052555        0.052135
v  Pressure             -0.045424        0.060676     -0.00017408     -3.1731e-18
v  k                   3.1862e-19      0.00027805      1.4955e-05      1.3993e-05
v  epsilon             1.2544e-12       0.0054516      0.00028439      0.00025605
v  TempC                    20.33          29.735          22.758          22.604
v  Density                 1.1664          1.2036          1.1945          1.1952
v  TurbVisc            9.3753e-31      1.3973e-06      8.4366e-08       8.142e-08
v  CourantNb              0.04058          13.539          3.7079          3.5959
v  FourierNb              0.41731           2.678         0.88746         0.83404
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  TempC                     20.328              30          22.928          23.109
v  Boundary Density          1.1664          1.2036          1.1935          1.1931
v  Yplus                          0          4.7821         0.14624         0.28776


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53849           15.76          4.5954          4.4299


 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         0.117211493E-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 0.31898E-01
   Friction velocity        uet   :  0.11699E-02 0.20980E-01
   Friction velocity        uk    :  0.11696E-02 0.31380E-01
   Dimensionless distance   yplus :  0.15076E+00 0.49072E+01
   Friction thermal sca.    tstar : -0.77940E+01-0.20927E+00
   Rough dim-less th. sca.  tplus :  0.11248E+00 0.36614E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        100
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69063E-05     116   0.13113E+00   0.21282E-03 0.29196E+00 
c  Velocity[X]                                      0.81537E-04 
c  Velocity[Y]                                      0.13128E-03 
c  Velocity[Z]                                      0.66804E-31 
c  Pressure     0.29116E-04     172   0.58500E-02   0.19948E+00 0.10801E+00 
c  k            0.47983E-07      55   0.15678E-04   0.10859E-09 0.26576E+00 
c  epsilon      0.15885E-05      37   0.54609E-05   0.42131E-07 0.26970E+00 
c  TempC        0.20376E+01     117   0.13913E-01   0.39549E+00 0.38800E-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]           -0.12626         0.12624       0.0002422     -2.4023e-06
v  Velocity[Y]          -0.096044          0.1913       0.0049789      0.00094957
v  Velocity[Z]        -6.8256e-15       4.762e-15     -3.2231e-18     -1.2127e-17
v  ǁVelocityǁ          0.00098225         0.19779        0.058056        0.057661
v  Pressure             -0.043985        0.060823     -0.00028042      4.9141e-18
v  k                   1.4021e-18      0.00032743      1.6116e-05      1.5295e-05
v  epsilon             2.8142e-11       0.0059038      0.00030518        0.000279
v  TempC                   20.333          29.836          22.929          22.785
v  Density                 1.1662          1.2036          1.1938          1.1944
v  TurbVisc            3.4638e-28      1.6413e-06      9.5707e-08      9.3336e-08
v  CourantNb             0.042787          15.394          4.2851          4.1572
v  FourierNb              0.41742           2.669         0.88798          0.8344
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  TempC                      20.33              30            23.1          23.276
v  Boundary Density          1.1662          1.2036          1.1928          1.1925
v  Yplus                          0          4.9072         0.15034         0.29638


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58497          17.607          5.1731          4.9916


 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         0.105804026E-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 0.31840E-01
   Friction velocity        uet   :  0.54542E-03 0.21586E-01
   Friction velocity        uk    :  0.54540E-03 0.31791E-01
   Dimensionless distance   yplus :  0.70547E-01 0.49476E+01
   Friction thermal sca.    tstar : -0.27013E+02-0.12299E+00
   Rough dim-less th. sca.  tplus :  0.52636E-01 0.36915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         93
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74297E-05     124   0.14776E+00   0.18269E-03 0.25555E+00 
c  Velocity[X]                                      0.69951E-04 
c  Velocity[Y]                                      0.11274E-03 
c  Velocity[Z]                                      0.68052E-31 
c  Pressure     0.27742E-04     171   0.59348E-02   0.17129E+00 0.12518E+00 
c  k            0.52027E-07      58   0.88300E-05   0.86940E-10 0.22129E+00 
c  epsilon      0.17033E-05      38   0.27281E-05   0.29207E-07 0.21187E+00 
c  TempC        0.20494E+01     122   0.14472E-01   0.36558E+00 0.37011E-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]           -0.13112         0.13072      0.00029428     -6.7117e-07
v  Velocity[Y]           -0.10361         0.19554       0.0054021      0.00097898
v  Velocity[Z]        -6.9577e-15      4.5749e-15      -5.209e-18     -1.4651e-17
v  ǁVelocityǁ          0.00014079         0.19812        0.062092        0.061747
v  Pressure             -0.041871        0.060568     -0.00037617      -1.404e-18
v  k                   1.6497e-17      0.00037354      1.7109e-05      1.6427e-05
v  epsilon              1.543e-11       0.0066495      0.00032003      0.00029633
v  TempC                   20.336          29.815           23.09          22.965
v  Density                 1.1658          1.2036          1.1931          1.1937
v  TurbVisc            2.4083e-27      1.9298e-06      1.0448e-07      1.0286e-07
v  CourantNb             0.057411          16.451          4.7834          4.6435
v  FourierNb              0.41742          2.6566         0.89002         0.83618
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  TempC                     20.333              30          23.263          23.441
v  Boundary Density          1.1658          1.2036          1.1921          1.1918
v  Yplus                          0          4.9476         0.15227         0.30034


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56643          17.646          5.6734          5.4797


 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         0.116318138E-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   :  0.24877E-02 0.21567E-01
   Friction velocity        uk    :  0.24877E-02 0.31721E-01
   Dimensionless distance   yplus :  0.39747E+00 0.49464E+01
   Friction thermal sca.    tstar : -0.92367E+01-0.15040E+00
   Rough dim-less th. sca.  tplus :  0.29655E+00 0.36906E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         94
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77835E-05     130   0.16721E+00   0.16308E-03 0.23416E+00 
c  Velocity[X]                                      0.61135E-04 
c  Velocity[Y]                                      0.10195E-03 
c  Velocity[Z]                                      0.54901E-31 
c  Pressure     0.25297E-04     169   0.53841E-02   0.14638E+00 0.13245E+00 
c  k            0.54652E-07      61   0.93025E-05   0.83017E-10 0.20536E+00 
c  epsilon      0.17534E-05      39   0.28952E-05   0.28485E-07 0.20272E+00 
c  TempC        0.20614E+01     124   0.15268E-01   0.32221E+00 0.34479E-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]           -0.13468         0.13266      0.00033139      5.5042e-07
v  Velocity[Y]           -0.10967         0.19578       0.0057134      0.00094156
v  Velocity[Z]        -6.7196e-15      4.3587e-15     -8.1834e-18      -1.799e-17
v  ǁVelocityǁ          0.00078958         0.19613         0.06468        0.064409
v  Pressure             -0.039036        0.059971     -0.00044526      4.0015e-18
v  k                   5.9247e-17      0.00041466      1.7753e-05      1.7188e-05
v  epsilon             1.3555e-10       0.0072175      0.00032756      0.00030609
v  TempC                   20.337          29.809          23.248          23.144
v  Density                 1.1659          1.2036          1.1925           1.193
v  TurbVisc            1.8234e-25      2.2329e-06       1.134e-07      1.1256e-07
v  CourantNb             0.023486          17.905           5.182          5.0323
v  FourierNb              0.41727          2.6484         0.89073         0.83734
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  TempC                     20.336              30          23.417          23.604
v  Boundary Density          1.1659          1.2036          1.1915          1.1911
v  Yplus                          0          4.9464         0.15356         0.30253


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64539          19.102          6.0727          5.8696


 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         0.641561283E-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 0.32068E-01
   Friction velocity        uet   :  0.49446E-03 0.21517E-01
   Friction velocity        uk    :  0.49446E-03 0.32183E-01
   Dimensionless distance   yplus :  0.64264E-01 0.49260E+01
   Friction thermal sca.    tstar : -0.59581E+02-0.22178E+00
   Rough dim-less th. sca.  tplus :  0.47948E-01 0.36754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         91
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79791E-05     136   0.17507E+00   0.15630E-03 0.22684E+00 
c  Velocity[X]                                      0.58580E-04 
c  Velocity[Y]                                      0.97719E-04 
c  Velocity[Z]                                      0.46756E-31 
c  Pressure     0.23897E-04     167   0.47954E-02   0.13471E+00 0.13332E+00 
c  k            0.55831E-07      62   0.75286E-05   0.50343E-10 0.15514E+00 
c  epsilon      0.17492E-05      39   0.22356E-05   0.19531E-07 0.16650E+00 
c  TempC        0.20734E+01     123   0.16548E-01   0.28473E+00 0.32166E-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]            -0.1343          0.1328      0.00034144      6.7135e-07
v  Velocity[Y]           -0.11217          0.1943       0.0058925      0.00085745
v  Velocity[Z]        -6.4619e-15      4.2347e-15     -1.2354e-17     -2.2463e-17
v  ǁVelocityǁ          0.00061482         0.19435        0.065987        0.065782
v  Pressure             -0.035727        0.059097     -0.00048302     -1.2075e-18
v  k                   7.9418e-17      0.00044344      1.8067e-05      1.7603e-05
v  epsilon             1.7329e-12       0.0075346      0.00032576      0.00030702
v  TempC                   20.341           29.82          23.404          23.323
v  Density                 1.1659          1.2036          1.1918          1.1922
v  TurbVisc            2.6249e-24       2.533e-06      1.2053e-07      1.2044e-07
v  CourantNb              0.08104          19.028          5.4705          5.3172
v  FourierNb              0.41693          2.6471         0.89146         0.83869
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  TempC                     20.337              30          23.567          23.767
v  Boundary Density          1.1659          1.2036          1.1909          1.1905
v  Yplus                          0           4.926         0.15275         0.30068


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72047          20.638           6.362          6.1559


 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         0.135856144E-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 0.32042E-01
   Friction velocity        uet   :  0.20463E-02 0.21361E-01
   Friction velocity        uk    :  0.20394E-02 0.32141E-01
   Dimensionless distance   yplus :  0.29060E+00 0.48992E+01
   Friction thermal sca.    tstar : -0.63506E+01-0.18550E+00
   Rough dim-less th. sca.  tplus :  0.21682E+00 0.36553E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         84
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80291E-05     138   0.18173E+00   0.14439E-03 0.21914E+00 
c  Velocity[X]                                      0.56342E-04 
c  Velocity[Y]                                      0.88050E-04 
c  Velocity[Z]                                      0.38386E-31 
c  Pressure     0.24106E-04     166   0.45683E-02   0.13653E+00 0.13263E+00 
c  k            0.55592E-07      63   0.91429E-05   0.40370E-10 0.13773E+00 
c  epsilon      0.17072E-05      40   0.26301E-05   0.17723E-07 0.16007E+00 
c  TempC        0.20854E+01     121   0.15755E-01   0.26209E+00 0.30632E-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]           -0.13042         0.12923      0.00033024     -2.2006e-06
v  Velocity[Y]           -0.11348         0.19009       0.0059028      0.00077191
v  Velocity[Z]        -6.2633e-15      3.9633e-15      -1.722e-17     -2.8169e-17
v  ǁVelocityǁ          0.00097079         0.19011        0.065976        0.065874
v  Pressure             -0.033506         0.05796     -0.00049492     -4.0577e-18
v  k                   9.2603e-17      0.00045511      1.8246e-05      1.7817e-05
v  epsilon             7.5781e-11       0.0074985      0.00032325      0.00030528
v  TempC                   20.325           29.83          23.563            23.5
v  Density                 1.1659          1.2035          1.1912          1.1915
v  TurbVisc            5.1898e-24      2.7809e-06      1.2669e-07      1.2719e-07
v  CourantNb             0.026662          20.584          5.6508           5.498
v  FourierNb              0.41644          2.6502         0.89154         0.83787
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  TempC                     20.341              30          23.716           23.93
v  Boundary Density          1.1659          1.2035          1.1903          1.1898
v  Yplus                          0          4.8992          0.1513         0.29757


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51735          22.193          6.5424          6.3359


 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         0.132427480E-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 0.32025E-01
   Friction velocity        uet   :  0.15910E-02 0.20961E-01
   Friction velocity        uk    :  0.15676E-02 0.31761E-01
   Dimensionless distance   yplus :  0.21192E+00 0.48514E+01
   Friction thermal sca.    tstar : -0.14969E+02-0.18846E+00
   Rough dim-less th. sca.  tplus :  0.15811E+00 0.36197E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         93
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79345E-05     138   0.17549E+00   0.12542E-03 0.20811E+00 
c  Velocity[X]                                      0.53787E-04 
c  Velocity[Y]                                      0.71635E-04 
c  Velocity[Z]                                      0.33269E-31 
c  Pressure     0.25555E-04     169   0.45750E-02   0.14820E+00 0.13199E+00 
c  k            0.54067E-07      62   0.86046E-05   0.11154E-09 0.23233E+00 
c  epsilon      0.16438E-05      40   0.21504E-05   0.37625E-07 0.23850E+00 
c  TempC        0.20971E+01     120   0.15750E-01   0.23778E+00 0.28963E-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]           -0.12657          0.1246      0.00031813     -6.3346e-06
v  Velocity[Y]           -0.11331         0.18748       0.0057374      0.00069731
v  Velocity[Z]        -6.0576e-15      3.5494e-15     -2.3739e-17     -3.5004e-17
v  ǁVelocityǁ          0.00041667          0.1875         0.06466        0.064727
v  Pressure             -0.032755         0.05658     -0.00048679      2.2745e-18
v  k                   9.7219e-17      0.00044276      1.8181e-05      1.7735e-05
v  epsilon             1.3656e-10       0.0071311      0.00032198      0.00030273
v  TempC                   20.331          29.853          23.727          23.677
v  Density                 1.1658          1.2036          1.1906          1.1908
v  TurbVisc            4.9348e-24      2.9299e-06      1.3248e-07      1.3341e-07
v  CourantNb             0.014838          21.732          5.7103          5.5648
v  FourierNb               0.4159          2.6541         0.89251         0.83936
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  TempC                     20.325              30          23.868          24.091
v  Boundary Density          1.1658          1.2036          1.1897          1.1892
v  Yplus                          0          4.8514         0.14963         0.29429


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49071          23.339          6.6028          6.4042


 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         0.117261124E-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 0.31960E-01
   Friction velocity        uet   :  0.10280E-02 0.20700E-01
   Friction velocity        uk    :  0.10273E-02 0.31115E-01
   Dimensionless distance   yplus :  0.13234E+00 0.48205E+01
   Friction thermal sca.    tstar : -0.10819E+02-0.16732E+00
   Rough dim-less th. sca.  tplus :  0.98737E-01 0.35966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         98
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77744E-05     138   0.17682E+00   0.10165E-03 0.19290E+00 
c  Velocity[X]                                      0.45874E-04 
c  Velocity[Y]                                      0.55778E-04 
c  Velocity[Z]                                      0.28069E-31 
c  Pressure     0.25356E-04     170   0.48284E-02   0.15194E+00 0.13941E+00 
c  k            0.51807E-07      59   0.93482E-05   0.68620E-10 0.18891E+00 
c  epsilon      0.15658E-05      38   0.21449E-05   0.27263E-07 0.21182E+00 
c  TempC        0.21081E+01     117   0.16506E-01   0.21257E+00 0.27186E-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]           -0.11757         0.11804      0.00029788     -1.0121e-05
v  Velocity[Y]           -0.11114         0.18447       0.0054638       0.0006486
v  Velocity[Z]        -5.7897e-15      3.5556e-15      -2.996e-17     -4.2267e-17
v  ǁVelocityǁ          0.00063757         0.18516        0.062434        0.062716
v  Pressure             -0.031243        0.054864     -0.00047031     -1.5444e-19
v  k                   1.4697e-16      0.00041282      1.7654e-05      1.7268e-05
v  epsilon             1.5723e-10       0.0065176      0.00030857      0.00029076
v  TempC                   20.309          29.866          23.896          23.852
v  Density                 1.1657          1.2036          1.1899          1.1901
v  TurbVisc            6.5629e-24      2.9223e-06      1.3473e-07      1.3605e-07
v  CourantNb             0.017306          22.623          5.6459           5.516
v  FourierNb              0.41552          2.6601         0.88993         0.83702
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  TempC                     20.331              30          24.024          24.251
v  Boundary Density          1.1657          1.2036          1.1891          1.1885
v  Yplus                          0          4.8205         0.14731         0.29014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47047          24.229          6.5358           6.353


 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         0.114159196E-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 0.31937E-01
   Friction velocity        uet   :  0.18700E-02 0.20476E-01
   Friction velocity        uk    :  0.18587E-02 0.30875E-01
   Dimensionless distance   yplus :  0.23983E+00 0.47668E+01
   Friction thermal sca.    tstar : -0.79801E+01-0.17136E+00
   Rough dim-less th. sca.  tplus :  0.17894E+00 0.35566E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        103
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75353E-05     137   0.17698E+00   0.94895E-04 0.19370E+00 
c  Velocity[X]                                      0.41584E-04 
c  Velocity[Y]                                      0.53312E-04 
c  Velocity[Z]                                      0.24614E-31 
c  Pressure     0.25116E-04     171   0.49876E-02   0.15577E+00 0.14685E+00 
c  k            0.49331E-07      56   0.93475E-05   0.77056E-10 0.20927E+00 
c  epsilon      0.14873E-05      37   0.19746E-05   0.23454E-07 0.20576E+00 
c  TempC        0.21185E+01     113   0.17186E-01   0.18058E+00 0.24878E-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]           -0.11007          0.1092      0.00028571      -1.107e-05
v  Velocity[Y]           -0.10756         0.18215       0.0051323      0.00061438
v  Velocity[Z]         -5.472e-15      3.4619e-15     -3.6051e-17     -4.9167e-17
v  ǁVelocityǁ          0.00023336         0.18362         0.05957         0.06007
v  Pressure             -0.029164        0.052876     -0.00045122     -2.1482e-18
v  k                   1.7854e-16      0.00037633      1.7053e-05      1.6704e-05
v  epsilon             1.7865e-10       0.0063858      0.00029544       0.0002785
v  TempC                   20.304          29.874          24.066          24.027
v  Density                 1.1657          1.2037          1.1892          1.1894
v  TurbVisc            7.5152e-24      2.7685e-06      1.3505e-07        1.37e-07
v  CourantNb             0.051914          22.535          5.4658          5.3591
v  FourierNb              0.41496          2.6659          0.8914         0.83874
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  TempC                     20.309              30          24.184          24.411
v  Boundary Density          1.1657          1.2037          1.1884          1.1879
v  Yplus                          0          4.7668         0.14483         0.28573


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47297           24.14          6.3572          6.1979


 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         0.826270714E-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 0.32032E-01
   Friction velocity        uet   :  0.75189E-03 0.20298E-01
   Friction velocity        uk    :  0.75176E-03 0.30608E-01
   Dimensionless distance   yplus :  0.11961E+00 0.47440E+01
   Friction thermal sca.    tstar : -0.16519E+02-0.16698E+00
   Rough dim-less th. sca.  tplus :  0.89240E-01 0.35396E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        111
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72482E-05     134   0.18037E+00   0.10754E-03 0.21612E+00 
c  Velocity[X]                                      0.40266E-04 
c  Velocity[Y]                                      0.67274E-04 
c  Velocity[Z]                                      0.23457E-31 
c  Pressure     0.25463E-04     169   0.49830E-02   0.16338E+00 0.15188E+00 
c  k            0.47106E-07      54   0.10135E-04   0.77994E-10 0.21977E+00 
c  epsilon      0.14170E-05      35   0.19143E-05   0.23211E-07 0.21391E+00 
c  TempC        0.21288E+01     108   0.14944E-01   0.14917E+00 0.22452E-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]           -0.10414         0.10154      0.00027026     -1.5905e-05
v  Velocity[Y]           -0.10278         0.18065       0.0047438      0.00059132
v  Velocity[Z]        -5.1153e-15      3.2186e-15      -4.161e-17     -5.5292e-17
v  ǁVelocityǁ          0.00014157         0.18322         0.05632        0.057007
v  Pressure             -0.027897        0.050749     -0.00043043     -1.5444e-18
v  k                   1.4449e-16      0.00037566      1.6421e-05      1.6113e-05
v  epsilon             1.8586e-10       0.0063622      0.00028211      0.00026623
v  TempC                   20.376          29.872          24.235            24.2
v  Density                 1.1657          1.2037          1.1885          1.1887
v  TurbVisc            5.8778e-24      2.4872e-06      1.3457e-07      1.3699e-07
v  CourantNb            0.0048626          21.435          5.2012          5.1195
v  FourierNb              0.41445          2.6707         0.89602         0.84375
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  TempC                     20.304              30          24.346           24.57
v  Boundary Density          1.1657          1.2037          1.1878          1.1872
v  Yplus                          0           4.744         0.14248         0.28137


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46632           23.04          6.0972          5.9633


 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         0.835617855E-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 0.31982E-01
   Friction velocity        uet   :  0.11441E-02 0.20618E-01
   Friction velocity        uk    :  0.11429E-02 0.30439E-01
   Dimensionless distance   yplus :  0.14731E+00 0.47392E+01
   Friction thermal sca.    tstar : -0.12975E+02-0.18349E+00
   Rough dim-less th. sca.  tplus :  0.10991E+00 0.35360E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        118
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68728E-05     128   0.17164E+00   0.14280E-03 0.26217E+00 
c  Velocity[X]                                      0.45390E-04 
c  Velocity[Y]                                      0.97410E-04 
c  Velocity[Z]                                      0.24788E-31 
c  Pressure     0.25084E-04     167   0.48889E-02   0.16557E+00 0.15162E+00 
c  k            0.45290E-07      51   0.11145E-04   0.56969E-10 0.19487E+00 
c  epsilon      0.13584E-05      33   0.20319E-05   0.17441E-07 0.19265E+00 
c  TempC        0.21389E+01     101   0.13491E-01   0.12862E+00 0.20705E-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]          -0.097674         0.09783      0.00025809     -1.8659e-05
v  Velocity[Y]          -0.096058         0.17842       0.0043151      0.00058084
v  Velocity[Z]        -4.4651e-15      3.1162e-15     -4.6641e-17     -6.0371e-17
v  ǁVelocityǁ            0.000491         0.18244        0.052841        0.053667
v  Pressure             -0.026736        0.048669     -0.00040946      2.3447e-18
v  k                   1.1007e-16       0.0003764      1.5787e-05      1.5533e-05
v  epsilon             1.2818e-10       0.0063728      0.00026902      0.00025442
v  TempC                   20.413          29.861          24.402           24.37
v  Density                 1.1657          1.2034          1.1879           1.188
v  TurbVisc            4.0641e-24      2.3812e-06      1.3362e-07      1.3657e-07
v  CourantNb             0.003458          20.269           4.888          4.8294
v  FourierNb              0.41442          2.6744         0.89393         0.84122
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  TempC                     20.376              30          24.508          24.727
v  Boundary Density          1.1657          1.2034          1.1871          1.1866
v  Yplus                          0          4.7392         0.14007         0.27707


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42529          21.559          5.7819          5.6706


 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         0.833632621E-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 0.31950E-01
   Friction velocity        uet   :  0.35874E-03 0.20318E-01
   Friction velocity        uk    :  0.35873E-03 0.30670E-01
   Dimensionless distance   yplus :  0.46599E-01 0.47298E+01
   Friction thermal sca.    tstar : -0.77672E+02-0.16868E+00
   Rough dim-less th. sca.  tplus :  0.34768E-01 0.35290E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        121
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65731E-05     119   0.17501E+00   0.18825E-03 0.31590E+00 
c  Velocity[X]                                      0.52829E-04 
c  Velocity[Y]                                      0.13542E-03 
c  Velocity[Z]                                      0.24030E-31 
c  Pressure     0.24360E-04     166   0.47926E-02   0.16524E+00 0.14468E+00 
c  k            0.43895E-07      48   0.11838E-04   0.39767E-10 0.16752E+00 
c  epsilon      0.13120E-05      32   0.21686E-05   0.14412E-07 0.18051E+00 
c  TempC        0.21492E+01      96   0.12997E-01   0.12882E+00 0.20583E-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]          -0.095552        0.095854      0.00024823     -2.4291e-05
v  Velocity[Y]           -0.10203         0.17543       0.0038341      0.00058741
v  Velocity[Z]        -3.6383e-15       3.467e-15     -5.1394e-17     -6.4927e-17
v  ǁVelocityǁ          0.00055635         0.18132        0.049701        0.050603
v  Pressure             -0.025725        0.046785     -0.00039222      1.5866e-18
v  k                   7.4704e-17      0.00037702      1.5309e-05      1.5073e-05
v  epsilon              2.956e-11       0.0063757      0.00025835      0.00024465
v  TempC                   20.475          29.854          24.566          24.537
v  Density                 1.1657          1.2032          1.1872          1.1873
v  TurbVisc            2.6796e-24      2.3886e-06      1.3249e-07      1.3606e-07
v  CourantNb             0.018839          18.683          4.5461          4.5064
v  FourierNb              0.41386          2.6772         0.89417         0.84114
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  TempC                     20.413              30          24.667          24.882
v  Boundary Density          1.1657          1.2032          1.1865           1.186
v  Yplus                          0          4.7298          0.1379          0.2731


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45259           20.28          5.4403          5.3475


 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         0.670347168E-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 0.31981E-01
   Friction velocity        uet   :  0.16973E-02 0.20102E-01
   Friction velocity        uk    :  0.16950E-02 0.31222E-01
   Dimensionless distance   yplus :  0.24334E+00 0.47148E+01
   Friction thermal sca.    tstar : -0.15763E+02-0.19988E+00
   Rough dim-less th. sca.  tplus :  0.18156E+00 0.35178E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        121
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63200E-05     118   0.17510E+00   0.23474E-03 0.36706E+00 
c  Velocity[X]                                      0.62752E-04 
c  Velocity[Y]                                      0.17199E-03 
c  Velocity[Z]                                      0.33148E-31 
c  Pressure     0.24301E-04     167   0.48069E-02   0.16898E+00 0.13981E+00 
c  k            0.42797E-07      49   0.14810E-04   0.30642E-10 0.15023E+00 
c  epsilon      0.12748E-05      36   0.28994E-05   0.12797E-07 0.17430E+00 
c  TempC        0.21592E+01      96   0.13268E-01   0.15332E+00 0.22312E-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]          -0.092234        0.093657      0.00025063     -2.4413e-05
v  Velocity[Y]           -0.10613         0.17143       0.0032882       0.0006102
v  Velocity[Z]        -2.6384e-15      3.5277e-15     -5.5913e-17     -6.8815e-17
v  ǁVelocityǁ          0.00036217         0.17972        0.047675        0.048515
v  Pressure              -0.02476        0.045132     -0.00038031       1.755e-19
v  k                   2.7877e-17      0.00037575      1.4995e-05      1.4767e-05
v  epsilon             9.2782e-11       0.0063732      0.00025029      0.00023718
v  TempC                   20.567          29.872          24.727          24.698
v  Density                 1.1657           1.203          1.1865          1.1867
v  TurbVisc            2.5701e-24      2.3986e-06      1.3217e-07      1.3617e-07
v  CourantNb             0.022632          17.175          4.2322          4.2026
v  FourierNb              0.41394          2.6797         0.89364         0.84121
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  TempC                     20.475              30          24.824          25.033
v  Boundary Density          1.1657           1.203          1.1859          1.1853
v  Yplus                          0          4.7148          0.1355          0.2686


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44423          18.769          5.1258          5.0438


 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         0.432708518E-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 0.31897E-01
   Friction velocity        uet   :  0.12885E-02 0.19966E-01
   Friction velocity        uk    :  0.12885E-02 0.31859E-01
   Dimensionless distance   yplus :  0.16718E+00 0.46920E+01
   Friction thermal sca.    tstar : -0.18949E+02-0.16201E+00
   Rough dim-less th. sca.  tplus :  0.12474E+00 0.35008E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        123
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61427E-05     121   0.17245E+00   0.26132E-03 0.39716E+00 
c  Velocity[X]                                      0.69766E-04 
c  Velocity[Y]                                      0.19156E-03 
c  Velocity[Z]                                      0.37646E-31 
c  Pressure     0.22965E-04     170   0.46776E-02   0.16308E+00 0.15522E+00 
c  k            0.41781E-07      48   0.17970E-04   0.32204E-10 0.15706E+00 
c  epsilon      0.12421E-05      35   0.34601E-05   0.12270E-07 0.17442E+00 
c  TempC        0.21687E+01      97   0.11453E-01   0.20269E+00 0.25495E-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]          -0.089842        0.089808      0.00025168     -2.1238e-05
v  Velocity[Y]           -0.11036         0.16593       0.0027079      0.00065348
v  Velocity[Z]         -2.622e-15      3.1421e-15     -6.0407e-17     -7.2463e-17
v  ǁVelocityǁ          0.00069584         0.17608        0.046608        0.047274
v  Pressure             -0.023825         0.04356     -0.00037398      1.6427e-18
v  k                    3.319e-17      0.00036777      1.4705e-05      1.4484e-05
v  epsilon             7.8627e-11       0.0061962      0.00024408      0.00023139
v  TempC                     20.5          29.885          24.884          24.854
v  Density                 1.1657          1.2026          1.1859           1.186
v  TurbVisc            6.4557e-26      2.3935e-06      1.3285e-07      1.3719e-07
v  CourantNb             0.017445          15.637          4.0372          4.0016
v  FourierNb              0.41379          2.6821         0.89441         0.84188
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  TempC                     20.567              30          24.976           25.18
v  Boundary Density          1.1657          1.2026          1.1852          1.1847
v  Yplus                          0           4.692         0.13336         0.26474


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43889          16.758          4.9316          4.8435


 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         0.659481376E-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 0.32075E-01
   Friction velocity        uet   :  0.17592E-02 0.20249E-01
   Friction velocity        uk    :  0.17591E-02 0.31636E-01
   Dimensionless distance   yplus :  0.23989E+00 0.46559E+01
   Friction thermal sca.    tstar : -0.11354E+02-0.15297E+00
   Rough dim-less th. sca.  tplus :  0.17899E+00 0.34738E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        120
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60182E-05     121   0.17611E+00   0.26334E-03 0.40326E+00 
c  Velocity[X]                                      0.72269E-04 
c  Velocity[Y]                                      0.19107E-03 
c  Velocity[Z]                                      0.43749E-31 
c  Pressure     0.24009E-04     171   0.45600E-02   0.17390E+00 0.19857E+00 
c  k            0.40822E-07      47   0.19122E-04   0.30192E-10 0.15501E+00 
c  epsilon      0.12090E-05      33   0.28782E-05   0.12511E-07 0.18035E+00 
c  TempC        0.21785E+01      94   0.12861E-01   0.23580E+00 0.27337E-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]          -0.093777        0.091967      0.00025537     -1.2615e-05
v  Velocity[Y]           -0.11187         0.15848       0.0020956      0.00068258
v  Velocity[Z]         -3.274e-15      3.1198e-15     -6.4567e-17     -7.6124e-17
v  ǁVelocityǁ          0.00032603         0.17088        0.046106        0.046711
v  Pressure              -0.02236        0.041652     -0.00036524      -9.056e-19
v  k                   9.0496e-18      0.00035813      1.4393e-05      1.4189e-05
v  epsilon             2.0508e-10       0.0060641       0.0002372      0.00022512
v  TempC                   20.274          29.871          25.037          25.006
v  Density                 1.1656          1.2029          1.1853          1.1854
v  TurbVisc            2.5765e-25      2.3628e-06      1.3298e-07      1.3759e-07
v  CourantNb             0.031859          15.888          3.9322          3.8795
v  FourierNb              0.41381          2.6846         0.89484         0.84201
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  TempC                       20.5              30          25.126          25.322
v  Boundary Density          1.1656          1.2029          1.1846          1.1841
v  Yplus                          0          4.6559         0.13295           0.264


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48019          16.937          4.8271          4.7215


 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         0.897077374E-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 0.32165E-01
   Friction velocity        uet   :  0.41737E-03 0.20209E-01
   Friction velocity        uk    :  0.41646E-03 0.30964E-01
   Dimensionless distance   yplus :  0.65968E-01 0.45930E+01
   Friction thermal sca.    tstar : -0.14628E+02-0.15598E+00
   Rough dim-less th. sca.  tplus :  0.49220E-01 0.34269E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        117
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58988E-05     115   0.17242E+00   0.24484E-03 0.39084E+00 
c  Velocity[X]                                      0.70940E-04 
c  Velocity[Y]                                      0.17390E-03 
c  Velocity[Z]                                      0.41064E-31 
c  Pressure     0.24717E-04     173   0.51472E-02   0.18312E+00 0.24517E+00 
c  k            0.39718E-07      48   0.21989E-04   0.53111E-10 0.20982E+00 
c  epsilon      0.11649E-05      33   0.31347E-05   0.18033E-07 0.22315E+00 
c  TempC        0.21874E+01      93   0.13032E-01   0.26081E+00 0.28586E-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]          -0.097674        0.096882      0.00026251      -1.543e-06
v  Velocity[Y]           -0.12821         0.14844        0.001552      0.00069603
v  Velocity[Z]        -3.7189e-15      3.1274e-15     -6.7512e-17     -7.8887e-17
v  ǁVelocityǁ           0.0006657         0.16262        0.045683        0.046368
v  Pressure             -0.020375        0.039376     -0.00035091      1.0249e-18
v  k                   8.7662e-16      0.00034182      1.4105e-05      1.3925e-05
v  epsilon             6.0892e-10       0.0057783      0.00023012      0.00021918
v  TempC                   20.735          29.885          25.189          25.153
v  Density                 1.1657          1.2038          1.1847          1.1848
v  TurbVisc            4.2194e-26      2.2969e-06      1.3256e-07      1.3735e-07
v  CourantNb             0.082495          16.651          3.8803          3.8191
v  FourierNb              0.41401          2.6878         0.89403           0.841
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  TempC                     20.274              30          25.272           25.46
v  Boundary Density          1.1657          1.2038           1.184          1.1836
v  Yplus                          0           4.593         0.13219          0.2627


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53895          17.705          4.7743          4.6601


 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         0.696982384E-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 0.32147E-01
   Friction velocity        uet   :  0.95860E-03 0.20400E-01
   Friction velocity        uk    :  0.95859E-03 0.29819E-01
   Dimensionless distance   yplus :  0.12372E+00 0.44907E+01
   Friction thermal sca.    tstar : -0.10726E+02-0.12522E+00
   Rough dim-less th. sca.  tplus :  0.92312E-01 0.33505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        126
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57710E-05     107   0.16035E+00   0.20980E-03 0.36462E+00 
c  Velocity[X]                                      0.65571E-04 
c  Velocity[Y]                                      0.14423E-03 
c  Velocity[Z]                                      0.36817E-31 
c  Pressure     0.25109E-04     172   0.56177E-02   0.19156E+00 0.29213E+00 
c  k            0.38303E-07      49   0.23278E-04   0.92700E-10 0.28499E+00 
c  epsilon      0.11114E-05      33   0.48007E-05   0.26178E-07 0.27886E+00 
c  TempC        0.21963E+01      94   0.12525E-01   0.25512E+00 0.28116E-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]          -0.099044        0.099254      0.00027212      7.7867e-06
v  Velocity[Y]           -0.14098         0.14532       0.0011335      0.00069349
v  Velocity[Z]         -3.929e-15      3.0724e-15     -6.9761e-17     -8.0621e-17
v  ǁVelocityǁ          0.00051051         0.15676        0.045079        0.045949
v  Pressure             -0.018239        0.036694     -0.00033381       -6.95e-19
v  k                   2.8656e-15      0.00032523      1.3574e-05      1.3464e-05
v  epsilon             2.0733e-10         0.00533      0.00022201      0.00021202
v  TempC                   20.898          29.885          25.337          25.297
v  Density                 1.1656          1.2019           1.184          1.1842
v  TurbVisc            2.3998e-23      2.2018e-06      1.3224e-07      1.3695e-07
v  CourantNb             0.067723          16.468          3.8419          3.7837
v  FourierNb              0.41447          2.6918         0.89433         0.84178
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  TempC                     20.735              30          25.417          25.594
v  Boundary Density          1.1656          1.2019          1.1834           1.183
v  Yplus                          0          4.4907         0.13054         0.26007


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52952          17.629          4.7363          4.6255


 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         0.331120399E-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 0.32060E-01
   Friction velocity        uet   :  0.16353E-02 0.20625E-01
   Friction velocity        uk    :  0.16353E-02 0.29024E-01
   Dimensionless distance   yplus :  0.25927E+00 0.43780E+01
   Friction thermal sca.    tstar : -0.14449E+02-0.10922E+00
   Rough dim-less th. sca.  tplus :  0.19345E+00 0.32665E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        138
   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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56205E-05     102   0.15805E+00   0.18336E-03 0.34676E+00 
c  Velocity[X]                                      0.60775E-04 
c  Velocity[Y]                                      0.12259E-03 
c  Velocity[Z]                                      0.27996E-31 
c  Pressure     0.25315E-04     172   0.54046E-02   0.20121E+00 0.30946E+00 
c  k            0.36756E-07      49   0.19648E-04   0.92213E-10 0.29441E+00 
c  epsilon      0.10533E-05      34   0.33495E-05   0.24893E-07 0.28487E+00 
c  TempC        0.22047E+01      92   0.12164E-01   0.23231E+00 0.26687E-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]          -0.098005        0.098476       0.0002958      1.2202e-05
v  Velocity[Y]           -0.14313         0.14118      0.00082633      0.00067259
v  Velocity[Z]        -3.6837e-15       2.978e-15     -7.1726e-17      -8.124e-17
v  ǁVelocityǁ          0.00022162         0.15154        0.044185        0.045266
v  Pressure             -0.016267         0.03391     -0.00031386     -3.7207e-19
v  k                    5.108e-15      0.00030105      1.2755e-05      1.2809e-05
v  epsilon             1.6461e-09       0.0048734      0.00020773      0.00020055
v  TempC                   21.043          29.881          25.482          25.437
v  Density                 1.1656          1.2013          1.1835          1.1836
v  TurbVisc            1.1028e-22      2.1037e-06      1.2961e-07      1.3465e-07
v  CourantNb             0.061325          17.541          3.7977          3.7537
v  FourierNb              0.41385           2.696         0.89698         0.84436
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  TempC                     20.898              30          25.558          25.724
v  Boundary Density          1.1656          1.2013          1.1829          1.1825
v  Yplus                          0           4.378         0.12779         0.25553


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48191          18.706          4.6947          4.5981


 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        -0.285790902E-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 0.31968E-01
   Friction velocity        uet   :  0.76591E-03 0.20451E-01
   Friction velocity        uk    :  0.76589E-03 0.28324E-01
   Dimensionless distance   yplus :  0.12141E+00 0.42918E+01
   Friction thermal sca.    tstar : -0.97205E+01-0.13210E+00
   Rough dim-less th. sca.  tplus :  0.90585E-01 0.32022E+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
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54298E-05     100   0.14823E+00   0.15904E-03 0.33227E+00 
c  Velocity[X]                                      0.53240E-04 
c  Velocity[Y]                                      0.10580E-03 
c  Velocity[Z]                                      0.20058E-31 
c  Pressure     0.24525E-04     172   0.52483E-02   0.20441E+00 0.30890E+00 
c  k            0.35179E-07      48   0.19300E-04   0.11001E-09 0.33268E+00 
c  epsilon      0.99846E-06      32   0.36597E-05   0.26109E-07 0.30454E+00 
c  TempC        0.22130E+01      85   0.11421E-01   0.20207E+00 0.24760E-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]          -0.095434        0.096736      0.00032514      1.5577e-05
v  Velocity[Y]           -0.13531         0.13579      0.00059034      0.00065074
v  Velocity[Z]        -3.1495e-15      3.0526e-15     -7.3247e-17     -8.1408e-17
v  ǁVelocityǁ          0.00048842         0.14594        0.042926        0.044182
v  Pressure             -0.014554        0.030948     -0.00029199     -4.9843e-19
v  k                   1.0185e-14      0.00028107      1.1965e-05      1.2196e-05
v  epsilon             3.1923e-10       0.0045129      0.00019475      0.00019037
v  TempC                   21.126          29.885          25.621          25.574
v  Density                 1.1656          1.2007          1.1829          1.1831
v  TurbVisc            2.7927e-22      1.9928e-06       1.249e-07      1.3093e-07
v  CourantNb              0.01805          17.127          3.7282          3.7027
v  FourierNb              0.41418          2.7002         0.89633         0.84445
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  TempC                     21.043              30          25.695          25.852
v  Boundary Density          1.1656          1.2007          1.1823           1.182
v  Yplus                          0          4.2918         0.12366         0.24868


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45077          18.296          4.6245          4.5472


 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         0.415234328E-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 0.31944E-01
   Friction velocity        uet   :  0.89493E-03 0.20434E-01
   Friction velocity        uk    :  0.89491E-03 0.27337E-01
   Dimensionless distance   yplus :  0.13021E+00 0.42040E+01
   Friction thermal sca.    tstar : -0.91627E+01-0.12772E+00
   Rough dim-less th. sca.  tplus :  0.97148E-01 0.31367E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        167
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52205E-05      97   0.15674E+00   0.13533E-03 0.31816E+00 
c  Velocity[X]                                      0.43301E-04 
c  Velocity[Y]                                      0.92029E-04 
c  Velocity[Z]                                      0.14883E-31 
c  Pressure     0.22734E-04     172   0.50716E-02   0.19819E+00 0.30626E+00 
c  k            0.33628E-07      46   0.18628E-04   0.50499E-10 0.23429E+00 
c  epsilon      0.94045E-06      31   0.33920E-05   0.17851E-07 0.26601E+00 
c  TempC        0.22209E+01      81   0.10540E-01   0.16509E+00 0.22270E-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]          -0.093647        0.094414      0.00036435      1.8152e-05
v  Velocity[Y]           -0.12287         0.12996      0.00041783      0.00062969
v  Velocity[Z]        -2.7468e-15      3.2807e-15     -7.3509e-17     -8.1354e-17
v  ǁVelocityǁ          0.00087371         0.14001         0.04145        0.042801
v  Pressure             -0.012983        0.027995     -0.00027542      3.3697e-19
v  k                   1.5075e-14      0.00026549      1.1152e-05      1.1511e-05
v  epsilon             2.7594e-10        0.004192      0.00017797      0.00017656
v  TempC                   21.199          29.888          25.758          25.705
v  Density                 1.1656          1.2003          1.1823          1.1825
v  TurbVisc            1.4965e-21      1.8744e-06      1.1995e-07      1.2715e-07
v  CourantNb            0.0031677          15.182          3.6331          3.6238
v  FourierNb              0.41419          2.7011         0.89338         0.84174
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  TempC                     21.126              30          25.829          25.976
v  Boundary Density          1.1656          1.2003          1.1818          1.1815
v  Yplus                          0           4.204         0.12033         0.24284


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49955          16.353          4.5265          4.4655


 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         0.354198738E-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 0.31912E-01
   Friction velocity        uet   :  0.10987E-02 0.20444E-01
   Friction velocity        uk    :  0.10987E-02 0.27197E-01
   Dimensionless distance   yplus :  0.14183E+00 0.41275E+01
   Friction thermal sca.    tstar : -0.78381E+01-0.13692E+00
   Rough dim-less th. sca.  tplus :  0.10582E+00 0.30796E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49878E-05      96   0.14704E+00   0.10881E-03 0.29670E+00 
c  Velocity[X]                                      0.33808E-04 
c  Velocity[Y]                                      0.75002E-04 
c  Velocity[Z]                                      0.14438E-31 
c  Pressure     0.20396E-04     172   0.47369E-02   0.18475E+00 0.30504E+00 
c  k            0.32059E-07      43   0.16483E-04   0.37144E-10 0.20880E+00 
c  epsilon      0.88113E-06      30   0.36551E-05   0.12029E-07 0.23077E+00 
c  TempC        0.22285E+01      79   0.85389E-02   0.13570E+00 0.20095E-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]          -0.093071        0.092544      0.00040082      1.1567e-05
v  Velocity[Y]            -0.1073         0.12417      0.00033182       0.0006216
v  Velocity[Z]        -3.0826e-15      3.6088e-15     -7.2347e-17     -8.0857e-17
v  ǁVelocityǁ          0.00075337         0.13418        0.039991        0.041335
v  Pressure             -0.011462        0.025262     -0.00026767     -3.3697e-19
v  k                   6.5637e-15      0.00025021      1.0449e-05      1.0904e-05
v  epsilon             8.8337e-10       0.0040288      0.00016313      0.00016439
v  TempC                   21.259          29.891           25.89          25.831
v  Density                 1.1656             1.2          1.1818           1.182
v  TurbVisc            1.3428e-21      1.7864e-06      1.1528e-07      1.2318e-07
v  CourantNb             0.013226          14.456          3.5196          3.5224
v  FourierNb              0.41465           2.698         0.89145         0.84028
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  TempC                     21.199              30          25.958          26.095
v  Boundary Density          1.1656             1.2          1.1813           1.181
v  Yplus                          0          4.1275         0.11862         0.23936


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54067          15.836           4.411          4.3627


 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         0.223669638E-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 0.31928E-01
   Friction velocity        uet   :  0.70035E-03 0.20400E-01
   Friction velocity        uk    :  0.70034E-03 0.26775E-01
   Dimensionless distance   yplus :  0.90391E-01 0.40863E+01
   Friction thermal sca.    tstar : -0.11393E+02-0.14747E+00
   Rough dim-less th. sca.  tplus :  0.67442E-01 0.30489E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47862E-05      95   0.14624E+00   0.86117E-04 0.27413E+00 
c  Velocity[X]                                      0.26118E-04 
c  Velocity[Y]                                      0.59999E-04 
c  Velocity[Z]                                      0.15732E-31 
c  Pressure     0.17599E-04     169   0.42878E-02   0.16443E+00 0.31208E+00 
c  k            0.30522E-07      41   0.13229E-04   0.36045E-10 0.21397E+00 
c  epsilon      0.82600E-06      28   0.27365E-05   0.10626E-07 0.22889E+00 
c  TempC        0.22356E+01      77   0.72776E-02   0.11064E+00 0.18063E-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]          -0.091002        0.089165      0.00043117      1.1797e-05
v  Velocity[Y]          -0.088216         0.12109      0.00034053      0.00062049
v  Velocity[Z]        -3.5388e-15      3.8079e-15     -7.0544e-17      -7.975e-17
v  ǁVelocityǁ          0.00024404         0.12693        0.038556        0.039832
v  Pressure             -0.010081        0.022841     -0.00026785      8.0732e-20
v  k                   3.7559e-15      0.00023858       9.821e-06      1.0331e-05
v  epsilon             9.7315e-10       0.0038432      0.00015103      0.00015387
v  TempC                    21.31          29.893           26.02          25.951
v  Density                 1.1656          1.1998          1.1813          1.1815
v  TurbVisc            7.1077e-22      1.7097e-06      1.1124e-07      1.1949e-07
v  CourantNb              0.03964           14.27          3.4063          3.4142
v  FourierNb              0.41566          2.6935         0.89372         0.84311
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  TempC                     21.259              30          26.085           26.21
v  Boundary Density          1.1656          1.1998          1.1807          1.1805
v  Yplus                          0          4.0863         0.11697         0.23566


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50245          15.652             4.3          4.2573


 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         0.280579664E-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 0.31900E-01
   Friction velocity        uet   :  0.70813E-03 0.20398E-01
   Friction velocity        uk    :  0.70812E-03 0.26048E-01
   Dimensionless distance   yplus :  0.11230E+00 0.40911E+01
   Friction thermal sca.    tstar : -0.40846E+02-0.14002E+00
   Rough dim-less th. sca.  tplus :  0.83788E-01 0.30524E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        193
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45954E-05      93   0.14937E+00   0.67238E-04 0.25063E+00 
c  Velocity[X]                                      0.20577E-04 
c  Velocity[Y]                                      0.46662E-04 
c  Velocity[Z]                                      0.19705E-31 
c  Pressure     0.15349E-04     169   0.41292E-02   0.14699E+00 0.32120E+00 
c  k            0.29017E-07      41   0.10010E-04   0.36774E-10 0.22571E+00 
c  epsilon      0.77475E-06      27   0.20763E-05   0.88919E-08 0.22161E+00 
c  TempC        0.22425E+01      75   0.57235E-02   0.96775E-01 0.16821E-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]          -0.087466        0.086092      0.00044748      1.0612e-05
v  Velocity[Y]          -0.079471         0.12239      0.00046002      0.00062435
v  Velocity[Z]        -3.6132e-15      3.7213e-15     -6.8542e-17     -7.8129e-17
v  ǁVelocityǁ          0.00062765          0.1264        0.037387        0.038591
v  Pressure            -0.0086491        0.020895     -0.00027443     -3.4399e-19
v  k                   2.1468e-15      0.00022776      9.1598e-06      9.7139e-06
v  epsilon             1.0338e-10       0.0036149      0.00013879      0.00014317
v  TempC                   21.362          29.894          26.146          26.066
v  Density                 1.1656          1.1996          1.1807           1.181
v  TurbVisc            8.8215e-22      1.6425e-06      1.0731e-07      1.1571e-07
v  CourantNb             0.030205          14.168          3.2935          3.3015
v  FourierNb              0.41619          2.6903         0.89043         0.83938
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  TempC                      21.31              30          26.208          26.319
v  Boundary Density          1.1656          1.1996          1.1802            1.18
v  Yplus                          0          4.0911         0.11419         0.22989


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4512           15.55          4.1839          4.1409


 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         0.494323134E-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 0.31711E-01
   Friction velocity        uet   :  0.30534E-03 0.20357E-01
   Friction velocity        uk    :  0.30534E-03 0.25699E-01
   Dimensionless distance   yplus :  0.48362E-01 0.40886E+01
   Friction thermal sca.    tstar : -0.97911E+01-0.14737E+00
   Rough dim-less th. sca.  tplus :  0.36084E-01 0.30505E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44212E-05      90   0.13287E+00   0.55313E-04 0.23452E+00 
c  Velocity[X]                                      0.16999E-04 
c  Velocity[Y]                                      0.38313E-04 
c  Velocity[Z]                                      0.20472E-31 
c  Pressure     0.13990E-04     170   0.40459E-02   0.13659E+00 0.32056E+00 
c  k            0.27678E-07      42   0.91631E-05   0.37595E-10 0.23748E+00 
c  epsilon      0.73053E-06      27   0.20870E-05   0.90530E-08 0.23541E+00 
c  TempC        0.22489E+01      75   0.56570E-02   0.87166E-01 0.15899E-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]          -0.083701        0.082438      0.00045088      1.1552e-05
v  Velocity[Y]          -0.076898         0.12274       0.0006786      0.00063598
v  Velocity[Z]        -3.6769e-15      3.3023e-15     -6.7087e-17     -7.6371e-17
v  ǁVelocityǁ          0.00046376         0.12597        0.036275        0.037425
v  Pressure            -0.0079511         0.01941     -0.00028616     -4.8439e-19
v  k                   6.2374e-16      0.00021753      8.5822e-06      9.1643e-06
v  epsilon             2.4744e-11        0.003327      0.00012894      0.00013395
v  TempC                   21.411          29.896          26.266          26.176
v  Density                 1.1656          1.1994          1.1802          1.1806
v  TurbVisc            1.4329e-22      1.5873e-06      1.0264e-07      1.1105e-07
v  CourantNb              0.05291          14.078          3.2026          3.2097
v  FourierNb              0.41668          2.6907          0.8892         0.83818
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  TempC                     21.362              30          26.328          26.424
v  Boundary Density          1.1656          1.1994          1.1798          1.1796
v  Yplus                          0          4.0886         0.11153         0.22454


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47382           15.46          4.0919          4.0479


 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         0.595570041E-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 0.31271E-01
   Friction velocity        uet   :  0.42311E-03 0.20447E-01
   Friction velocity        uk    :  0.42311E-03 0.25647E-01
   Dimensionless distance   yplus :  0.54543E-01 0.40787E+01
   Friction thermal sca.    tstar : -0.17793E+02-0.14096E+00
   Rough dim-less th. sca.  tplus :  0.40695E-01 0.30432E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        204
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42709E-05      88   0.11338E+00   0.50432E-04 0.23054E+00 
c  Velocity[X]                                      0.15609E-04 
c  Velocity[Y]                                      0.34823E-04 
c  Velocity[Z]                                      0.17385E-31 
c  Pressure     0.12390E-04     167   0.37550E-02   0.12289E+00 0.31978E+00 
c  k            0.26552E-07      41   0.12556E-04   0.60781E-10 0.31268E+00 
c  epsilon      0.69530E-06      27   0.23822E-05   0.14832E-07 0.31372E+00 
c  TempC        0.22550E+01      76   0.56278E-02   0.80112E-01 0.15183E-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]          -0.080303        0.079823      0.00043675      6.2885e-06
v  Velocity[Y]          -0.074649         0.12186      0.00097994      0.00065294
v  Velocity[Z]        -3.5011e-15      3.7049e-15     -6.6045e-17     -7.4887e-17
v  ǁVelocityǁ            2.47e-05         0.12453        0.035072        0.036182
v  Pressure            -0.0075027        0.018106     -0.00030322      6.4235e-19
v  k                     1.09e-16      0.00020874      8.1182e-06      8.7153e-06
v  epsilon             3.9909e-11       0.0031289       0.0001222      0.00012722
v  TempC                   21.458          29.904           26.38           26.28
v  Density                 1.1656          1.1992          1.1798          1.1801
v  TurbVisc            2.0029e-23      1.5398e-06      9.8515e-08      1.0708e-07
v  CourantNb             0.027833          13.855          3.1072          3.1162
v  FourierNb              0.41701           2.693         0.89239         0.84118
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  TempC                     21.411              30          26.443          26.523
v  Boundary Density          1.1656          1.1992          1.1793          1.1792
v  Yplus                          0          4.0787         0.10862         0.21901


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45734          15.237          3.9996          3.9574


 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         0.328225267E-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 0.30595E-01
   Friction velocity        uet   :  0.63400E-03 0.20503E-01
   Friction velocity        uk    :  0.63399E-03 0.25501E-01
   Dimensionless distance   yplus :  0.10042E+00 0.40547E+01
   Friction thermal sca.    tstar : -0.95608E+01-0.13633E+00
   Rough dim-less th. sca.  tplus :  0.74925E-01 0.30252E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        204
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41437E-05      88   0.10341E+00   0.51061E-04 0.23820E+00 
c  Velocity[X]                                      0.16343E-04 
c  Velocity[Y]                                      0.34718E-04 
c  Velocity[Z]                                      0.12956E-31 
c  Pressure     0.11313E-04     164   0.33941E-02   0.11373E+00 0.31491E+00 
c  k            0.25694E-07      42   0.15920E-04   0.58946E-10 0.31586E+00 
c  epsilon      0.66705E-06      29   0.61056E-05   0.21339E-07 0.38898E+00 
c  TempC        0.22609E+01      77   0.46735E-02   0.71409E-01 0.14282E-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]          -0.076934        0.076271      0.00040896     -2.1107e-06
v  Velocity[Y]          -0.073433         0.11959       0.0013497      0.00067348
v  Velocity[Z]        -3.3502e-15      3.9698e-15     -6.5198e-17     -7.3687e-17
v  ǁVelocityǁ           0.0004249         0.12176        0.033869        0.034936
v  Pressure            -0.0070684        0.016966      -0.0003236      3.4048e-19
v  k                   1.0193e-16      0.00020062       7.898e-06      8.4471e-06
v  epsilon             2.3565e-10        0.003073      0.00011742      0.00012202
v  TempC                    21.51          29.911          26.486           26.38
v  Density                 1.1655           1.199          1.1793          1.1797
v  TurbVisc            5.8471e-25       1.493e-06      9.4688e-08      1.0352e-07
v  CourantNb             0.031705          13.354          2.9952          3.0076
v  FourierNb              0.41722          2.6959         0.88764         0.83678
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  TempC                     21.458              30          26.551          26.618
v  Boundary Density          1.1655           1.199          1.1789          1.1788
v  Yplus                          0          4.0547         0.10626         0.21435


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            0.45          14.736          3.8828          3.8444


 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         0.211758237E-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 0.30746E-01
   Friction velocity        uet   :  0.42687E-03 0.19986E-01
   Friction velocity        uk    :  0.42686E-03 0.25225E-01
   Dimensionless distance   yplus :  0.68055E-01 0.40100E+01
   Friction thermal sca.    tstar : -0.41292E+02-0.12846E+00
   Rough dim-less th. sca.  tplus :  0.50776E-01 0.29919E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        201
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40282E-05      90   0.11333E+00   0.55881E-04 0.25492E+00 
c  Velocity[X]                                      0.18605E-04 
c  Velocity[Y]                                      0.37276E-04 
c  Velocity[Z]                                      0.93112E-32 
c  Pressure     0.10737E-04     164   0.31274E-02   0.10920E+00 0.29564E+00 
c  k            0.25049E-07      42   0.10855E-04   0.62067E-10 0.32970E+00 
c  epsilon      0.64542E-06      26   0.42823E-05   0.23751E-07 0.41907E+00 
c  TempC        0.22666E+01      77   0.47949E-02   0.61599E-01 0.13218E-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]          -0.073353        0.073775      0.00037597     -8.6692e-06
v  Velocity[Y]          -0.074647         0.11605       0.0017526      0.00069281
v  Velocity[Z]          -3.26e-15       3.919e-15      -6.483e-17      -7.269e-17
v  ǁVelocityǁ          0.00055519         0.11787        0.032804        0.033815
v  Pressure            -0.0068149        0.015918     -0.00034589     -6.0374e-19
v  k                   8.5533e-17      0.00019315      7.8292e-06      8.2986e-06
v  epsilon             1.6615e-10       0.0031626      0.00011569      0.00011906
v  TempC                   21.592          29.916          26.584          26.476
v  Density                 1.1655          1.1988          1.1789          1.1793
v  TurbVisc            2.6962e-24      1.4536e-06      9.2631e-08      1.0128e-07
v  CourantNb             0.017105          12.835          2.8745          2.8905
v  FourierNb              0.41742           2.699         0.88927         0.83786
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  TempC                      21.51              30          26.652          26.709
v  Boundary Density          1.1655          1.1988          1.1784          1.1784
v  Yplus                          0            4.01          0.1055         0.21242


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44806          14.216          3.7637          3.7283


 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         0.440721830E-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 0.30626E-01
   Friction velocity        uet   :  0.11485E-02 0.20375E-01
   Friction velocity        uk    :  0.11485E-02 0.24834E-01
   Dimensionless distance   yplus :  0.14963E+00 0.39470E+01
   Friction thermal sca.    tstar : -0.11280E+02-0.12403E+00
   Rough dim-less th. sca.  tplus :  0.11164E+00 0.29449E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        200
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39237E-05      93   0.10781E+00   0.61292E-04 0.27185E+00 
c  Velocity[X]                                      0.21133E-04 
c  Velocity[Y]                                      0.40160E-04 
c  Velocity[Z]                                      0.78635E-32 
c  Pressure     0.11207E-04     168   0.30541E-02   0.11537E+00 0.25889E+00 
c  k            0.24513E-07      41   0.13563E-04   0.75292E-10 0.36808E+00 
c  epsilon      0.63050E-06      26   0.37392E-05   0.27440E-07 0.45552E+00 
c  TempC        0.22722E+01      76   0.51045E-02   0.53419E-01 0.12267E-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]           -0.07014        0.071438      0.00033231     -1.2398e-05
v  Velocity[Y]          -0.073987         0.11253       0.0021591      0.00071279
v  Velocity[Z]        -3.3116e-15      3.5008e-15     -6.4618e-17     -7.1837e-17
v  ǁVelocityǁ          7.7243e-05          0.1137        0.032123        0.033033
v  Pressure             -0.006659        0.014988     -0.00036619     -4.0366e-19
v  k                   1.5267e-16      0.00018773      7.8431e-06      8.2142e-06
v  epsilon             7.7897e-11       0.0032256      0.00011657      0.00011819
v  TempC                   21.685          29.923          26.676          26.567
v  Density                 1.1655          1.1984          1.1785          1.1789
v  TurbVisc            3.2093e-25      1.4198e-06      9.1946e-08      1.0026e-07
v  CourantNb             0.020433          12.269          2.7632          2.7804
v  FourierNb               0.4172          2.7017         0.88931         0.83766
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  TempC                     21.592              30          26.745          26.796
v  Boundary Density          1.1655          1.1984          1.1781          1.1781
v  Yplus                          0           3.947          0.1055         0.21189


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44134           13.65          3.6525          3.6181


 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         0.125731453E-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 0.30631E-01
   Friction velocity        uet   :  0.44217E-03 0.20301E-01
   Friction velocity        uk    :  0.44217E-03 0.24414E-01
   Dimensionless distance   yplus :  0.70031E-01 0.38795E+01
   Friction thermal sca.    tstar : -0.11967E+02-0.10550E+00
   Rough dim-less th. sca.  tplus :  0.52251E-01 0.28945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        198
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38413E-05      94   0.10177E+00   0.64419E-04 0.28201E+00 
c  Velocity[X]                                      0.22489E-04 
c  Velocity[Y]                                      0.41930E-04 
c  Velocity[Z]                                      0.70399E-32 
c  Pressure     0.11234E-04     167   0.30386E-02   0.11691E+00 0.22962E+00 
c  k            0.24082E-07      42   0.12389E-04   0.64014E-10 0.34353E+00 
c  epsilon      0.61946E-06      27   0.35846E-05   0.25080E-07 0.44138E+00 
c  TempC        0.22777E+01      76   0.45144E-02   0.50412E-01 0.11879E-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]          -0.067106        0.068427      0.00028775     -1.5665e-05
v  Velocity[Y]          -0.071873         0.10904       0.0025406      0.00073341
v  Velocity[Z]        -3.3284e-15       3.249e-15     -6.4403e-17     -7.0952e-17
v  ǁVelocityǁ          0.00015971         0.10965        0.031801        0.032579
v  Pressure            -0.0070891        0.014133     -0.00038134       1.053e-19
v  k                   1.1346e-16      0.00018319       7.851e-06      8.1453e-06
v  epsilon             7.5262e-12       0.0033739      0.00011661      0.00011678
v  TempC                   21.808          29.932          26.762          26.655
v  Density                 1.1655          1.1981          1.1782          1.1786
v  TurbVisc            1.9988e-24      1.3878e-06      9.1499e-08      9.9308e-08
v  CourantNb             0.014262          11.233          2.6848          2.6979
v  FourierNb              0.41649          2.7051         0.89097         0.83989
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  TempC                     21.685              30          26.833          26.879
v  Boundary Density          1.1655          1.1981          1.1777          1.1777
v  Yplus                          0          3.8795         0.10554         0.21147


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43517          12.614          3.5758          3.5378


 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         0.647186111E-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 0.30945E-01
   Friction velocity        uet   :  0.19714E-03 0.19051E-01
   Friction velocity        uk    :  0.19714E-03 0.24008E-01
   Dimensionless distance   yplus :  0.31226E-01 0.38141E+01
   Friction thermal sca.    tstar : -0.10435E+02-0.96866E-01
   Rough dim-less th. sca.  tplus :  0.23298E-01 0.28457E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        192
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37960E-05      94   0.10445E+00   0.66371E-04 0.28730E+00 
c  Velocity[X]                                      0.22906E-04 
c  Velocity[Y]                                      0.43464E-04 
c  Velocity[Z]                                      0.77729E-32 
c  Pressure     0.11544E-04     168   0.30081E-02   0.12142E+00 0.22261E+00 
c  k            0.23801E-07      45   0.12048E-04   0.42727E-10 0.28268E+00 
c  epsilon      0.61168E-06      31   0.36961E-05   0.18412E-07 0.38192E+00 
c  TempC        0.22831E+01      76   0.48542E-02   0.51456E-01 0.11964E-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]          -0.064729        0.066346      0.00024667     -1.3449e-05
v  Velocity[Y]          -0.074829          0.1052       0.0028677      0.00075146
v  Velocity[Z]        -3.2605e-15      2.9907e-15     -6.4062e-17     -6.9764e-17
v  ǁVelocityǁ          0.00013397         0.10542        0.031927        0.032567
v  Pressure             -0.007351        0.014033     -0.00038911      9.6176e-19
v  k                   2.1295e-16      0.00017952      7.9278e-06      8.1334e-06
v  epsilon             1.6711e-11       0.0033504      0.00011697      0.00011592
v  TempC                   21.891          29.935          26.845          26.741
v  Density                 1.1654          1.1976          1.1778          1.1782
v  TurbVisc            1.9615e-24      1.3621e-06      9.1607e-08      9.9047e-08
v  CourantNb            0.0077994          10.125          2.6457          2.6501
v  FourierNb              0.41544          2.7089         0.89115         0.83989
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  TempC                     21.808              30          26.916          26.959
v  Boundary Density          1.1654          1.1976          1.1774          1.1774
v  Yplus                          0          3.8141         0.10598         0.21172


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42873          11.266          3.5369            3.49


 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         0.453956720E-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 0.31222E-01
   Friction velocity        uet   :  0.66614E-03 0.20302E-01
   Friction velocity        uk    :  0.66613E-03 0.23783E-01
   Dimensionless distance   yplus :  0.85790E-01 0.37485E+01
   Friction thermal sca.    tstar : -0.50750E+01-0.94188E-01
   Rough dim-less th. sca.  tplus :  0.64009E-01 0.27968E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37730E-05      94   0.10699E+00   0.64711E-04 0.28273E+00 
c  Velocity[X]                                      0.22347E-04 
c  Velocity[Y]                                      0.42364E-04 
c  Velocity[Z]                                      0.96604E-32 
c  Pressure     0.11722E-04     167   0.30104E-02   0.12428E+00 0.21636E+00 
c  k            0.23587E-07      47   0.12792E-04   0.57636E-10 0.32807E+00 
c  epsilon      0.60934E-06      27   0.50452E-05   0.21877E-07 0.41358E+00 
c  TempC        0.22884E+01      77   0.45657E-02   0.54034E-01 0.12223E-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]          -0.062654        0.063641      0.00019696     -6.1173e-06
v  Velocity[Y]          -0.074422         0.10251       0.0031112      0.00076252
v  Velocity[Z]        -3.1142e-15      2.7228e-15     -6.3207e-17     -6.7947e-17
v  ǁVelocityǁ          0.00058826         0.10295        0.032489        0.032991
v  Pressure            -0.0074788        0.014887     -0.00039212      4.4578e-19
v  k                   1.6751e-16      0.00017575      8.1533e-06      8.2382e-06
v  epsilon             8.7043e-11       0.0033778      0.00012124      0.00011781
v  TempC                   21.963           29.94          26.925          26.824
v  Density                 1.1654          1.1972          1.1775          1.1779
v  TurbVisc             6.796e-24      1.3376e-06      9.2191e-08      9.9134e-08
v  CourantNb             0.010193          9.6573          2.6538          2.6482
v  FourierNb              0.41546          2.7137         0.89009         0.83865
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  TempC                     21.891              30          26.994          27.037
v  Boundary Density          1.1654          1.1972          1.1771          1.1771
v  Yplus                          0          3.7485         0.10681         0.21271


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4311          10.797          3.5439          3.4869


 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         0.526748614E-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 0.31311E-01
   Friction velocity        uet   :  0.95274E-04 0.20368E-01
   Friction velocity        uk    :  0.95272E-04 0.24077E-01
   Dimensionless distance   yplus :  0.12269E-01 0.37117E+01
   Friction thermal sca.    tstar : -0.27825E+02-0.10391E+00
   Rough dim-less th. sca.  tplus :  0.91542E-02 0.27693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        188
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37678E-05      94   0.10129E+00   0.61057E-04 0.27213E+00 
c  Velocity[X]                                      0.21104E-04 
c  Velocity[Y]                                      0.39953E-04 
c  Velocity[Z]                                      0.10984E-31 
c  Pressure     0.11328E-04     167   0.30511E-02   0.12112E+00 0.21864E+00 
c  k            0.23401E-07      49   0.12331E-04   0.22912E-10 0.20889E+00 
c  epsilon      0.60707E-06      29   0.47013E-05   0.67399E-08 0.23172E+00 
c  TempC        0.22936E+01      78   0.46243E-02   0.58126E-01 0.12640E-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]          -0.061559        0.060842       0.0001388      1.6726e-07
v  Velocity[Y]          -0.074568         0.10155       0.0032874      0.00077711
v  Velocity[Z]        -3.1231e-15      2.7047e-15     -6.1744e-17     -6.5652e-17
v  ǁVelocityǁ          0.00025993         0.10197        0.033222        0.033616
v  Pressure            -0.0076535         0.01578     -0.00039189      1.1039e-18
v  k                   3.2208e-16      0.00017316      8.1579e-06      8.1907e-06
v  epsilon             6.5871e-11       0.0033738      0.00012134      0.00011705
v  TempC                   22.032          29.943          27.002          26.905
v  Density                 1.1654          1.1969          1.1772          1.1776
v  TurbVisc             5.876e-24      1.3152e-06      9.3609e-08      9.9953e-08
v  CourantNb             0.013295          10.032          2.7091          2.6893
v  FourierNb              0.41512           2.719          0.8911          0.8395
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  TempC                     21.963              30           27.07          27.112
v  Boundary Density          1.1654          1.1969          1.1768          1.1768
v  Yplus                          0          3.7117         0.10704         0.21271


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4393          10.952          3.6002          3.5289


 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         0.682920314E-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 0.31382E-01
   Friction velocity        uet   :  0.61849E-03 0.18765E-01
   Friction velocity        uk    :  0.61841E-03 0.24452E-01
   Dimensionless distance   yplus :  0.79637E-01 0.36963E+01
   Friction thermal sca.    tstar : -0.50018E+01-0.89320E-01
   Rough dim-less th. sca.  tplus :  0.59418E-01 0.27578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        185
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37753E-05      94   0.10008E+00   0.56506E-04 0.25877E+00 
c  Velocity[X]                                      0.19370E-04 
c  Velocity[Y]                                      0.37135E-04 
c  Velocity[Z]                                      0.12422E-31 
c  Pressure     0.11307E-04     164   0.28805E-02   0.12169E+00 0.21677E+00 
c  k            0.23232E-07      50   0.12910E-04   0.15758E-10 0.17369E+00 
c  epsilon      0.60379E-06      30   0.39792E-05   0.76913E-08 0.24822E+00 
c  TempC        0.22987E+01      80   0.56479E-02   0.56964E-01 0.12478E-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]          -0.064772        0.059963      8.2884e-05      1.2401e-06
v  Velocity[Y]          -0.075549         0.10131       0.0034023      0.00079073
v  Velocity[Z]        -3.1834e-15      2.7354e-15      -5.984e-17     -6.2775e-17
v  ǁVelocityǁ            0.000213         0.10146         0.03392        0.034257
v  Pressure            -0.0078494        0.016687     -0.00039094      9.3544e-19
v  k                   2.1875e-16      0.00017198      8.2479e-06      8.2111e-06
v  epsilon             4.7893e-11       0.0033898      0.00012231      0.00011691
v  TempC                   22.105          29.943          27.078          26.983
v  Density                 1.1654          1.1966          1.1769          1.1773
v  TurbVisc            2.0689e-23      1.2954e-06      9.3818e-08      9.9757e-08
v  CourantNb             0.018392          9.8454          2.7842          2.7515
v  FourierNb              0.41517          2.7229         0.89096         0.83899
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  TempC                     22.032              30          27.144          27.186
v  Boundary Density          1.1654          1.1966          1.1765          1.1765
v  Yplus                          0          3.6963         0.10743         0.21303


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43933          10.765          3.6752          3.5905


 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         0.103149422E-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 0.31628E-01
   Friction velocity        uet   :  0.89292E-03 0.20305E-01
   Friction velocity        uk    :  0.89292E-03 0.25040E-01
   Dimensionless distance   yplus :  0.14142E+00 0.36859E+01
   Friction thermal sca.    tstar : -0.84756E+01-0.89034E-01
   Rough dim-less th. sca.  tplus :  0.10551E+00 0.27501E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37955E-05      94   0.10359E+00   0.50395E-04 0.24180E+00 
c  Velocity[X]                                      0.17574E-04 
c  Velocity[Y]                                      0.32821E-04 
c  Velocity[Z]                                      0.10249E-31 
c  Pressure     0.10912E-04     161   0.27204E-02   0.11793E+00 0.20953E+00 
c  k            0.23065E-07      50   0.98353E-05   0.13338E-10 0.16125E+00 
c  epsilon      0.59995E-06      33   0.31090E-05   0.37315E-08 0.17423E+00 
c  TempC        0.23035E+01      80   0.42891E-02   0.57569E-01 0.12509E-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]          -0.069886        0.063331      3.1913e-05      4.2661e-07
v  Velocity[Y]          -0.078745         0.10106       0.0034624      0.00079498
v  Velocity[Z]        -2.8136e-15      2.7365e-15     -5.7165e-17     -5.9641e-17
v  ǁVelocityǁ          0.00041439         0.10109        0.034455        0.034779
v  Pressure             -0.008185        0.017548     -0.00038923      1.6971e-18
v  k                   1.7976e-16      0.00016988       8.203e-06      8.1487e-06
v  epsilon             1.5955e-11       0.0034502      0.00012228       0.0001164
v  TempC                   22.222          29.941          27.151          27.061
v  Density                 1.1654          1.1964          1.1766          1.1769
v  TurbVisc            1.1604e-23      1.2772e-06      9.4604e-08      1.0001e-07
v  CourantNb             0.022782          9.2117          2.8555          2.8158
v  FourierNb              0.41543          2.7249         0.89108         0.83904
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  TempC                     22.105              30          27.216          27.258
v  Boundary Density          1.1654          1.1964          1.1762          1.1762
v  Yplus                          0          3.6859         0.10747         0.21278


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44372          11.309          3.7466          3.6548


 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         0.765803811E-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 0.31792E-01
   Friction velocity        uet   :  0.88045E-03 0.20699E-01
   Friction velocity        uk    :  0.88045E-03 0.25409E-01
   Dimensionless distance   yplus :  0.13944E+00 0.36792E+01
   Friction thermal sca.    tstar : -0.82883E+01-0.96078E-01
   Rough dim-less th. sca.  tplus :  0.10404E+00 0.27451E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        180
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38099E-05      93   0.98114E-01   0.43427E-04 0.22306E+00 
c  Velocity[X]                                      0.15512E-04 
c  Velocity[Y]                                      0.27915E-04 
c  Velocity[Z]                                      0.90560E-32 
c  Pressure     0.11086E-04     162   0.26257E-02   0.12027E+00 0.19564E+00 
c  k            0.22857E-07      51   0.94779E-05   0.44200E-10 0.29624E+00 
c  epsilon      0.59411E-06      29   0.25368E-05   0.79031E-08 0.25596E+00 
c  TempC        0.23082E+01      81   0.59312E-02   0.52192E-01 0.11878E-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]          -0.074258        0.064548     -1.5753e-05     -3.9239e-06
v  Velocity[Y]          -0.076933         0.10162       0.0034778      0.00079557
v  Velocity[Z]        -2.6974e-15      2.7227e-15     -5.4314e-17     -5.6235e-17
v  ǁVelocityǁ          0.00040617         0.10202        0.034764        0.035085
v  Pressure            -0.0084613        0.018331     -0.00038544     -1.2268e-18
v  k                   1.3085e-16      0.00017051      8.1625e-06      8.1186e-06
v  epsilon             3.7375e-11       0.0035419      0.00012216      0.00011633
v  TempC                   22.299          29.942          27.223          27.136
v  Density                 1.1654          1.1959          1.1763          1.1766
v  TurbVisc            4.9627e-24      1.2638e-06       9.414e-08      9.9212e-08
v  CourantNb             0.027023          11.626          2.9086          2.8667
v  FourierNb              0.41614          2.7228         0.89443         0.84243
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  TempC                     22.222              30          27.286          27.328
v  Boundary Density          1.1654          1.1959          1.1759          1.1759
v  Yplus                          0          3.6792          0.1072         0.21207


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44796          13.991          3.8031          3.7091


 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         0.107847808E-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 0.31819E-01
   Friction velocity        uet   :  0.71080E-03 0.20231E-01
   Friction velocity        uk    :  0.71078E-03 0.25573E-01
   Dimensionless distance   yplus :  0.91743E-01 0.36861E+01
   Friction thermal sca.    tstar : -0.11383E+02-0.96381E-01
   Rough dim-less th. sca.  tplus :  0.68450E-01 0.27503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        182
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38191E-05      92   0.10296E+00   0.36709E-04 0.20494E+00 
c  Velocity[X]                                      0.13210E-04 
c  Velocity[Y]                                      0.23499E-04 
c  Velocity[Z]                                      0.86603E-32 
c  Pressure     0.10873E-04     162   0.24525E-02   0.11816E+00 0.17796E+00 
c  k            0.22583E-07      52   0.12361E-04   0.46442E-10 0.30570E+00 
c  epsilon      0.58501E-06      33   0.42281E-05   0.14821E-07 0.35423E+00 
c  TempC        0.23129E+01      81   0.49582E-02   0.48190E-01 0.11384E-01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.4311e-09                             2
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.077057        0.064956     -5.0345e-05     -8.1264e-06
v  Velocity[Y]          -0.081445         0.10301       0.0034594      0.00079734
v  Velocity[Z]        -2.5022e-15         2.7e-15     -5.1556e-17     -5.2888e-17
v  ǁVelocityǁ          0.00012237         0.10372         0.03486        0.035175
v  Pressure            -0.0086899           0.019     -0.00038041     -1.5971e-19
v  k                   1.1042e-16        0.000172      8.1409e-06      8.0734e-06
v  epsilon             3.8378e-11       0.0035698      0.00012129       0.0001152
v  TempC                   22.346          29.942          27.293           27.21
v  Density                 1.1654          1.1956           1.176          1.1763
v  TurbVisc            2.1598e-23      1.2583e-06      9.3921e-08       9.873e-08
v  CourantNb             0.027709          13.329          2.9404           2.898
v  FourierNb              0.41651          2.7214         0.89299         0.84102
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  TempC                     22.299              30          27.354          27.396
v  Boundary Density          1.1654          1.1956          1.1756          1.1756
v  Yplus                          0          3.6861         0.10653         0.21051


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45481          15.692          3.8334           3.739


 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         0.106408514E-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 0.31777E-01
   Friction velocity        uet   :  0.53843E-03 0.20320E-01
   Friction velocity        uk    :  0.53843E-03 0.25243E-01
   Dimensionless distance   yplus :  0.85273E-01 0.37100E+01
   Friction thermal sca.    tstar : -0.18706E+02-0.10220E+00
   Rough dim-less th. sca.  tplus :  0.63623E-01 0.27681E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38103E-05      93   0.10234E+00   0.30707E-04 0.18828E+00 
c  Velocity[X]                                      0.10881E-04 
c  Velocity[Y]                                      0.19827E-04 
c  Velocity[Z]                                      0.72624E-32 
c  Pressure     0.10229E-04     160   0.21770E-02   0.11129E+00 0.15984E+00 
c  k            0.22266E-07      52   0.10639E-04   0.24832E-10 0.22644E+00 
c  epsilon      0.57327E-06      30   0.35658E-05   0.60682E-08 0.23140E+00 
c  TempC        0.23174E+01      81   0.51432E-02   0.43277E-01 0.10761E-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]          -0.075374        0.061496     -7.2437e-05     -1.3485e-05
v  Velocity[Y]          -0.079065         0.10264       0.0034294      0.00080012
v  Velocity[Z]        -2.2527e-15      2.6795e-15     -4.8761e-17     -4.9704e-17
v  ǁVelocityǁ          0.00040803         0.10321         0.03481        0.035109
v  Pressure            -0.0089877        0.019557     -0.00037354     -1.9305e-19
v  k                   1.0384e-16      0.00017276      7.9877e-06      7.9346e-06
v  epsilon             3.5138e-11        0.003392      0.00011831       0.0001126
v  TempC                   22.374          29.944          27.362          27.282
v  Density                 1.1654          1.1954          1.1757          1.1761
v  TurbVisc            1.7208e-23      1.2666e-06      9.3654e-08      9.8037e-08
v  CourantNb            0.0013149          13.954          2.9532          2.9108
v  FourierNb              0.41657          2.7204         0.89337         0.84114
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  TempC                     22.346              30          27.421          27.463
v  Boundary Density          1.1654          1.1954          1.1754          1.1753
v  Yplus                          0            3.71         0.10555         0.20843


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44011          16.213          3.8465          3.7519


 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         0.758359186E-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 0.31483E-01
   Friction velocity        uet   :  0.67861E-03 0.20531E-01
   Friction velocity        uk    :  0.67859E-03 0.24578E-01
   Dimensionless distance   yplus :  0.87431E-01 0.37032E+01
   Friction thermal sca.    tstar : -0.10563E+02-0.93328E-01
   Rough dim-less th. sca.  tplus :  0.65233E-01 0.27630E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37749E-05      94   0.10693E+00   0.26939E-04 0.17814E+00 
c  Velocity[X]                                      0.93844E-05 
c  Velocity[Y]                                      0.17555E-04 
c  Velocity[Z]                                      0.56065E-32 
c  Pressure     0.10022E-04     159   0.18849E-02   0.10918E+00 0.14523E+00 
c  k            0.21841E-07      51   0.13614E-04   0.26899E-10 0.23875E+00 
c  epsilon      0.56040E-06      32   0.51911E-05   0.71545E-08 0.25573E+00 
c  TempC        0.23218E+01      80   0.56843E-02   0.37766E-01 0.10027E-01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -6.9241e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.073917         0.06134     -8.0262e-05      -1.347e-05
v  Velocity[Y]           -0.07812         0.10125       0.0033989      0.00080534
v  Velocity[Z]        -2.0283e-15      2.6627e-15      -4.636e-17     -4.6765e-17
v  ǁVelocityǁ          0.00019362         0.10176        0.034605        0.034872
v  Pressure            -0.0093557        0.020015      -0.0003654     -3.0011e-19
v  k                   8.2761e-17      0.00017287      7.8278e-06      7.7862e-06
v  epsilon             2.5508e-11       0.0032284       0.0001156      0.00011014
v  TempC                   22.497          29.944           27.43          27.352
v  Density                 1.1654          1.1953          1.1755          1.1758
v  TurbVisc            1.1362e-23      1.2698e-06      9.2675e-08       9.682e-08
v  CourantNb              0.01675          14.643          2.9512          2.9087
v  FourierNb              0.41703          2.7201         0.89378         0.84091
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  TempC                     22.374              30          27.487          27.529
v  Boundary Density          1.1654          1.1953          1.1751          1.1751
v  Yplus                          0          3.7032         0.10477         0.20677


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4377          16.901           3.845          3.7496


 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         0.660421001E-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 0.31138E-01
   Friction velocity        uet   :  0.13197E-04 0.20653E-01
   Friction velocity        uk    :  0.13197E-04 0.23913E-01
   Dimensionless distance   yplus :  0.20901E-02 0.36778E+01
   Friction thermal sca.    tstar : -0.59271E+02-0.88333E-01
   Rough dim-less th. sca.  tplus :  0.15595E-02 0.27440E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        192
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37146E-05      94   0.10080E+00   0.25028E-04 0.17429E+00 
c  Velocity[X]                                      0.87518E-05 
c  Velocity[Y]                                      0.16277E-04 
c  Velocity[Z]                                      0.52931E-32 
c  Pressure     0.98340E-05     163   0.17726E-02   0.10720E+00 0.13682E+00 
c  k            0.21378E-07      50   0.84828E-05   0.30778E-10 0.26122E+00 
c  epsilon      0.54619E-06      28   0.25358E-05   0.52398E-08 0.22467E+00 
c  TempC        0.23261E+01      78   0.37399E-02   0.35597E-01 0.97116E-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]          -0.070461        0.061302     -7.7657e-05     -1.3806e-05
v  Velocity[Y]          -0.076045        0.099853         0.00338      0.00080919
v  Velocity[Z]        -1.8297e-15      2.6473e-15     -4.4213e-17     -4.4185e-17
v  ǁVelocityǁ          0.00024514         0.10038        0.034249        0.034467
v  Pressure            -0.0097659        0.020421     -0.00035745      6.2129e-19
v  k                    7.301e-17      0.00017165      7.5618e-06       7.531e-06
v  epsilon             7.2627e-15       0.0029571      0.00011119      0.00010619
v  TempC                   22.632          29.946          27.497           27.42
v  Density                 1.1654          1.1948          1.1752          1.1755
v  TurbVisc            7.5709e-24      1.2708e-06      9.1255e-08      9.5177e-08
v  CourantNb            0.0090336          14.304          2.9358          2.8932
v  FourierNb              0.41689          2.7201         0.89198         0.83989
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  TempC                     22.497              30          27.552          27.592
v  Boundary Density          1.1654          1.1948          1.1748          1.1748
v  Yplus                          0          3.6778          0.1038         0.20481


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45896          16.562          3.8278          3.7331


 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         0.187935435E-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 0.30489E-01
   Friction velocity        uet   :  0.35094E-03 0.20239E-01
   Friction velocity        uk    :  0.35093E-03 0.23116E-01
   Dimensionless distance   yplus :  0.45187E-01 0.36543E+01
   Friction thermal sca.    tstar : -0.60662E+01-0.87810E-01
   Rough dim-less th. sca.  tplus :  0.33714E-01 0.27265E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        198
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36436E-05      94   0.10170E+00   0.23731E-04 0.17306E+00 
c  Velocity[X]                                      0.88169E-05 
c  Velocity[Y]                                      0.14914E-04 
c  Velocity[Z]                                      0.45537E-32 
c  Pressure     0.95820E-05     166   0.17495E-02   0.10461E+00 0.12574E+00 
c  k            0.20900E-07      48   0.98570E-05   0.37456E-10 0.29225E+00 
c  epsilon      0.53343E-06      27   0.33915E-05   0.92926E-08 0.30421E+00 
c  TempC        0.23302E+01      75   0.51733E-02   0.31309E-01 0.90867E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -8.4593e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.0681        0.062078     -6.5691e-05     -1.4585e-05
v  Velocity[Y]          -0.073088        0.096728       0.0033697      0.00081709
v  Velocity[Z]        -1.8278e-15      2.6327e-15     -4.2462e-17     -4.1999e-17
v  ǁVelocityǁ          0.00029316         0.09775        0.033727        0.033897
v  Pressure             -0.010169        0.020792     -0.00034949      2.5957e-18
v  k                   7.7363e-17      0.00016919      7.3971e-06       7.357e-06
v  epsilon             6.4217e-11       0.0028744       0.0001089      0.00010361
v  TempC                   22.788          29.949          27.562          27.486
v  Density                 1.1654          1.1942          1.1749          1.1752
v  TurbVisc             6.413e-24       1.269e-06      8.8802e-08      9.2325e-08
v  CourantNb            0.0026205          13.588          2.9093          2.8657
v  FourierNb               0.4171          2.7183         0.89399         0.84149
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  TempC                     22.632              30          27.616          27.654
v  Boundary Density          1.1654          1.1942          1.1746          1.1746
v  Yplus                          0          3.6543         0.10305         0.20321


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44611          15.844          3.8033          3.7072


 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         0.124407964E-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 0.30275E-01
   Friction velocity        uet   :  0.39016E-03 0.20365E-01
   Friction velocity        uk    :  0.39011E-03 0.22735E-01
   Dimensionless distance   yplus :  0.61778E-01 0.36009E+01
   Friction thermal sca.    tstar : -0.72920E+01-0.84533E-01
   Rough dim-less th. sca.  tplus :  0.46094E-01 0.26866E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35590E-05      92   0.10755E+00   0.22032E-04 0.17063E+00 
c  Velocity[X]                                      0.85277E-05 
c  Velocity[Y]                                      0.13504E-04 
c  Velocity[Z]                                      0.50775E-32 
c  Pressure     0.94308E-05     166   0.16492E-02   0.10327E+00 0.11977E+00 
c  k            0.20436E-07      47   0.15249E-04   0.17048E-10 0.20098E+00 
c  epsilon      0.51874E-06      30   0.54193E-05   0.61786E-08 0.25517E+00 
c  TempC        0.23341E+01      73   0.33979E-02   0.30797E-01 0.89917E-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]          -0.065754        0.063986     -4.2059e-05     -1.1789e-05
v  Velocity[Y]          -0.069061        0.094014       0.0033672      0.00082519
v  Velocity[Z]        -1.8227e-15      2.6202e-15     -4.0932e-17     -4.0183e-17
v  ǁVelocityǁ           0.0002657        0.095173         0.03308        0.033194
v  Pressure             -0.010574        0.021189     -0.00034268     -1.6989e-18
v  k                   1.4959e-17      0.00016631       7.186e-06      7.1459e-06
v  epsilon             8.0824e-11       0.0028538      0.00010412      9.9402e-05
v  TempC                   22.979          29.952          27.625           27.55
v  Density                 1.1654          1.1936          1.1747           1.175
v  TurbVisc            5.3195e-24      1.2617e-06      8.6973e-08      9.0138e-08
v  CourantNb             0.038543          12.814          2.8677          2.8224
v  FourierNb              0.41738          2.7172         0.89586         0.84372
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  TempC                     22.788              30          27.678          27.714
v  Boundary Density          1.1654          1.1936          1.1743          1.1743
v  Yplus                          0          3.6009         0.10219         0.20146


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46201           15.07          3.7635          3.6662


 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         0.356018536E-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 0.30143E-01
   Friction velocity        uet   :  0.14599E-02 0.20578E-01
   Friction velocity        uk    :  0.14592E-02 0.22575E-01
   Dimensionless distance   yplus :  0.18795E+00 0.35553E+01
   Friction thermal sca.    tstar : -0.56527E+01-0.88284E-01
   Rough dim-less th. sca.  tplus :  0.14023E+00 0.26527E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34633E-05      89   0.96784E-01   0.21464E-04 0.17275E+00 
c  Velocity[X]                                      0.81741E-05 
c  Velocity[Y]                                      0.13290E-04 
c  Velocity[Z]                                      0.56840E-32 
c  Pressure     0.91191E-05     166   0.15427E-02   0.10057E+00 0.11293E+00 
c  k            0.19875E-07      44   0.75079E-05   0.20342E-10 0.22455E+00 
c  epsilon      0.50427E-06      25   0.22778E-05   0.38155E-08 0.20555E+00 
c  TempC        0.23380E+01      70   0.37539E-02   0.27971E-01 0.85504E-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]          -0.063463        0.064701     -8.6272e-06     -8.5792e-06
v  Velocity[Y]          -0.063694        0.091188       0.0033598      0.00083152
v  Velocity[Z]        -1.9321e-15      2.6095e-15     -3.9655e-17     -3.8746e-17
v  ǁVelocityǁ          0.00033788        0.092093        0.032343        0.032409
v  Pressure             -0.011014        0.021609     -0.00033741        3.26e-19
v  k                   2.9418e-18      0.00016284      6.9407e-06      6.9172e-06
v  epsilon              1.022e-12       0.0029623      0.00010071      9.5875e-05
v  TempC                   23.208          29.955          27.685          27.613
v  Density                 1.1654          1.1928          1.1744          1.1747
v  TurbVisc            2.2275e-25      1.2499e-06      8.5038e-08      8.7816e-08
v  CourantNb             0.058212          12.191           2.816          2.7679
v  FourierNb              0.41728          2.7172         0.89324          0.8413
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  TempC                     22.979              30          27.737          27.773
v  Boundary Density          1.1654          1.1928          1.1741          1.1741
v  Yplus                          0          3.5553         0.10153         0.20006


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47914          14.446          3.7092          3.6092


 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         0.480426500E-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 0.30266E-01
   Friction velocity        uet   :  0.19170E-03 0.20393E-01
   Friction velocity        uk    :  0.19170E-03 0.22607E-01
   Dimensionless distance   yplus :  0.30359E-01 0.35012E+01
   Friction thermal sca.    tstar : -0.10956E+02-0.84701E-01
   Rough dim-less th. sca.  tplus :  0.22651E-01 0.26123E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        211
   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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33700E-05      86   0.98206E-01   0.20718E-04 0.17426E+00 
c  Velocity[X]                                      0.79884E-05 
c  Velocity[Y]                                      0.12730E-04 
c  Velocity[Z]                                      0.46250E-32 
c  Pressure     0.90647E-05     166   0.14716E-02   0.10080E+00 0.10932E+00 
c  k            0.19298E-07      43   0.69471E-05   0.18755E-10 0.22114E+00 
c  epsilon      0.48725E-06      25   0.23751E-05   0.44065E-08 0.22884E+00 
c  TempC        0.23419E+01      68   0.34825E-02   0.27119E-01 0.84013E-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]          -0.062621        0.064277        3.16e-05     -2.3162e-06
v  Velocity[Y]          -0.057226        0.088755       0.0033511      0.00084265
v  Velocity[Z]        -2.0032e-15      2.5986e-15     -3.8698e-17      -3.765e-17
v  ǁVelocityǁ          0.00010979        0.089474        0.031574        0.031589
v  Pressure              -0.01147        0.022076     -0.00033384      2.4455e-18
v  k                    3.686e-18      0.00016481      6.6696e-06      6.6668e-06
v  epsilon             6.0845e-13       0.0030571      9.5462e-05      9.1405e-05
v  TempC                    23.43          29.957          27.743          27.673
v  Density                 1.1654          1.1919          1.1742          1.1745
v  TurbVisc            3.5517e-26      1.2351e-06      8.2777e-08      8.5478e-08
v  CourantNb             0.056835          11.622          2.7542          2.7032
v  FourierNb              0.41762          2.7173         0.89307          0.8412
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  TempC                     23.208              30          27.795           27.83
v  Boundary Density          1.1654          1.1919          1.1739          1.1739
v  Yplus                          0          3.5012         0.10054         0.19808


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47781          13.878          3.6472          3.5444


 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         0.431457408E-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 0.30401E-01
   Friction velocity        uet   :  0.51737E-03 0.19672E-01
   Friction velocity        uk    :  0.51737E-03 0.22740E-01
   Dimensionless distance   yplus :  0.66621E-01 0.34582E+01
   Friction thermal sca.    tstar : -0.40002E+01-0.81897E-01
   Rough dim-less th. sca.  tplus :  0.49707E-01 0.25802E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        214
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32764E-05      84   0.88481E-01   0.20907E-04 0.17964E+00 
c  Velocity[X]                                      0.78849E-05 
c  Velocity[Y]                                      0.13022E-04 
c  Velocity[Z]                                      0.46400E-32 
c  Pressure     0.86927E-05     164   0.14712E-02   0.97431E-01 0.10426E+00 
c  k            0.18716E-07      41   0.65166E-05   0.15286E-10 0.20423E+00 
c  epsilon      0.46941E-06      24   0.19065E-05   0.44903E-08 0.23887E+00 
c  TempC        0.23457E+01      67   0.39787E-02   0.26103E-01 0.82257E-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]           -0.06273        0.063196      7.5328e-05      1.8737e-06
v  Velocity[Y]          -0.055536        0.085228       0.0033289      0.00085296
v  Velocity[Z]        -2.0642e-15      2.5888e-15     -3.7891e-17     -3.6721e-17
v  ǁVelocityǁ          0.00021421        0.086543        0.030809        0.030786
v  Pressure             -0.011931        0.022571      -0.0003316     -2.2157e-18
v  k                   1.1367e-16      0.00016528      6.4607e-06      6.4717e-06
v  epsilon             5.7208e-11       0.0030743      9.1243e-05      8.7469e-05
v  TempC                     23.6           29.96          27.799          27.731
v  Density                 1.1653           1.191           1.174          1.1742
v  TurbVisc            1.6714e-24      1.2184e-06      8.0544e-08      8.3053e-08
v  CourantNb             0.015605          11.211          2.6884          2.6339
v  FourierNb              0.41773          2.7174         0.89265         0.84064
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  TempC                      23.43              30           27.85          27.885
v  Boundary Density          1.1653           1.191          1.1737          1.1736
v  Yplus                          0          3.4582        0.099492         0.19604


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47492          13.467          3.5811          3.4745


 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         0.215728704E-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 0.30418E-01
   Friction velocity        uet   :  0.30036E-03 0.20574E-01
   Friction velocity        uk    :  0.30036E-03 0.22761E-01
   Dimensionless distance   yplus :  0.38689E-01 0.33967E+01
   Friction thermal sca.    tstar : -0.18030E+02-0.82099E-01
   Rough dim-less th. sca.  tplus :  0.28867E-01 0.25343E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        214
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31950E-05      82   0.83128E-01   0.21648E-04 0.18716E+00 
c  Velocity[X]                                      0.81233E-05 
c  Velocity[Y]                                      0.13525E-04 
c  Velocity[Z]                                      0.42311E-32 
c  Pressure     0.83877E-05     161   0.15107E-02   0.94784E-01 0.10257E+00 
c  k            0.18201E-07      40   0.61064E-05   0.19161E-10 0.23433E+00 
c  epsilon      0.45180E-06      24   0.16929E-05   0.30899E-08 0.20507E+00 
c  TempC        0.23493E+01      65   0.37364E-02   0.26351E-01 0.82484E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -8.4732e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.061403        0.061952      0.00011877       6.896e-06
v  Velocity[Y]          -0.055731        0.082797        0.003295       0.0008643
v  Velocity[Z]        -2.1118e-15      2.5778e-15     -3.7398e-17     -3.6053e-17
v  ǁVelocityǁ           0.0002856        0.083959        0.030109        0.030053
v  Pressure             -0.012372        0.023097     -0.00032981     -3.3697e-19
v  k                   1.0557e-16      0.00016495      6.2288e-06      6.2714e-06
v  epsilon             6.3333e-12        0.003058      8.7163e-05      8.3925e-05
v  TempC                   23.681          29.962          27.852          27.788
v  Density                 1.1653          1.1903          1.1737           1.174
v  TurbVisc            2.4876e-24      1.1997e-06      7.8746e-08      8.1127e-08
v  CourantNb             0.016225          10.952          2.6213          2.5636
v  FourierNb              0.41789           2.717         0.89465         0.84307
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  TempC                       23.6              30          27.903          27.938
v  Boundary Density          1.1653          1.1903          1.1734          1.1734
v  Yplus                          0          3.3967        0.098185         0.19356


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47534          13.208          3.5159          3.4066


 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         0.307049443E-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 0.30277E-01
   Friction velocity        uet   :  0.26227E-03 0.20674E-01
   Friction velocity        uk    :  0.26225E-03 0.22596E-01
   Dimensionless distance   yplus :  0.33849E-01 0.33504E+01
   Friction thermal sca.    tstar : -0.30991E+02-0.71781E-01
   Rough dim-less th. sca.  tplus :  0.25255E-01 0.24998E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31234E-05      81   0.83020E-01   0.21742E-04 0.19146E+00 
c  Velocity[X]                                      0.79751E-05 
c  Velocity[Y]                                      0.13767E-04 
c  Velocity[Z]                                      0.39596E-32 
c  Pressure     0.82254E-05     158   0.15840E-02   0.93746E-01 0.99991E-01 
c  k            0.17693E-07      38   0.10855E-04   0.38096E-10 0.33581E+00 
c  epsilon      0.43663E-06      23   0.36654E-05   0.11062E-07 0.39624E+00 
c  TempC        0.23528E+01      64   0.36987E-02   0.25357E-01 0.80760E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.0932e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.060792        0.060835      0.00015899      1.0026e-05
v  Velocity[Y]          -0.055844         0.08053       0.0032377       0.0008718
v  Velocity[Z]        -2.1637e-15      2.5658e-15     -3.6962e-17      -3.563e-17
v  ǁVelocityǁ          0.00019884        0.081778        0.029478        0.029402
v  Pressure             -0.012807        0.023648     -0.00032858     -5.9847e-19
v  k                     8.78e-17      0.00016325      6.1278e-06      6.1642e-06
v  epsilon             5.7488e-11       0.0030223      8.5593e-05      8.2201e-05
v  TempC                   23.772          29.964          27.904          27.842
v  Density                 1.1653            1.19          1.1735          1.1738
v  TurbVisc            1.5391e-24      1.1883e-06      7.6767e-08      7.9118e-08
v  CourantNb              0.02136          10.667          2.5597           2.499
v  FourierNb              0.41764          2.7164         0.89506         0.84328
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  TempC                     23.681              30          27.954          27.989
v  Boundary Density          1.1653            1.19          1.1732          1.1732
v  Yplus                          0          3.3504          0.0973         0.19189


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4746          12.922          3.4548          3.3423


 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         0.565129794E-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 0.30136E-01
   Friction velocity        uet   :  0.14508E-02 0.20112E-01
   Friction velocity        uk    :  0.14508E-02 0.22426E-01
   Dimensionless distance   yplus :  0.22975E+00 0.33079E+01
   Friction thermal sca.    tstar : -0.95379E+01-0.78063E-01
   Rough dim-less th. sca.  tplus :  0.17142E+00 0.24680E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        219
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30654E-05      81   0.77995E-01   0.20886E-04 0.19080E+00 
c  Velocity[X]                                      0.77467E-05 
c  Velocity[Y]                                      0.13139E-04 
c  Velocity[Z]                                      0.40014E-32 
c  Pressure     0.81418E-05     155   0.17434E-02   0.93426E-01 0.96292E-01 
c  k            0.17271E-07      38   0.77906E-05   0.28012E-10 0.29307E+00 
c  epsilon      0.42235E-06      23   0.24539E-05   0.75742E-08 0.33758E+00 
c  TempC        0.23562E+01      63   0.30696E-02   0.24176E-01 0.78713E-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]          -0.061348        0.059558      0.00019042      1.0393e-05
v  Velocity[Y]          -0.056135        0.078638        0.003164      0.00088093
v  Velocity[Z]        -2.2061e-15      2.5502e-15     -3.6695e-17     -3.5379e-17
v  ǁVelocityǁ           0.0003536        0.079813        0.028956         0.02887
v  Pressure             -0.013218        0.024199     -0.00032705      4.4578e-19
v  k                   8.4233e-17      0.00016052      5.9545e-06      6.0123e-06
v  epsilon             4.5407e-11       0.0029527      8.2226e-05      7.9324e-05
v  TempC                   23.873          29.965          27.954          27.894
v  Density                 1.1653          1.1896          1.1733          1.1736
v  TurbVisc            6.4693e-24      1.1761e-06      7.5355e-08      7.7486e-08
v  CourantNb             0.023742          10.425          2.5022          2.4397
v  FourierNb              0.41786          2.7156         0.89299         0.84113
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  TempC                     23.772              30          28.003          28.038
v  Boundary Density          1.1653          1.1896           1.173           1.173
v  Yplus                          0          3.3079        0.096124         0.18969


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47412          12.679          3.3952          3.2808


 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         0.330872245E-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 0.29953E-01
   Friction velocity        uet   :  0.53708E-03 0.20373E-01
   Friction velocity        uk    :  0.53703E-03 0.22245E-01
   Dimensionless distance   yplus :  0.69313E-01 0.32672E+01
   Friction thermal sca.    tstar : -0.14841E+02-0.76923E-01
   Rough dim-less th. sca.  tplus :  0.51715E-01 0.24377E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        220
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30194E-05      80   0.82497E-01   0.19522E-04 0.18692E+00 
c  Velocity[X]                                      0.75520E-05 
c  Velocity[Y]                                      0.11970E-04 
c  Velocity[Z]                                      0.45551E-32 
c  Pressure     0.79401E-05     154   0.18634E-02   0.91638E-01 0.93064E-01 
c  k            0.16930E-07      39   0.76512E-05   0.24337E-10 0.27601E+00 
c  epsilon      0.40995E-06      23   0.21199E-05   0.66852E-08 0.32354E+00 
c  TempC        0.23596E+01      62   0.35844E-02   0.21353E-01 0.73846E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -3.7708e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.06156        0.057429      0.00021508      9.1615e-06
v  Velocity[Y]          -0.055884        0.076385       0.0030706      0.00088666
v  Velocity[Z]         -2.175e-15      2.5282e-15     -3.6356e-17     -3.5064e-17
v  ǁVelocityǁ          6.0927e-05        0.077797        0.028535        0.028454
v  Pressure              -0.01362        0.024763     -0.00032463      1.8112e-18
v  k                   5.5165e-17      0.00015821      5.8702e-06       5.952e-06
v  epsilon             1.0373e-10       0.0028907      7.9889e-05      7.7493e-05
v  TempC                   23.952          29.967          28.002          27.944
v  Density                 1.1653          1.1892          1.1731          1.1734
v  TurbVisc            8.0858e-24      1.1712e-06      7.3602e-08      7.5634e-08
v  CourantNb             0.035927          10.214          2.4566          2.3925
v  FourierNb              0.41767          2.7149         0.89437         0.84266
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  TempC                     23.873              30          28.051          28.085
v  Boundary Density          1.1653          1.1892          1.1729          1.1728
v  Yplus                          0          3.2672        0.094904         0.18754


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47438          12.468          3.3509          3.2352


 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         0.452633231E-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 0.29560E-01
   Friction velocity        uet   :  0.43902E-03 0.20446E-01
   Friction velocity        uk    :  0.43901E-03 0.21963E-01
   Dimensionless distance   yplus :  0.63075E-01 0.32394E+01
   Friction thermal sca.    tstar : -0.84107E+01-0.68959E-01
   Rough dim-less th. sca.  tplus :  0.47061E-01 0.24169E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29795E-05      80   0.79840E-01   0.18029E-04 0.18180E+00 
c  Velocity[X]                                      0.72309E-05 
c  Velocity[Y]                                      0.10798E-04 
c  Velocity[Z]                                      0.40336E-32 
c  Pressure     0.75786E-05     157   0.18205E-02   0.87843E-01 0.85450E-01 
c  k            0.16550E-07      39   0.85343E-05   0.32390E-10 0.32399E+00 
c  epsilon      0.39847E-06      24   0.19997E-05   0.51026E-08 0.28921E+00 
c  TempC        0.23627E+01      62   0.30837E-02   0.20000E-01 0.71346E-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]          -0.065153        0.057435      0.00023958      6.4874e-06
v  Velocity[Y]          -0.055977        0.074874       0.0029665      0.00089207
v  Velocity[Z]        -2.1422e-15      2.5057e-15     -3.5806e-17     -3.4466e-17
v  ǁVelocityǁ          0.00026616         0.08108        0.028161        0.028086
v  Pressure             -0.013976        0.025292      -0.0003209     -8.9683e-19
v  k                   7.0305e-18      0.00016049      5.6798e-06      5.8158e-06
v  epsilon             1.1472e-11        0.002908      7.7428e-05      7.5869e-05
v  TempC                   24.038          29.968          28.049          27.993
v  Density                 1.1653          1.1889          1.1729          1.1732
v  TurbVisc            8.9731e-26      1.1572e-06      7.2529e-08      7.4511e-08
v  CourantNb             0.042811          9.9956          2.4202          2.3554
v  FourierNb              0.41788          2.7142         0.89318         0.84158
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  TempC                     23.952              30          28.097          28.131
v  Boundary Density          1.1653          1.1889          1.1727          1.1726
v  Yplus                          0          3.2394        0.093579         0.18519


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46383           12.25          3.3133           3.197


 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         0.780858498E-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 0.29737E-01
   Friction velocity        uet   :  0.29611E-03 0.20488E-01
   Friction velocity        uk    :  0.29611E-03 0.22019E-01
   Dimensionless distance   yplus :  0.38144E-01 0.33237E+01
   Friction thermal sca.    tstar : -0.61762E+01-0.63640E-01
   Rough dim-less th. sca.  tplus :  0.28460E-01 0.24799E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29414E-05      79   0.75699E-01   0.16975E-04 0.17857E+00 
c  Velocity[X]                                      0.70848E-05 
c  Velocity[Y]                                      0.98901E-05 
c  Velocity[Z]                                      0.36957E-32 
c  Pressure     0.70905E-05     157   0.16398E-02   0.82498E-01 0.78404E-01 
c  k            0.16228E-07      49   0.16041E-04   0.23572E-10 0.28079E+00 
c  epsilon      0.38751E-06      43   0.75272E-05   0.70846E-08 0.34974E+00 
c  TempC        0.23657E+01      63   0.28921E-02   0.17400E-01 0.66437E-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]          -0.064704        0.057301      0.00026192      4.0024e-06
v  Velocity[Y]          -0.055014         0.07375       0.0028534      0.00089702
v  Velocity[Z]        -2.2226e-15      2.4844e-15     -3.5131e-17     -3.3732e-17
v  ǁVelocityǁ           0.0004233        0.083097        0.027796        0.027734
v  Pressure             -0.014254        0.025781     -0.00031553     -2.0218e-18
v  k                    1.315e-16      0.00015986      5.5188e-06      5.6717e-06
v  epsilon             6.3283e-12       0.0028854      7.4446e-05      7.3345e-05
v  TempC                   24.131           29.97          28.095           28.04
v  Density                 1.1653          1.1886          1.1728           1.173
v  TurbVisc            2.4321e-25      1.1506e-06       7.033e-08      7.2437e-08
v  CourantNb              0.03108           9.821          2.3905          2.3244
v  FourierNb              0.41771          2.7132         0.89175         0.84053
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  TempC                     24.038              30          28.142          28.175
v  Boundary Density          1.1653          1.1886          1.1725          1.1725
v  Yplus                          0          3.3237        0.092262         0.18291


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46143          12.074          3.2822          3.1649


 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         0.153524722E-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 0.29807E-01
   Friction velocity        uet   :  0.51552E-03 0.20456E-01
   Friction velocity        uk    :  0.51547E-03 0.22090E-01
   Dimensionless distance   yplus :  0.66386E-01 0.33630E+01
   Friction thermal sca.    tstar : -0.17361E+02-0.67112E-01
   Rough dim-less th. sca.  tplus :  0.49531E-01 0.25092E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29019E-05      78   0.74078E-01   0.16181E-04 0.17681E+00 
c  Velocity[X]                                      0.67736E-05 
c  Velocity[Y]                                      0.94075E-05 
c  Velocity[Z]                                      0.34553E-32 
c  Pressure     0.64208E-05     157   0.15234E-02   0.74852E-01 0.69312E-01 
c  k            0.15915E-07      37   0.11201E-04   0.23174E-10 0.28268E+00 
c  epsilon      0.37735E-06      24   0.65141E-05   0.58225E-08 0.32393E+00 
c  TempC        0.23686E+01      63   0.28650E-02   0.16414E-01 0.64426E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.2157e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.064439        0.055809      0.00027382     -2.7735e-07
v  Velocity[Y]          -0.053299        0.073178       0.0027324      0.00090204
v  Velocity[Z]        -2.2971e-15      2.4733e-15     -3.4342e-17     -3.3018e-17
v  ǁVelocityǁ          0.00064036        0.085011        0.027367        0.027324
v  Pressure             -0.014522        0.026216     -0.00030802     -2.9028e-18
v  k                   1.1188e-16      0.00015968      5.3268e-06      5.5221e-06
v  epsilon             6.3643e-11       0.0029065      7.1375e-05      7.0962e-05
v  TempC                   24.216          29.971           28.14          28.086
v  Density                 1.1653          1.1882          1.1726          1.1728
v  TurbVisc            1.6921e-24      1.1415e-06      6.8189e-08      7.0162e-08
v  CourantNb             0.022813          9.5452          2.3623          2.2953
v  FourierNb              0.41789          2.7125         0.89283         0.84128
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  TempC                     24.131              30          28.185          28.218
v  Boundary Density          1.1653          1.1882          1.1723          1.1723
v  Yplus                          0           3.363        0.090782         0.18023


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45486          11.799          3.2551          3.1366


 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        -0.542630482E-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 0.29829E-01
   Friction velocity        uet   :  0.37818E-03 0.20649E-01
   Friction velocity        uk    :  0.37818E-03 0.22116E-01
   Dimensionless distance   yplus :  0.59893E-01 0.33935E+01
   Friction thermal sca.    tstar : -0.34777E+01-0.64489E-01
   Rough dim-less th. sca.  tplus :  0.44687E-01 0.25319E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        234
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28555E-05      78   0.71824E-01   0.15979E-04 0.17863E+00 
c  Velocity[X]                                      0.64768E-05 
c  Velocity[Y]                                      0.95024E-05 
c  Velocity[Z]                                      0.33939E-32 
c  Pressure     0.63145E-05     155   0.14546E-02   0.73756E-01 0.61845E-01 
c  k            0.15692E-07      40   0.12185E-04   0.23140E-10 0.28829E+00 
c  epsilon      0.36752E-06      35   0.62371E-05   0.54301E-08 0.32116E+00 
c  TempC        0.23714E+01      63   0.25062E-02   0.16346E-01 0.64192E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.7365e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.06344        0.054575      0.00028076     -1.3059e-06
v  Velocity[Y]          -0.052299        0.071773       0.0026139      0.00090874
v  Velocity[Z]        -2.3655e-15      2.4672e-15     -3.3922e-17     -3.2682e-17
v  ǁVelocityǁ          0.00028678        0.085694        0.026861        0.026838
v  Pressure             -0.014903        0.026611     -0.00030092      7.0202e-20
v  k                   2.7812e-16      0.00015829      5.1282e-06      5.3642e-06
v  epsilon             1.1603e-11       0.0028765      6.8485e-05      6.8769e-05
v  TempC                    24.42          29.973          28.185          28.131
v  Density                 1.1653          1.1879          1.1724          1.1726
v  TurbVisc             1.878e-24      1.1381e-06      6.6142e-08      6.8216e-08
v  CourantNb             0.031456          9.1381          2.3281          2.2616
v  FourierNb              0.41779          2.7128         0.89177         0.84037
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  TempC                     24.216              30          28.228           28.26
v  Boundary Density          1.1653          1.1879          1.1721          1.1721
v  Yplus                          0          3.3935        0.089308         0.17765


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45747          11.392          3.2199          3.1019


 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         0.378517848E-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 0.29509E-01
   Friction velocity        uet   :  0.65676E-03 0.20708E-01
   Friction velocity        uk    :  0.65667E-03 0.21797E-01
   Dimensionless distance   yplus :  0.84699E-01 0.34074E+01
   Friction thermal sca.    tstar : -0.89708E+01-0.61599E-01
   Rough dim-less th. sca.  tplus :  0.63195E-01 0.25423E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        242
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28044E-05      77   0.73072E-01   0.15228E-04 0.17798E+00 
c  Velocity[X]                                      0.58613E-05 
c  Velocity[Y]                                      0.93664E-05 
c  Velocity[Z]                                      0.32454E-32 
c  Pressure     0.62069E-05     154   0.14491E-02   0.72686E-01 0.52969E-01 
c  k            0.15308E-07      40   0.87341E-05   0.48548E-10 0.42511E+00 
c  epsilon      0.35933E-06      28   0.42909E-05   0.11192E-07 0.46673E+00 
c  TempC        0.23741E+01      63   0.25033E-02   0.15183E-01 0.61773E-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]          -0.061362        0.052504      0.00026377     -3.7875e-06
v  Velocity[Y]          -0.051808        0.072534       0.0024886      0.00091188
v  Velocity[Z]        -2.4301e-15      2.4655e-15     -3.4062e-17     -3.2746e-17
v  ǁVelocityǁ          0.00043946        0.085981        0.026237        0.026237
v  Pressure             -0.015189         0.02694     -0.00029263      1.1583e-18
v  k                   1.6451e-16      0.00015393      4.9321e-06      5.2242e-06
v  epsilon             4.5672e-11       0.0027419      6.7226e-05       6.774e-05
v  TempC                   24.535          29.974          28.228          28.175
v  Density                 1.1653           1.187          1.1722          1.1724
v  TurbVisc            9.0651e-24      1.1252e-06      6.3932e-08      6.6107e-08
v  CourantNb            0.0018796           8.875          2.2855          2.2205
v  FourierNb              0.41774          2.7144         0.89223         0.84108
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  TempC                      24.42              30          28.271          28.301
v  Boundary Density          1.1653           1.187           1.172          1.1719
v  Yplus                          0          3.4074        0.087767         0.17491


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46249          10.854          3.1778          3.0615


 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         0.247492439E-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 0.29242E-01
   Friction velocity        uet   :  0.15730E-02 0.20677E-01
   Friction velocity        uk    :  0.15730E-02 0.21634E-01
   Dimensionless distance   yplus :  0.20263E+00 0.34134E+01
   Friction thermal sca.    tstar : -0.37414E+01-0.59712E-01
   Rough dim-less th. sca.  tplus :  0.15119E+00 0.25468E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        255
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27439E-05      76   0.74717E-01   0.14851E-04 0.18023E+00 
c  Velocity[X]                                      0.57178E-05 
c  Velocity[Y]                                      0.91333E-05 
c  Velocity[Z]                                      0.30112E-32 
c  Pressure     0.62905E-05     158   0.14811E-02   0.73801E-01 0.46812E-01 
c  k            0.14798E-07      35   0.14066E-04   0.49755E-10 0.44653E+00 
c  epsilon      0.34980E-06      20   0.38936E-05   0.87436E-08 0.42966E+00 
c  TempC        0.23768E+01      62   0.22965E-02   0.14949E-01 0.61206E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -6.1953e-11                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.05755         0.04932      0.00022822      -4.638e-06
v  Velocity[Y]          -0.049687        0.074589       0.0023631      0.00091676
v  Velocity[Z]        -2.4845e-15      2.4817e-15       -3.46e-17     -3.3151e-17
v  ǁVelocityǁ          0.00037266        0.086021         0.02548        0.025511
v  Pressure             -0.015309         0.02722     -0.00028364     -1.9586e-18
v  k                   4.0812e-17      0.00015139      4.5073e-06      4.9085e-06
v  epsilon             3.6339e-11       0.0026836      6.2514e-05       6.423e-05
v  TempC                   24.608          29.975          28.271          28.218
v  Density                 1.1653          1.1866          1.1721          1.1723
v  TurbVisc            1.1479e-24      1.1198e-06      6.1858e-08      6.4399e-08
v  CourantNb             0.022181          8.8538          2.2328          2.1694
v  FourierNb              0.41806          2.7184         0.89141         0.84006
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  TempC                     24.535              30          28.312          28.341
v  Boundary Density          1.1653          1.1866          1.1718          1.1718
v  Yplus                          0          3.4134        0.086025          0.1718


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45985          10.498          3.1242          3.0095


 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         0.137642854E-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 0.29593E-01
   Friction velocity        uet   :  0.64540E-03 0.20430E-01
   Friction velocity        uk    :  0.64540E-03 0.22109E-01
   Dimensionless distance   yplus :  0.10288E+00 0.34106E+01
   Friction thermal sca.    tstar : -0.26489E+02-0.58590E-01
   Rough dim-less th. sca.  tplus :  0.76758E-01 0.25447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        266
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26757E-05      75   0.73266E-01   0.14008E-04 0.18010E+00 
c  Velocity[X]                                      0.57354E-05 
c  Velocity[Y]                                      0.82725E-05 
c  Velocity[Z]                                      0.26513E-32 
c  Pressure     0.62248E-05     163   0.15357E-02   0.73212E-01 0.47718E-01 
c  k            0.14315E-07      36   0.11721E-04   0.37525E-10 0.39966E+00 
c  epsilon      0.33737E-06      26   0.37047E-05   0.10870E-07 0.50206E+00 
c  TempC        0.23793E+01      61   0.20709E-02   0.14705E-01 0.60616E-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]          -0.054299        0.046761      0.00017563     -7.1063e-06
v  Velocity[Y]          -0.048029        0.076133       0.0022513      0.00092187
v  Velocity[Z]        -2.5262e-15      2.5062e-15     -3.5329e-17     -3.3891e-17
v  ǁVelocityǁ           8.825e-05        0.085335        0.024628        0.024688
v  Pressure             -0.015386        0.027472     -0.00027278      5.3002e-19
v  k                     3.43e-16      0.00015429      4.1529e-06      4.6183e-06
v  epsilon             6.8491e-12       0.0028507      5.6067e-05       5.941e-05
v  TempC                   24.677          29.975          28.312          28.259
v  Density                 1.1653          1.1863          1.1719          1.1721
v  TurbVisc            4.8088e-24      1.1136e-06      5.8379e-08      6.1609e-08
v  CourantNb             0.011744          8.7512          2.1691          2.1089
v  FourierNb              0.41811          2.7229         0.89056         0.83959
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  TempC                     24.608              30          28.353           28.38
v  Boundary Density          1.1653          1.1863          1.1717          1.1716
v  Yplus                          0          3.4106        0.083892         0.16793


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45571          10.395          3.0597          2.9485


 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         0.430133919E-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 0.29976E-01
   Friction velocity        uet   :  0.96746E-03 0.20260E-01
   Friction velocity        uk    :  0.96745E-03 0.22333E-01
   Dimensionless distance   yplus :  0.12461E+00 0.34005E+01
   Friction thermal sca.    tstar : -0.57058E+01-0.58846E-01
   Rough dim-less th. sca.  tplus :  0.92976E-01 0.25371E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        268
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26050E-05      74   0.73500E-01   0.13058E-04 0.17932E+00 
c  Velocity[X]                                      0.59085E-05 
c  Velocity[Y]                                      0.71498E-05 
c  Velocity[Z]                                      0.23153E-32 
c  Pressure     0.61003E-05     163   0.15706E-02   0.71914E-01 0.47964E-01 
c  k            0.14095E-07      34   0.83167E-05   0.90126E-11 0.19905E+00 
c  epsilon      0.32578E-06      20   0.31704E-05   0.61820E-08 0.39341E+00 
c  TempC        0.23818E+01      60   0.21022E-02   0.14254E-01 0.59598E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -7.9615e-10                             2
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.051051        0.046113      0.00011183      -7.901e-06
v  Velocity[Y]           -0.04664        0.077077       0.0021626       0.0009303
v  Velocity[Z]        -2.5577e-15      2.5392e-15     -3.6235e-17     -3.4702e-17
v  ǁVelocityǁ          0.00019848        0.083833        0.023723        0.023808
v  Pressure             -0.015459        0.027739     -0.00026218     -1.9411e-18
v  k                   2.8125e-16      0.00015561      3.9992e-06      4.4594e-06
v  epsilon             8.0117e-11       0.0028476      5.1007e-05      5.5217e-05
v  TempC                    24.75          29.976          28.352            28.3
v  Density                 1.1653           1.186          1.1717          1.1719
v  TurbVisc            5.5612e-23      1.1118e-06      5.5478e-08      5.8928e-08
v  CourantNb              0.01192          8.5004          2.0959          2.0391
v  FourierNb              0.41819          2.7262         0.88851         0.83735
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  TempC                     24.677              30          28.392          28.417
v  Boundary Density          1.1653           1.186          1.1715          1.1715
v  Yplus                          0          3.4005        0.081832         0.16414


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4578          10.143          2.9844          2.8765


 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        -0.404987628E-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 0.29967E-01
   Friction velocity        uet   :  0.43228E-03 0.20716E-01
   Friction velocity        uk    :  0.43227E-03 0.22328E-01
   Dimensionless distance   yplus :  0.55691E-01 0.33736E+01
   Friction thermal sca.    tstar : -0.13545E+02-0.59296E-01
   Rough dim-less th. sca.  tplus :  0.41552E-01 0.25171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        269
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25329E-05      74   0.77973E-01   0.12760E-04 0.18315E+00 
c  Velocity[X]                                      0.60913E-05 
c  Velocity[Y]                                      0.66685E-05 
c  Velocity[Z]                                      0.22515E-32 
c  Pressure     0.60083E-05     159   0.15630E-02   0.70949E-01 0.44695E-01 
c  k            0.13813E-07      40   0.97019E-05   0.89725E-11 0.20180E+00 
c  epsilon      0.31548E-06      30   0.34079E-05   0.23251E-08 0.24662E+00 
c  TempC        0.23843E+01      59   0.19903E-02   0.13785E-01 0.58531E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -3.2628e-09                             3
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.047432        0.045449      4.0222e-05     -7.2782e-06
v  Velocity[Y]          -0.045691        0.077077       0.0020879      0.00093599
v  Velocity[Z]        -2.5807e-15      2.5833e-15     -3.6998e-17     -3.5539e-17
v  ǁVelocityǁ          0.00025481        0.081245        0.022786         0.02289
v  Pressure             -0.015531        0.027992     -0.00025269     -2.1499e-18
v  k                   2.2561e-16      0.00015764      3.9199e-06      4.3625e-06
v  epsilon             2.8408e-11        0.002894      4.9119e-05      5.3185e-05
v  TempC                   24.808          29.976          28.391          28.339
v  Density                 1.1653          1.1857          1.1716          1.1718
v  TurbVisc             5.289e-23      1.1082e-06      5.4393e-08      5.7658e-08
v  CourantNb              0.01876          8.1965          2.0155          1.9623
v  FourierNb              0.41836           2.728         0.89172         0.84126
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  TempC                      24.75              30           28.43          28.454
v  Boundary Density          1.1653          1.1857          1.1713          1.1713
v  Yplus                          0          3.3736        0.079963         0.16052


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45718          9.8387          2.9072          2.8036


 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         0.575717706E-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 0.30063E-01
   Friction velocity        uet   :  0.33234E-03 0.20768E-01
   Friction velocity        uk    :  0.33233E-03 0.22392E-01
   Dimensionless distance   yplus :  0.42798E-01 0.33234E+01
   Friction thermal sca.    tstar : -0.12656E+02-0.59021E-01
   Rough dim-less th. sca.  tplus :  0.31932E-01 0.24797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        273
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24603E-05      73   0.74267E-01   0.12902E-04 0.19064E+00 
c  Velocity[X]                                      0.62115E-05 
c  Velocity[Y]                                      0.66906E-05 
c  Velocity[Z]                                      0.21353E-32 
c  Pressure     0.59627E-05     156   0.15279E-02   0.70463E-01 0.40526E-01 
c  k            0.13428E-07      36   0.10797E-04   0.11402E-10 0.23233E+00 
c  epsilon      0.30605E-06      26   0.38900E-05   0.20283E-08 0.23535E+00 
c  TempC        0.23866E+01      57   0.16448E-02   0.13018E-01 0.56803E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.6693e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.044271        0.045468     -3.2779e-05     -8.9916e-06
v  Velocity[Y]          -0.044802        0.076208       0.0020242      0.00094233
v  Velocity[Z]        -2.5952e-15       2.638e-15     -3.7671e-17     -3.6329e-17
v  ǁVelocityǁ          0.00016678        0.078241        0.021834        0.021953
v  Pressure             -0.015619        0.028217     -0.00024445     -1.3128e-18
v  k                     8.06e-17      0.00015649      3.7911e-06      4.2258e-06
v  epsilon             2.4055e-11       0.0028821      4.7829e-05      5.1643e-05
v  TempC                   24.873          29.977          28.428          28.377
v  Density                 1.1653          1.1855          1.1714          1.1716
v  TurbVisc            3.6577e-23      1.1084e-06      5.3764e-08      5.6896e-08
v  CourantNb             0.030563          7.7672           1.931           1.882
v  FourierNb              0.41866          2.7284         0.88938         0.83864
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  TempC                     24.808              30          28.467           28.49
v  Boundary Density          1.1653          1.1855          1.1712          1.1712
v  Yplus                          0          3.3234        0.078905         0.15835


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45155          9.3823          2.8204          2.7206


 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         0.348077602E-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 0.29993E-01
   Friction velocity        uet   :  0.81789E-03 0.20757E-01
   Friction velocity        uk    :  0.81789E-03 0.22334E-01
   Dimensionless distance   yplus :  0.12952E+00 0.32408E+01
   Friction thermal sca.    tstar : -0.52160E+01-0.59747E-01
   Rough dim-less th. sca.  tplus :  0.96638E-01 0.24180E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        279
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23889E-05      71   0.74341E-01   0.13482E-04 0.20195E+00 
c  Velocity[X]                                      0.63036E-05 
c  Velocity[Y]                                      0.71788E-05 
c  Velocity[Z]                                      0.21618E-32 
c  Pressure     0.58389E-05     154   0.15029E-02   0.69023E-01 0.37386E-01 
c  k            0.12895E-07      33   0.10254E-04   0.20703E-10 0.32488E+00 
c  epsilon      0.29547E-06      20   0.33569E-05   0.19769E-08 0.24142E+00 
c  TempC        0.23890E+01      55   0.20523E-02   0.12336E-01 0.55225E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -3.3262e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.0436        0.046482     -0.00010205     -9.3617e-06
v  Velocity[Y]          -0.042975        0.074134       0.0019681      0.00094964
v  Velocity[Z]        -2.6033e-15      2.6986e-15     -3.8107e-17      -3.692e-17
v  ǁVelocityǁ          0.00014329         0.07606        0.020907        0.021033
v  Pressure             -0.015747        0.028425     -0.00023781     -2.7273e-18
v  k                   3.7366e-17      0.00015357      3.5347e-06      3.9859e-06
v  epsilon             5.5178e-11        0.002832      4.5232e-05      4.9081e-05
v  TempC                   24.938          29.977          28.464          28.415
v  Density                 1.1653          1.1852          1.1713          1.1715
v  TurbVisc            3.6781e-25      1.1091e-06      5.2543e-08      5.5673e-08
v  CourantNb             0.019642          7.2724          1.8433          1.7985
v  FourierNb              0.41853          2.7279         0.88825         0.83751
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  TempC                     24.873              30          28.502          28.525
v  Boundary Density          1.1653          1.1852          1.1711           1.171
v  Yplus                          0          3.2408        0.078108         0.15672


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44063          8.8848          2.7315           2.636


 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         0.207787770E-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 0.29728E-01
   Friction velocity        uet   :  0.41875E-03 0.20575E-01
   Friction velocity        uk    :  0.41875E-03 0.22063E-01
   Dimensionless distance   yplus :  0.53923E-01 0.31320E+01
   Friction thermal sca.    tstar : -0.41467E+01-0.60582E-01
   Rough dim-less th. sca.  tplus :  0.40233E-01 0.23368E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        281
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23189E-05      70   0.82190E-01   0.14078E-04 0.21352E+00 
c  Velocity[X]                                      0.63731E-05 
c  Velocity[Y]                                      0.77049E-05 
c  Velocity[Z]                                      0.21858E-32 
c  Pressure     0.60087E-05     154   0.14785E-02   0.71011E-01 0.36958E-01 
c  k            0.12426E-07      33   0.72070E-05   0.17527E-10 0.30902E+00 
c  epsilon      0.28236E-06      22   0.27365E-05   0.44534E-08 0.38201E+00 
c  TempC        0.23914E+01      53   0.17516E-02   0.12729E-01 0.56029E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.7871e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.043299        0.049695     -0.00016895     -8.7231e-06
v  Velocity[Y]          -0.040767        0.071415       0.0019137      0.00095561
v  Velocity[Z]         -2.533e-15      2.7685e-15     -3.8299e-17     -3.7202e-17
v  ǁVelocityǁ           0.0003258        0.072553        0.020068          0.0202
v  Pressure             -0.015944        0.028638     -0.00023188     -1.4391e-19
v  k                   2.3292e-17      0.00015222      3.3179e-06       3.785e-06
v  epsilon             5.1183e-11       0.0027327      4.1538e-05      4.5749e-05
v  TempC                   25.014          29.978          28.498          28.451
v  Density                 1.1653           1.185          1.1711          1.1713
v  TurbVisc            1.9323e-25      1.1086e-06      5.0244e-08       5.353e-08
v  CourantNb             0.011348          6.8419          1.7565          1.7153
v  FourierNb              0.41858           2.727         0.88869         0.83819
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  TempC                     24.938              30          28.536          28.559
v  Boundary Density          1.1653           1.185          1.1709          1.1709
v  Yplus                          0           3.132        0.077173         0.15486


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43234          8.3549          2.6452          2.5535


 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         0.555865372E-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 0.29495E-01
   Friction velocity        uet   :  0.38277E-03 0.20121E-01
   Friction velocity        uk    :  0.38277E-03 0.21864E-01
   Dimensionless distance   yplus :  0.60613E-01 0.30295E+01
   Friction thermal sca.    tstar : -0.36858E+01-0.61406E-01
   Rough dim-less th. sca.  tplus :  0.45224E-01 0.22603E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        282
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.22548E-05      69   0.84658E-01   0.14377E-04 0.22277E+00 
c  Velocity[X]                                      0.61399E-05 
c  Velocity[Y]                                      0.82370E-05 
c  Velocity[Z]                                      0.23172E-32 
c  Pressure     0.63855E-05     153   0.15049E-02   0.75476E-01 0.37023E-01 
c  k            0.12047E-07      33   0.61295E-05   0.19100E-10 0.32917E+00 
c  epsilon      0.26888E-06      21   0.21707E-05   0.53409E-08 0.43727E+00 
c  TempC        0.23937E+01      51   0.22065E-02   0.12444E-01 0.55331E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.1086e-09                             2
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.043011        0.051895     -0.00022731     -7.1443e-06
v  Velocity[Y]          -0.040704        0.067854       0.0018607      0.00096244
v  Velocity[Z]        -2.4977e-15      2.8422e-15     -3.8053e-17     -3.7138e-17
v  ǁVelocityǁ           0.0001735        0.068877        0.019344        0.019479
v  Pressure             -0.016342        0.028853      -0.0002266      -6.248e-19
v  k                    3.472e-17      0.00015031      3.2276e-06      3.7101e-06
v  epsilon             1.4983e-11       0.0027173      3.8843e-05      4.3513e-05
v  TempC                   25.116          29.978          28.532          28.486
v  Density                 1.1653          1.1847           1.171          1.1712
v  TurbVisc            1.4302e-25      1.1071e-06        4.85e-08      5.1967e-08
v  CourantNb            0.0086033           6.407          1.6789          1.6415
v  FourierNb              0.41852          2.7257         0.88878         0.83845
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  TempC                     25.014              30          28.569          28.592
v  Boundary Density          1.1653          1.1847          1.1708          1.1708
v  Yplus                          0          3.0295         0.07625         0.15309


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4296          7.7923          2.5677          2.4799


 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         0.154848211E-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 0.28928E-01
   Friction velocity        uet   :  0.26136E-03 0.20116E-01
   Friction velocity        uk    :  0.26115E-03 0.21318E-01
   Dimensionless distance   yplus :  0.33656E-01 0.30136E+01
   Friction thermal sca.    tstar : -0.12464E+02-0.59625E-01
   Rough dim-less th. sca.  tplus :  0.25111E-01 0.22484E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        281
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.22034E-05      66   0.83287E-01   0.14218E-04 0.22768E+00 
c  Velocity[X]                                      0.59008E-05 
c  Velocity[Y]                                      0.83175E-05 
c  Velocity[Z]                                      0.26033E-32 
c  Pressure     0.63348E-05     153   0.14057E-02   0.74871E-01 0.37436E-01 
c  k            0.11718E-07      32   0.50496E-05   0.12235E-10 0.27019E+00 
c  epsilon      0.25529E-06      23   0.14526E-05   0.25865E-08 0.31946E+00 
c  TempC        0.23959E+01      50   0.19548E-02   0.12698E-01 0.55827E-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]          -0.042611        0.052277     -0.00027553     -5.1002e-06
v  Velocity[Y]          -0.040149        0.065369        0.001807      0.00096758
v  Velocity[Z]        -2.4712e-15      2.9175e-15     -3.7661e-17     -3.6809e-17
v  ǁVelocityǁ          0.00023466        0.065994        0.018799        0.018937
v  Pressure             -0.017018        0.029093     -0.00022232     -2.6571e-18
v  k                   4.3677e-17      0.00014131      3.1388e-06      3.6186e-06
v  epsilon             4.5499e-11       0.0025075      3.6558e-05      4.1357e-05
v  TempC                   25.172          29.978          28.564           28.52
v  Density                 1.1653          1.1843          1.1709           1.171
v  TurbVisc            2.9135e-25      1.1073e-06      4.7831e-08      5.1518e-08
v  CourantNb            0.0087383          6.0534          1.6128          1.5782
v  FourierNb              0.41883          2.7243         0.88875           0.838
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  TempC                     25.116              30          28.601          28.624
v  Boundary Density          1.1653          1.1843          1.1707          1.1707
v  Yplus                          0          3.0136        0.075515         0.15161


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42974           7.228          2.5016          2.4162


 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         0.191905902E-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 0.28258E-01
   Friction velocity        uet   :  0.64842E-03 0.20515E-01
   Friction velocity        uk    :  0.64841E-03 0.20773E-01
   Dimensionless distance   yplus :  0.83496E-01 0.30215E+01
   Friction thermal sca.    tstar : -0.60353E+01-0.56957E-01
   Rough dim-less th. sca.  tplus :  0.62298E-01 0.22544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        285
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21572E-05      65   0.85596E-01   0.14102E-04 0.23222E+00 
c  Velocity[X]                                      0.58229E-05 
c  Velocity[Y]                                      0.82788E-05 
c  Velocity[Z]                                      0.26055E-32 
c  Pressure     0.63074E-05     154   0.12846E-02   0.74502E-01 0.36139E-01 
c  k            0.11251E-07      34   0.11303E-04   0.21640E-10 0.36806E+00 
c  epsilon      0.24429E-06      25   0.40992E-05   0.37680E-08 0.39416E+00 
c  TempC        0.23981E+01      49   0.21723E-02   0.12910E-01 0.56228E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -4.2747e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.041838        0.052983     -0.00031051     -3.6646e-06
v  Velocity[Y]          -0.039238        0.063549       0.0017436      0.00096887
v  Velocity[Z]        -2.4491e-15      2.9944e-15     -3.7151e-17     -3.6261e-17
v  ǁVelocityǁ          0.00032627          0.0703        0.018415        0.018559
v  Pressure             -0.017628        0.029312     -0.00021795     -1.3935e-18
v  k                   1.8509e-18      0.00013887      3.0463e-06      3.5136e-06
v  epsilon             3.4465e-11       0.0024044      3.5912e-05      4.0465e-05
v  TempC                    25.22          29.979          28.596          28.554
v  Density                 1.1653           1.184          1.1707          1.1709
v  TurbVisc            3.8612e-25      1.1047e-06      4.7262e-08      5.1025e-08
v  CourantNb            0.0093575           5.727          1.5627          1.5301
v  FourierNb              0.41881          2.7232         0.88908         0.83853
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  TempC                     25.172              30          28.632          28.655
v  Boundary Density          1.1653           1.184          1.1705          1.1705
v  Yplus                          0          3.0215        0.075013         0.15059


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43036          7.2352          2.4518          2.3687


 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         0.522778147E-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 0.27415E-01
   Friction velocity        uet   :  0.74199E-03 0.19924E-01
   Friction velocity        uk    :  0.74194E-03 0.20085E-01
   Dimensionless distance   yplus :  0.95633E-01 0.30570E+01
   Friction thermal sca.    tstar : -0.60305E+01-0.58537E-01
   Rough dim-less th. sca.  tplus :  0.71353E-01 0.22808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        289
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21215E-05      63   0.87398E-01   0.13416E-04 0.23108E+00 
c  Velocity[X]                                      0.54641E-05 
c  Velocity[Y]                                      0.79518E-05 
c  Velocity[Z]                                      0.29233E-32 
c  Pressure     0.64512E-05     154   0.11939E-02   0.76213E-01 0.35144E-01 
c  k            0.10805E-07      32   0.84299E-05   0.16414E-10 0.33165E+00 
c  epsilon      0.23257E-06      23   0.28986E-05   0.32687E-08 0.38936E+00 
c  TempC        0.24001E+01      48   0.23087E-02   0.13001E-01 0.56364E-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]          -0.041126        0.053188     -0.00033541     -3.1838e-06
v  Velocity[Y]          -0.038245        0.061669       0.0016757      0.00097195
v  Velocity[Z]        -2.4267e-15      3.0631e-15     -3.6736e-17     -3.5673e-17
v  ǁVelocityǁ           0.0001513        0.068972        0.018155        0.018305
v  Pressure             -0.018136         0.02955     -0.00021402     -1.9902e-18
v  k                   1.2303e-18      0.00012952       2.885e-06      3.3505e-06
v  epsilon             2.5182e-11       0.0021795      3.3264e-05      3.7975e-05
v  TempC                   25.259          29.979          28.628          28.586
v  Density                 1.1653          1.1839          1.1706          1.1708
v  TurbVisc            1.0104e-27      1.0994e-06      4.6065e-08      4.9865e-08
v  CourantNb            0.0041747          5.6721          1.5293          1.4992
v  FourierNb              0.41882          2.7195         0.88716         0.83686
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  TempC                      25.22              30          28.663          28.685
v  Boundary Density          1.1653          1.1839          1.1704          1.1704
v  Yplus                          0           3.057        0.074476         0.14951


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43048           7.261          2.4165          2.3361


 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        -0.727918939E-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 0.26563E-01
   Friction velocity        uet   :  0.72794E-03 0.20388E-01
   Friction velocity        uk    :  0.72794E-03 0.19513E-01
   Dimensionless distance   yplus :  0.11527E+00 0.30169E+01
   Friction thermal sca.    tstar : -0.72683E+01-0.59897E-01
   Rough dim-less th. sca.  tplus :  0.86003E-01 0.22510E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20871E-05      61   0.84139E-01   0.13067E-04 0.23174E+00 
c  Velocity[X]                                      0.53044E-05 
c  Velocity[Y]                                      0.77628E-05 
c  Velocity[Z]                                      0.28862E-32 
c  Pressure     0.62035E-05     154   0.11304E-02   0.73311E-01 0.34640E-01 
c  k            0.10347E-07      30   0.68719E-05   0.11766E-10 0.29115E+00 
c  epsilon      0.22095E-06      20   0.16220E-05   0.15545E-08 0.28274E+00 
c  TempC        0.24022E+01      48   0.22137E-02   0.13023E-01 0.56350E-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]          -0.041565         0.05132     -0.00034976      -3.204e-06
v  Velocity[Y]          -0.037452        0.061033       0.0015987      0.00097459
v  Velocity[Z]        -2.4016e-15      3.1184e-15     -3.6627e-17     -3.5253e-17
v  ǁVelocityǁ          0.00021083        0.067499         0.01798        0.018138
v  Pressure             -0.018533         0.02979     -0.00021042      7.5818e-19
v  k                     8.71e-18      0.00012774      2.7203e-06      3.1879e-06
v  epsilon             3.0683e-11       0.0021041      3.0978e-05      3.5584e-05
v  TempC                   25.274           29.98          28.658          28.618
v  Density                 1.1653          1.1837          1.1705          1.1707
v  TurbVisc            7.0469e-28      1.0928e-06      4.4673e-08      4.8541e-08
v  CourantNb            0.0083477          5.4968          1.5078          1.4802
v  FourierNb              0.41873          2.7187         0.88815         0.83793
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  TempC                     25.259              30          28.693          28.715
v  Boundary Density          1.1653          1.1837          1.1703          1.1703
v  Yplus                          0          3.0169        0.073744         0.14804


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42935          7.2163           2.396          2.3181


 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         0.362635981E-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 0.25620E-01
   Friction velocity        uet   :  0.23155E-03 0.20576E-01
   Friction velocity        uk    :  0.23155E-03 0.18904E-01
   Dimensionless distance   yplus :  0.36666E-01 0.30064E+01
   Friction thermal sca.    tstar : -0.46831E+01-0.57326E-01
   Rough dim-less th. sca.  tplus :  0.27357E-01 0.22431E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        297
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20601E-05      59   0.82150E-01   0.12503E-04 0.22938E+00 
c  Velocity[X]                                      0.49560E-05 
c  Velocity[Y]                                      0.75473E-05 
c  Velocity[Z]                                      0.28869E-32 
c  Pressure     0.61067E-05     154   0.11491E-02   0.72239E-01 0.33335E-01 
c  k            0.98097E-08      31   0.10760E-04   0.21293E-10 0.40776E+00 
c  epsilon      0.20974E-06      22   0.18680E-05   0.23462E-08 0.36695E+00 
c  TempC        0.24041E+01      47   0.22727E-02   0.12924E-01 0.56076E-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]          -0.041798        0.051437      -0.0003553     -2.6433e-06
v  Velocity[Y]          -0.038558        0.059079       0.0015122      0.00097661
v  Velocity[Z]        -2.3805e-15      3.1617e-15     -3.6776e-17      -3.504e-17
v  ǁVelocityǁ          9.2682e-05        0.069067        0.017863        0.018031
v  Pressure             -0.018821        0.030024     -0.00020693      1.5901e-18
v  k                   1.9406e-17       0.0001143      2.5157e-06      3.0118e-06
v  epsilon             3.5342e-12       0.0018038      2.8641e-05      3.3452e-05
v  TempC                   25.278           29.98          28.689          28.649
v  Density                 1.1653          1.1836          1.1704          1.1705
v  TurbVisc            1.3481e-25      1.0874e-06      4.3282e-08      4.7298e-08
v  CourantNb            0.0081135          5.3605          1.4939          1.4681
v  FourierNb              0.41873          2.7183         0.88747          0.8371
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  TempC                     25.274              30          28.722          28.744
v  Boundary Density          1.1653          1.1836          1.1702          1.1702
v  Yplus                          0          3.0064         0.07293         0.14651


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42912          7.0804          2.3814          2.3052


 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        -0.156171700E-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 0.25056E-01
   Friction velocity        uet   :  0.48237E-03 0.20549E-01
   Friction velocity        uk    :  0.48237E-03 0.19162E-01
   Dimensionless distance   yplus :  0.76385E-01 0.30464E+01
   Friction thermal sca.    tstar : -0.17292E+02-0.54262E-01
   Rough dim-less th. sca.  tplus :  0.56992E-01 0.22730E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20395E-05      58   0.79224E-01   0.11898E-04 0.22564E+00 
c  Velocity[X]                                      0.47688E-05 
c  Velocity[Y]                                      0.71288E-05 
c  Velocity[Z]                                      0.27124E-32 
c  Pressure     0.60127E-05     154   0.12826E-02   0.71182E-01 0.32347E-01 
c  k            0.94062E-08      30   0.10346E-04   0.15871E-10 0.36334E+00 
c  epsilon      0.19995E-06      20   0.32747E-05   0.37681E-08 0.49229E+00 
c  TempC        0.24060E+01      46   0.19468E-02   0.12497E-01 0.55086E-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]          -0.041859        0.048685     -0.00035208     -2.4769e-06
v  Velocity[Y]           -0.03677        0.058016       0.0014241      0.00097897
v  Velocity[Z]        -2.3549e-15      3.1907e-15     -3.7071e-17     -3.4904e-17
v  ǁVelocityǁ          8.4427e-05        0.065833        0.017788        0.017968
v  Pressure             -0.019046        0.030271     -0.00020374     -2.2886e-18
v  k                   1.5512e-17      0.00011335      2.3591e-06      2.8611e-06
v  epsilon             1.8781e-11       0.0017708      2.5912e-05      3.1093e-05
v  TempC                   25.331          29.981          28.718          28.679
v  Density                 1.1653          1.1836          1.1703          1.1704
v  TurbVisc            2.3835e-25      1.0842e-06      4.1513e-08      4.5841e-08
v  CourantNb            0.0094583          5.1568          1.4859           1.461
v  FourierNb              0.41882          2.7181          0.8881         0.83801
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  TempC                     25.278              30          28.751          28.771
v  Boundary Density          1.1653          1.1836          1.1701          1.1701
v  Yplus                          0          3.0464        0.072242         0.14524


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43047          6.9912           2.374           2.299


 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         0.199846836E-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 0.24682E-01
   Friction velocity        uet   :  0.62496E-03 0.18167E-01
   Friction velocity        uk    :  0.62496E-03 0.18661E-01
   Dimensionless distance   yplus :  0.98964E-01 0.29657E+01
   Friction thermal sca.    tstar : -0.52429E+01-0.56598E-01
   Rough dim-less th. sca.  tplus :  0.73838E-01 0.22127E+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
------------------------------------------------------------




 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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20200E-05      57   0.73296E-01   0.11094E-04 0.21884E+00 
c  Velocity[X]                                      0.46165E-05 
c  Velocity[Y]                                      0.64776E-05 
c  Velocity[Z]                                      0.27134E-32 
c  Pressure     0.59441E-05     154   0.12522E-02   0.70507E-01 0.32342E-01 
c  k            0.92401E-08      29   0.84774E-05   0.86861E-11 0.27442E+00 
c  epsilon      0.19125E-06      19   0.21694E-05   0.29911E-08 0.45979E+00 
c  TempC        0.24078E+01      46   0.18237E-02   0.11384E-01 0.52525E-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]          -0.042165        0.049246     -0.00033959     -2.9542e-06
v  Velocity[Y]          -0.036451        0.057601       0.0013414      0.00098201
v  Velocity[Z]        -2.3313e-15      3.2085e-15     -3.7061e-17     -3.4676e-17
v  ǁVelocityǁ          0.00030935        0.064795        0.017758        0.017948
v  Pressure             -0.019244        0.030538      -0.0002011     -1.3373e-18
v  k                   1.1406e-17      0.00011167      2.2817e-06      2.7724e-06
v  epsilon             2.0506e-11       0.0012311      2.3819e-05       2.913e-05
v  TempC                   25.396          29.981          28.748          28.708
v  Density                 1.1653          1.1834          1.1701          1.1703
v  TurbVisc            1.5203e-25      1.0818e-06      4.0082e-08      4.4491e-08
v  CourantNb             0.013007          5.0519          1.4825          1.4586
v  FourierNb              0.41881          2.7179         0.88743         0.83719
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  TempC                     25.331              30          28.779          28.799
v  Boundary Density          1.1653          1.1834            1.17          1.1699
v  Yplus                          0          2.9657        0.071241         0.14343


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43402          7.1869          2.3699          2.2958


 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        -0.292491065E-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 0.24534E-01
   Friction velocity        uet   :  0.49015E-03 0.17019E-01
   Friction velocity        uk    :  0.49015E-03 0.18489E-01
   Dimensionless distance   yplus :  0.63116E-01 0.29367E+01
   Friction thermal sca.    tstar : -0.32880E+01-0.53105E-01
   Rough dim-less th. sca.  tplus :  0.47091E-01 0.21911E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20083E-05      56   0.66897E-01   0.10188E-04 0.21017E+00 
c  Velocity[X]                                      0.43528E-05 
c  Velocity[Y]                                      0.58353E-05 
c  Velocity[Z]                                      0.26935E-32 
c  Pressure     0.55403E-05     154   0.12441E-02   0.65850E-01 0.31273E-01 
c  k            0.91441E-08      28   0.83884E-05   0.20609E-10 0.42618E+00 
c  epsilon      0.18626E-06      18   0.23416E-05   0.27897E-08 0.44780E+00 
c  TempC        0.24095E+01      46   0.18830E-02   0.11136E-01 0.51899E-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]          -0.041264         0.04581     -0.00032083     -2.5591e-06
v  Velocity[Y]          -0.034822        0.056353       0.0012646      0.00098415
v  Velocity[Z]         -2.316e-15      3.2137e-15     -3.6827e-17      -3.438e-17
v  ǁVelocityǁ          7.9957e-05        0.063237        0.017727        0.017919
v  Pressure             -0.019419        0.030805      -0.0001982       1.555e-18
v  k                    8.274e-18      0.00010943       2.285e-06      2.7781e-06
v  epsilon             1.0956e-11       0.0011997      2.3865e-05      2.9254e-05
v  TempC                   25.433          29.981          28.777          28.736
v  Density                 1.1652          1.1832            1.17          1.1702
v  TurbVisc            8.9591e-26      1.0767e-06      3.9136e-08       4.352e-08
v  CourantNb            0.0061014          5.1484          1.4815          1.4582
v  FourierNb              0.41867          2.7177         0.88904         0.83915
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  TempC                     25.396              30          28.807          28.825
v  Boundary Density          1.1652          1.1832          1.1699          1.1698
v  Yplus                          0          2.9367        0.070599         0.14233


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42713          7.2887          2.3705          2.2974


 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         0.644539133E-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 0.24417E-01
   Friction velocity        uet   :  0.73281E-03 0.17073E-01
   Friction velocity        uk    :  0.73281E-03 0.18325E-01
   Dimensionless distance   yplus :  0.11309E+00 0.29113E+01
   Friction thermal sca.    tstar : -0.55526E+01-0.53000E-01
   Rough dim-less th. sca.  tplus :  0.84374E-01 0.21721E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19957E-05      56   0.68471E-01   0.92663E-05 0.20110E+00 
c  Velocity[X]                                      0.40676E-05 
c  Velocity[Y]                                      0.51987E-05 
c  Velocity[Z]                                      0.24571E-32 
c  Pressure     0.53915E-05     153   0.12412E-02   0.64236E-01 0.30121E-01 
c  k            0.90366E-08      29   0.62557E-05   0.28044E-10 0.50256E+00 
c  epsilon      0.18362E-06      18   0.14652E-05   0.38356E-08 0.52401E+00 
c  TempC        0.24112E+01      47   0.16153E-02   0.10941E-01 0.51393E-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]          -0.042038        0.045349     -0.00030478     -2.3208e-06
v  Velocity[Y]          -0.034963        0.055666       0.0011949      0.00098253
v  Velocity[Z]        -2.3111e-15      3.2082e-15     -3.6314e-17     -3.3982e-17
v  ǁVelocityǁ          0.00010612        0.066236        0.017646        0.017827
v  Pressure             -0.019822        0.031064      -0.0001951     -8.5646e-19
v  k                   4.3405e-18       0.0001067      2.2579e-06      2.7466e-06
v  epsilon             1.4749e-11       0.0012633      2.3952e-05      2.9372e-05
v  TempC                   25.575          29.981          28.806          28.764
v  Density                 1.1652           1.183          1.1699          1.1701
v  TurbVisc            5.3991e-26      1.0701e-06      3.8744e-08      4.3224e-08
v  CourantNb              0.00335          5.1264          1.4794          1.4558
v  FourierNb              0.41853          2.7177         0.88669         0.83625
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  TempC                     25.433              30          28.835          28.851
v  Boundary Density          1.1652           1.183          1.1697          1.1697
v  Yplus                          0          2.9113         0.06969          0.1407


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42438          7.3369          2.3661           2.292


 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         0.754388719E-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 0.24800E-01
   Friction velocity        uet   :  0.70406E-03 0.16341E-01
   Friction velocity        uk    :  0.70406E-03 0.18796E-01
   Dimensionless distance   yplus :  0.11148E+00 0.29859E+01
   Friction thermal sca.    tstar : -0.41323E+01-0.53813E-01
   Rough dim-less th. sca.  tplus :  0.83177E-01 0.22278E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19774E-05      56   0.63556E-01   0.81583E-05 0.18976E+00 
c  Velocity[X]                                      0.36327E-05 
c  Velocity[Y]                                      0.45256E-05 
c  Velocity[Z]                                      0.24787E-32 
c  Pressure     0.52805E-05     150   0.11836E-02   0.63015E-01 0.28262E-01 
c  k            0.90883E-08      29   0.12022E-04   0.23692E-10 0.45866E+00 
c  epsilon      0.18193E-06      22   0.35684E-05   0.46227E-08 0.57825E+00 
c  TempC        0.24128E+01      47   0.17110E-02   0.10191E-01 0.49555E-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]          -0.043027        0.045114     -0.00028475     -1.3909e-06
v  Velocity[Y]          -0.035009        0.055537        0.001138      0.00098154
v  Velocity[Z]        -2.3232e-15      3.1897e-15     -3.5544e-17     -3.3431e-17
v  ǁVelocityǁ          0.00027156        0.065953        0.017504        0.017666
v  Pressure             -0.020266        0.031317     -0.00019191      2.2745e-18
v  k                   2.8412e-18      0.00010352      2.2868e-06      2.7833e-06
v  epsilon             6.0091e-12       0.0012594      2.3783e-05      2.9165e-05
v  TempC                   25.656          29.982          28.835          28.792
v  Density                 1.1652          1.1824          1.1698            1.17
v  TurbVisc            6.5083e-27      1.0545e-06      3.7862e-08      4.2322e-08
v  CourantNb            0.0059937          5.1782          1.4743           1.449
v  FourierNb              0.41818          2.7178         0.88776         0.83754
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  TempC                     25.575              30          28.863          28.877
v  Boundary Density          1.1652          1.1824          1.1696          1.1696
v  Yplus                          0          2.9859        0.068665         0.13886


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42702           7.347          2.3621          2.2866


 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         0.558512350E-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 0.24784E-01
   Friction velocity        uet   :  0.21946E-03 0.16945E-01
   Friction velocity        uk    :  0.21946E-03 0.18751E-01
   Dimensionless distance   yplus :  0.34749E-01 0.29769E+01
   Friction thermal sca.    tstar : -0.31672E+01-0.51823E-01
   Rough dim-less th. sca.  tplus :  0.25927E-01 0.22211E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        302
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19576E-05      56   0.63383E-01   0.72726E-05 0.18108E+00 
c  Velocity[X]                                      0.32266E-05 
c  Velocity[Y]                                      0.40459E-05 
c  Velocity[Z]                                      0.24765E-32 
c  Pressure     0.50971E-05     148   0.10951E-02   0.60899E-01 0.24841E-01 
c  k            0.89424E-08      28   0.10222E-04   0.26949E-10 0.50207E+00 
c  epsilon      0.18094E-06      18   0.26548E-05   0.23520E-08 0.41238E+00 
c  TempC        0.24144E+01      47   0.15309E-02   0.96755E-02 0.48240E-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]          -0.042758        0.046631     -0.00026115     -2.8674e-07
v  Velocity[Y]          -0.035432        0.056996       0.0011014      0.00098197
v  Velocity[Z]        -2.3544e-15      3.1675e-15     -3.4899e-17     -3.3008e-17
v  ǁVelocityǁ          0.00012177         0.06695        0.017259          0.0174
v  Pressure             -0.020582        0.031536     -0.00018869      4.0717e-19
v  k                   5.6936e-18      0.00010254      2.2053e-06      2.6846e-06
v  epsilon             3.3744e-13       0.0013192      2.3749e-05      2.9125e-05
v  TempC                   25.737          29.982          28.863          28.819
v  Density                 1.1652          1.1821          1.1697          1.1699
v  TurbVisc            1.7025e-26      1.0395e-06      3.7786e-08      4.2411e-08
v  CourantNb            0.0013619          5.2545          1.4637          1.4362
v  FourierNb              0.41832           2.718         0.88681         0.83635
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  TempC                     25.656              30           28.89          28.902
v  Boundary Density          1.1652          1.1821          1.1695          1.1695
v  Yplus                          0          2.9769         0.06758         0.13693


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42238          7.3192          2.3505          2.2725


 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         0.121760986E-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 0.24915E-01
   Friction velocity        uet   :  0.42358E-03 0.16964E-01
   Friction velocity        uk    :  0.42358E-03 0.18950E-01
   Dimensionless distance   yplus :  0.67496E-01 0.30082E+01
   Friction thermal sca.    tstar : -0.38422E+02-0.48784E-01
   Rough dim-less th. sca.  tplus :  0.50360E-01 0.22445E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        309
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19269E-05      56   0.56721E-01   0.74708E-05 0.18654E+00 
c  Velocity[X]                                      0.32929E-05 
c  Velocity[Y]                                      0.41778E-05 
c  Velocity[Z]                                      0.22912E-32 
c  Pressure     0.47449E-05     148   0.10195E-02   0.56746E-01 0.22222E-01 
c  k            0.85676E-08      29   0.13667E-04   0.42111E-10 0.67182E+00 
c  epsilon      0.17884E-06      19   0.34357E-05   0.32462E-08 0.49671E+00 
c  TempC        0.24158E+01      47   0.13388E-02   0.91746E-02 0.46932E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.3641e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.041622        0.047181     -0.00023636         1.3e-06
v  Velocity[Y]          -0.035733        0.060236       0.0010875      0.00098372
v  Velocity[Z]        -2.3978e-15      3.1399e-15     -3.4538e-17     -3.2713e-17
v  ǁVelocityǁ          0.00021128        0.069583         0.01691        0.017032
v  Pressure             -0.020752        0.031715     -0.00018549     -3.4399e-18
v  k                   5.3746e-18      0.00010437      1.9829e-06      2.4132e-06
v  epsilon             1.4612e-12       0.0013283      2.2818e-05      2.7983e-05
v  TempC                   25.804          29.983          28.892          28.846
v  Density                 1.1652          1.1818          1.1696          1.1697
v  TurbVisc            2.9601e-26      1.0239e-06      3.6162e-08      4.0602e-08
v  CourantNb            0.0054317           5.299          1.4436          1.4142
v  FourierNb              0.41837          2.7182         0.88736         0.83702
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  TempC                     25.737              30          28.917          28.926
v  Boundary Density          1.1652          1.1818          1.1694          1.1694
v  Yplus                          0          3.0082         0.06629         0.13449


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42976          7.2743           2.331          2.2512


 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         0.291167576E-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 0.25233E-01
   Friction velocity        uet   :  0.27700E-03 0.16920E-01
   Friction velocity        uk    :  0.27700E-03 0.19321E-01
   Dimensionless distance   yplus :  0.43861E-01 0.30667E+01
   Friction thermal sca.    tstar : -0.74805E+01-0.46741E-01
   Rough dim-less th. sca.  tplus :  0.32725E-01 0.22881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        318
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18909E-05      56   0.58652E-01   0.72918E-05 0.18834E+00 
c  Velocity[X]                                      0.31071E-05 
c  Velocity[Y]                                      0.41847E-05 
c  Velocity[Z]                                      0.22424E-32 
c  Pressure     0.47386E-05     150   0.96381E-03   0.56743E-01 0.20504E-01 
c  k            0.82089E-08      29   0.15727E-04   0.53513E-10 0.78958E+00 
c  epsilon      0.17594E-06      19   0.41955E-05   0.75983E-08 0.77842E+00 
c  TempC        0.24174E+01      46   0.17276E-02   0.83234E-02 0.44662E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.9083e-09                             2
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.038427         0.04773     -0.00021139      1.6484e-06
v  Velocity[Y]          -0.036239        0.062369       0.0010962      0.00098679
v  Velocity[Z]        -2.4542e-15      3.1116e-15     -3.4323e-17     -3.2246e-17
v  ǁVelocityǁ          8.5149e-05        0.071712        0.016491        0.016597
v  Pressure             -0.020891         0.03188     -0.00018213      3.9383e-18
v  k                   5.2318e-18      0.00010821      1.8324e-06      2.2299e-06
v  epsilon             2.3402e-12        0.001394       2.161e-05      2.6503e-05
v  TempC                   25.866          29.983          28.919          28.872
v  Density                 1.1652          1.1815          1.1695          1.1696
v  TurbVisc            2.2646e-26      1.0087e-06      3.2806e-08      3.6677e-08
v  CourantNb            0.0075171          5.3278          1.4126          1.3819
v  FourierNb              0.41815          2.7185         0.88717         0.83676
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  TempC                     25.804              30          28.944          28.951
v  Boundary Density          1.1652          1.1815          1.1693          1.1693
v  Yplus                          0          3.0667         0.06516         0.13235


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43157          7.1828          2.2998          2.2187


 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        -0.338813179E-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 0.25451E-01
   Friction velocity        uet   :  0.50076E-03 0.16926E-01
   Friction velocity        uk    :  0.50072E-03 0.19635E-01
   Dimensionless distance   yplus :  0.64486E-01 0.31163E+01
   Friction thermal sca.    tstar : -0.93394E+01-0.44995E-01
   Rough dim-less th. sca.  tplus :  0.48113E-01 0.23251E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        328
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18520E-05      56   0.55241E-01   0.73982E-05 0.19479E+00 
c  Velocity[X]                                      0.30519E-05 
c  Velocity[Y]                                      0.43463E-05 
c  Velocity[Z]                                      0.23699E-32 
c  Pressure     0.48751E-05     153   0.98654E-03   0.58444E-01 0.18719E-01 
c  k            0.78226E-08      29   0.15532E-04   0.33441E-10 0.67003E+00 
c  epsilon      0.17081E-06      19   0.40415E-05   0.40445E-08 0.60631E+00 
c  TempC        0.24188E+01      45   0.12762E-02   0.79638E-02 0.43649E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.1076e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.035016        0.046936     -0.00018138      3.1835e-06
v  Velocity[Y]          -0.036466        0.064115       0.0011277      0.00099112
v  Velocity[Z]        -2.5244e-15      3.0871e-15     -3.4031e-17     -3.1647e-17
v  ǁVelocityǁ          0.00010368        0.073178        0.016045        0.016139
v  Pressure             -0.021389        0.032032     -0.00017884     -4.3525e-19
v  k                   6.2556e-18      0.00011103      1.5878e-06      1.9311e-06
v  epsilon             1.2284e-11       0.0014515      1.9026e-05      2.3332e-05
v  TempC                   25.964          29.984          28.946          28.898
v  Density                 1.1652          1.1813          1.1694          1.1695
v  TurbVisc            2.3239e-26      9.8981e-07      3.0364e-08      3.3874e-08
v  CourantNb            0.0057644          5.3659          1.3766          1.3459
v  FourierNb              0.41831          2.7189           0.887         0.83654
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  TempC                     25.866              30           28.97          28.975
v  Boundary Density          1.1652          1.1813          1.1692          1.1692
v  Yplus                          0          3.1163        0.063915         0.12988


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42678          7.0702          2.2636          2.1825


 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         0.103232140E-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 0.25592E-01
   Friction velocity        uet   :  0.40196E-03 0.16959E-01
   Friction velocity        uk    :  0.40196E-03 0.19850E-01
   Dimensionless distance   yplus :  0.63649E-01 0.31502E+01
   Friction thermal sca.    tstar : -0.38900E+01-0.44745E-01
   Rough dim-less th. sca.  tplus :  0.47489E-01 0.23504E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18060E-05      56   0.55052E-01   0.78531E-05 0.20677E+00 
c  Velocity[X]                                      0.32064E-05 
c  Velocity[Y]                                      0.46467E-05 
c  Velocity[Z]                                      0.22489E-32 
c  Pressure     0.47226E-05     152   0.10090E-02   0.56620E-01 0.17863E-01 
c  k            0.72764E-08      28   0.10678E-04   0.30233E-10 0.69826E+00 
c  epsilon      0.16424E-06      18   0.23019E-05   0.27645E-08 0.53577E+00 
c  TempC        0.24204E+01      44   0.16714E-02   0.72738E-02 0.41679E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.6383e-09                             2
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.031231        0.045364     -0.00014789      4.6165e-06
v  Velocity[Y]          -0.036486        0.064524       0.0011791       0.0009958
v  Velocity[Z]        -2.5856e-15      3.0667e-15     -3.3931e-17     -3.1043e-17
v  ǁVelocityǁ          0.00024728        0.073093        0.015592        0.015682
v  Pressure             -0.021856        0.032167     -0.00017569      3.0538e-18
v  k                     1.04e-18      0.00011395      1.3302e-06      1.6164e-06
v  epsilon             4.5108e-12       0.0015038      1.6462e-05      2.0187e-05
v  TempC                   26.059          29.984          28.972          28.924
v  Density                 1.1652          1.1809          1.1693          1.1694
v  TurbVisc            2.8603e-26      9.7813e-07      2.7347e-08       3.036e-08
v  CourantNb            0.0087706          5.4287          1.3382          1.3081
v  FourierNb              0.41826          2.7192          0.8851         0.83419
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  TempC                     25.964              30          28.996          28.999
v  Boundary Density          1.1652          1.1809          1.1691          1.1692
v  Yplus                          0          3.1502        0.062694         0.12738


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42979          6.8892          2.2234          2.1423


 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         0.264697796E-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 0.25609E-01
   Friction velocity        uet   :  0.86735E-03 0.16814E-01
   Friction velocity        uk    :  0.86735E-03 0.19819E-01
   Dimensionless distance   yplus :  0.13734E+00 0.31453E+01
   Friction thermal sca.    tstar : -0.42164E+01-0.45320E-01
   Rough dim-less th. sca.  tplus :  0.10247E+00 0.23468E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        347
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17625E-05      55   0.58966E-01   0.81461E-05 0.21710E+00 
c  Velocity[X]                                      0.33803E-05 
c  Velocity[Y]                                      0.47658E-05 
c  Velocity[Z]                                      0.25340E-32 
c  Pressure     0.47801E-05     153   0.99162E-03   0.57261E-01 0.17133E-01 
c  k            0.66941E-08      29   0.16645E-04   0.29264E-10 0.75132E+00 
c  epsilon      0.15624E-06      21   0.41515E-05   0.32475E-08 0.62782E+00 
c  TempC        0.24218E+01      42   0.11312E-02   0.72989E-02 0.41716E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -6.6548e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.034563        0.042969     -0.00011287      4.5273e-06
v  Velocity[Y]          -0.036477        0.064918       0.0012474       0.0010023
v  Velocity[Z]        -2.6236e-15      3.0499e-15     -3.3653e-17     -3.0448e-17
v  ǁVelocityǁ           0.0002119        0.072384        0.015157        0.015255
v  Pressure             -0.022293        0.032294     -0.00017291      2.4079e-18
v  k                   3.5848e-19      0.00011396       1.102e-06      1.3375e-06
v  epsilon             5.1867e-12       0.0014977      1.3846e-05      1.6977e-05
v  TempC                   26.157          29.984          28.996          28.949
v  Density                 1.1652          1.1805          1.1692          1.1693
v  TurbVisc            8.9997e-28      9.5799e-07      2.4075e-08      2.6527e-08
v  CourantNb            0.0083151          5.3988          1.2991          1.2705
v  FourierNb               0.4185          2.7196         0.88543         0.83458
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  TempC                     26.059              30           29.02          29.022
v  Boundary Density          1.1652          1.1805           1.169          1.1691
v  Yplus                          0          3.1453        0.061416         0.12469


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42934          6.6834          2.1846          2.1051


 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         0.370576914E-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 0.25570E-01
   Friction velocity        uet   :  0.77836E-03 0.16543E-01
   Friction velocity        uk    :  0.77833E-03 0.19742E-01
   Dimensionless distance   yplus :  0.10030E+00 0.31329E+01
   Friction thermal sca.    tstar : -0.41348E+01-0.44845E-01
   Rough dim-less th. sca.  tplus :  0.74834E-01 0.23375E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17187E-05      54   0.56520E-01   0.80310E-05 0.22157E+00 
c  Velocity[X]                                      0.34371E-05 
c  Velocity[Y]                                      0.45939E-05 
c  Velocity[Z]                                      0.27802E-32 
c  Pressure     0.46276E-05     154   0.98690E-03   0.55346E-01 0.18485E-01 
c  k            0.64698E-08      28   0.11363E-04   0.68686E-11 0.37878E+00 
c  epsilon      0.14736E-06      16   0.27209E-05   0.26161E-08 0.61791E+00 
c  TempC        0.24233E+01      41   0.15483E-02   0.69046E-02 0.40541E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.7627e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.037332        0.040207     -7.3769e-05      5.9879e-06
v  Velocity[Y]          -0.036219        0.064296       0.0013219       0.0010072
v  Velocity[Z]        -2.6019e-15      3.0347e-15     -3.3322e-17     -2.9808e-17
v  ǁVelocityǁ          7.3819e-05        0.071251        0.014766        0.014882
v  Pressure             -0.022731        0.032438     -0.00017038      6.7394e-19
v  k                   2.8837e-18      0.00011319      1.0017e-06      1.2157e-06
v  epsilon             7.3882e-12       0.0014753      1.1355e-05      1.3922e-05
v  TempC                   26.264          29.984           29.02          28.973
v  Density                 1.1652          1.1801          1.1691          1.1692
v  TurbVisc            2.6115e-27      9.1134e-07      2.1229e-08      2.3212e-08
v  CourantNb            0.0058167          5.3692          1.2594          1.2334
v  FourierNb               0.4185            2.72         0.88489         0.83391
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  TempC                     26.157              30          29.044          29.044
v  Boundary Density          1.1652          1.1801          1.1689           1.169
v  Yplus                          0          3.1329        0.060697         0.12288


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42684          6.6557          2.1443          2.0673


 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        -0.190582413E-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 0.25502E-01
   Friction velocity        uet   :  0.52247E-03 0.16282E-01
   Friction velocity        uk    :  0.52247E-03 0.19614E-01
   Dimensionless distance   yplus :  0.82733E-01 0.31123E+01
   Friction thermal sca.    tstar : -0.32457E+01-0.43218E-01
   Rough dim-less th. sca.  tplus :  0.61728E-01 0.23221E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        350
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16827E-05      53   0.60332E-01   0.79113E-05 0.22537E+00 
c  Velocity[X]                                      0.34319E-05 
c  Velocity[Y]                                      0.44794E-05 
c  Velocity[Z]                                      0.28985E-32 
c  Pressure     0.47217E-05     155   0.94412E-03   0.56346E-01 0.17410E-01 
c  k            0.61754E-08      28   0.10559E-04   0.71612E-11 0.39912E+00 
c  epsilon      0.13939E-06      20   0.24577E-05   0.10295E-08 0.40374E+00 
c  TempC        0.24248E+01      41   0.10822E-02   0.68889E-02 0.40463E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -5.6039e-12                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.03963        0.037205      -3.366e-05      7.4682e-06
v  Velocity[Y]          -0.035695        0.063078       0.0014053       0.0010135
v  Velocity[Z]        -2.5496e-15      3.0212e-15     -3.2679e-17     -2.9051e-17
v  ǁVelocityǁ           0.0001405        0.069115        0.014421        0.014561
v  Pressure             -0.023102        0.032577     -0.00016819      2.9836e-18
v  k                    2.329e-18      0.00011082      9.4805e-07      1.1505e-06
v  epsilon             5.6039e-12       0.0014439      1.0444e-05      1.2802e-05
v  TempC                   26.377          29.984          29.043          28.996
v  Density                 1.1652          1.1797           1.169          1.1692
v  TurbVisc            5.2803e-27      9.1262e-07      2.0088e-08      2.1975e-08
v  CourantNb             0.006203          5.2519          1.2222             1.2
v  FourierNb              0.41879          2.7204         0.88509         0.83414
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  TempC                     26.264              30          29.067          29.066
v  Boundary Density          1.1652          1.1797          1.1688          1.1689
v  Yplus                          0          3.1123        0.060149         0.12144


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42722          6.6089          2.1073          2.0341


 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         0.899972506E-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 0.25335E-01
   Friction velocity        uet   :  0.12079E-02 0.16806E-01
   Friction velocity        uk    :  0.12078E-02 0.19339E-01
   Dimensionless distance   yplus :  0.15562E+00 0.30683E+01
   Friction thermal sca.    tstar : -0.28781E+01-0.41307E-01
   Rough dim-less th. sca.  tplus :  0.11611E+00 0.22893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        351
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16523E-05      52   0.58412E-01   0.79057E-05 0.22992E+00 
c  Velocity[X]                                      0.33874E-05 
c  Velocity[Y]                                      0.45183E-05 
c  Velocity[Z]                                      0.32594E-32 
c  Pressure     0.46237E-05     156   0.93115E-03   0.55032E-01 0.17296E-01 
c  k            0.58745E-08      28   0.11394E-04   0.80614E-11 0.44937E+00 
c  epsilon      0.13207E-06      17   0.24520E-05   0.50272E-09 0.30035E+00 
c  TempC        0.24262E+01      41   0.17057E-02   0.65946E-02 0.39560E-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]          -0.042497        0.037777      4.6753e-06      8.2308e-06
v  Velocity[Y]          -0.035286        0.061044       0.0014916       0.0010197
v  Velocity[Z]        -2.4804e-15      3.0075e-15      -3.169e-17     -2.8156e-17
v  ǁVelocityǁ          0.00017821        0.065792         0.01415        0.014315
v  Pressure             -0.023474        0.032716     -0.00016634     -3.1029e-18
v  k                   2.7501e-18      0.00010858       8.649e-07      1.0496e-06
v  epsilon             6.4256e-12       0.0014032      9.5111e-06      1.1661e-05
v  TempC                   26.491          29.985          29.065          29.018
v  Density                 1.1652          1.1793          1.1689          1.1691
v  TurbVisc            4.6278e-27      9.0652e-07      1.9087e-08      2.0907e-08
v  CourantNb            0.0048833          5.1154          1.1879          1.1702
v  FourierNb              0.41882          2.7207         0.88494         0.83396
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  TempC                     26.377              30          29.088          29.087
v  Boundary Density          1.1652          1.1793          1.1687          1.1688
v  Yplus                          0          3.0683         0.05958         0.12005


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4259           6.499          2.0729          2.0042


 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         0.111173074E-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 0.25017E-01
   Friction velocity        uet   :  0.10175E-03 0.16772E-01
   Friction velocity        uk    :  0.10175E-03 0.18891E-01
   Dimensionless distance   yplus :  0.13104E-01 0.29968E+01
   Friction thermal sca.    tstar : -0.98345E+01-0.41175E-01
   Rough dim-less th. sca.  tplus :  0.97768E-02 0.22359E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        355
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16291E-05      51   0.60865E-01   0.78612E-05 0.23310E+00 
c  Velocity[X]                                      0.32898E-05 
c  Velocity[Y]                                      0.45714E-05 
c  Velocity[Z]                                      0.35140E-32 
c  Pressure     0.46508E-05     156   0.92636E-03   0.55164E-01 0.16047E-01 
c  k            0.54000E-08      28   0.14141E-04   0.17486E-10 0.71127E+00 
c  epsilon      0.12467E-06      19   0.24080E-05   0.14552E-08 0.54004E+00 
c  TempC        0.24276E+01      41   0.10505E-02   0.63064E-02 0.38657E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -7.1758e-11                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.043282        0.039819       3.969e-05      8.7872e-06
v  Velocity[Y]          -0.034689        0.058756       0.0015798       0.0010271
v  Velocity[Z]        -2.4019e-15      2.9941e-15     -3.0483e-17     -2.7091e-17
v  ǁVelocityǁ          0.00016883        0.062715        0.013938        0.014121
v  Pressure             -0.023807         0.03285     -0.00016487      1.0811e-18
v  k                   2.3664e-18       0.0001062      7.7215e-07      9.3649e-07
v  epsilon             6.2576e-13       0.0013308      8.8923e-06      1.0902e-05
v  TempC                   26.601          29.986          29.085           29.04
v  Density                 1.1652          1.1788          1.1688           1.169
v  TurbVisc            1.2819e-26      9.0025e-07      1.7896e-08      1.9582e-08
v  CourantNb            0.0054403          4.9684          1.1592          1.1459
v  FourierNb              0.41907          2.7211         0.88444         0.83333
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  TempC                     26.491              30          29.109          29.107
v  Boundary Density          1.1652          1.1788          1.1687          1.1687
v  Yplus                          0          2.9968        0.058986         0.11861


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42646           6.352          2.0437          1.9793


 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         0.121760986E-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 0.24691E-01
   Friction velocity        uet   :  0.52923E-03 0.16904E-01
   Friction velocity        uk    :  0.52906E-03 0.18481E-01
   Dimensionless distance   yplus :  0.68154E-01 0.29314E+01
   Friction thermal sca.    tstar : -0.37876E+01-0.41474E-01
   Rough dim-less th. sca.  tplus :  0.50850E-01 0.21871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        360
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16082E-05      51   0.57692E-01   0.77760E-05 0.23495E+00 
c  Velocity[X]                                      0.31659E-05 
c  Velocity[Y]                                      0.46100E-05 
c  Velocity[Z]                                      0.35622E-32 
c  Pressure     0.45041E-05     155   0.92697E-03   0.53245E-01 0.16041E-01 
c  k            0.48701E-08      28   0.15828E-04   0.18830E-10 0.82700E+00 
c  epsilon      0.11724E-06      16   0.29540E-05   0.19318E-08 0.68313E+00 
c  TempC        0.24289E+01      41   0.15131E-02   0.55430E-02 0.36217E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -9.9742e-10                             3
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.044394         0.03783      7.2476e-05       9.662e-06
v  Velocity[Y]          -0.033982        0.055339       0.0016642       0.0010327
v  Velocity[Z]        -2.3217e-15      2.9845e-15     -2.9243e-17     -2.5895e-17
v  ǁVelocityǁ          0.00012133        0.058399        0.013789        0.013984
v  Pressure             -0.024167        0.032985     -0.00016379     -1.2215e-18
v  k                   2.0609e-18      0.00010281      6.3913e-07      7.7423e-07
v  epsilon             5.7515e-12       0.0012728      7.7086e-06      9.4507e-06
v  TempC                   26.696          29.986          29.105          29.061
v  Density                 1.1652          1.1784          1.1687          1.1689
v  TurbVisc            1.7391e-26      8.9028e-07      1.6426e-08      1.7904e-08
v  CourantNb            0.0057167          4.8089          1.1375          1.1281
v  FourierNb              0.41911          2.7215         0.88446         0.83334
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  TempC                     26.601              30          29.129          29.127
v  Boundary Density          1.1652          1.1784          1.1686          1.1686
v  Yplus                          0          2.9314        0.058353         0.11712


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42674          6.1927          2.0219          1.9614


 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        -0.222346149E-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 0.24067E-01
   Friction velocity        uet   :  0.34777E-03 0.16436E-01
   Friction velocity        uk    :  0.34773E-03 0.17812E-01
   Dimensionless distance   yplus :  0.44783E-01 0.28251E+01
   Friction thermal sca.    tstar : -0.49064E+01-0.38917E-01
   Rough dim-less th. sca.  tplus :  0.33413E-01 0.21078E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        362
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15938E-05      51   0.58313E-01   0.72676E-05 0.22895E+00 
c  Velocity[X]                                      0.28944E-05 
c  Velocity[Y]                                      0.43732E-05 
c  Velocity[Z]                                      0.35778E-32 
c  Pressure     0.43618E-05     152   0.93657E-03   0.51362E-01 0.17212E-01 
c  k            0.44598E-08      28   0.13190E-04   0.14273E-10 0.79358E+00 
c  epsilon      0.10897E-06      17   0.26629E-05   0.22333E-08 0.83467E+00 
c  TempC        0.24302E+01      40   0.11644E-02   0.52241E-02 0.35136E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -3.5372e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.044952        0.035376      0.00010239      1.1049e-05
v  Velocity[Y]          -0.033516        0.052508       0.0017376       0.0010378
v  Velocity[Z]         -2.343e-15      2.9761e-15     -2.8088e-17     -2.4696e-17
v  ǁVelocityǁ          3.9829e-05         0.05465        0.013708        0.013911
v  Pressure             -0.024449        0.033132     -0.00016305      4.2121e-20
v  k                   1.6213e-18      9.5967e-05      5.4416e-07      6.5848e-07
v  epsilon             5.4546e-12       0.0011428      6.2909e-06      7.7113e-06
v  TempC                   26.785          29.986          29.124          29.081
v  Density                 1.1652           1.178          1.1686          1.1688
v  TurbVisc            2.9719e-27      8.7243e-07      1.4587e-08      1.5762e-08
v  CourantNb            0.0068757          4.6893          1.1211          1.1145
v  FourierNb               0.4193          2.7218         0.88496         0.83395
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  TempC                     26.696              30          29.148          29.146
v  Boundary Density          1.1652           1.178          1.1685          1.1686
v  Yplus                          0          2.8251        0.057712         0.11555


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4279          5.9855           2.006          1.9484


 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        -0.211758237E-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 0.23434E-01
   Friction velocity        uet   :  0.94761E-03 0.16861E-01
   Friction velocity        uk    :  0.94760E-03 0.17584E-01
   Dimensionless distance   yplus :  0.12204E+00 0.27928E+01
   Friction thermal sca.    tstar : -0.60166E+01-0.36710E-01
   Rough dim-less th. sca.  tplus :  0.91054E-01 0.20837E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        364
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15833E-05      51   0.56753E-01   0.67084E-05 0.22087E+00 
c  Velocity[X]                                      0.26663E-05 
c  Velocity[Y]                                      0.40421E-05 
c  Velocity[Z]                                      0.35587E-32 
c  Pressure     0.42014E-05     152   0.94817E-03   0.49274E-01 0.16634E-01 
c  k            0.40530E-08      27   0.10408E-04   0.14241E-10 0.86174E+00 
c  epsilon      0.10170E-06      17   0.15815E-05   0.20394E-08 0.87446E+00 
c  TempC        0.24315E+01      40   0.11772E-02   0.44988E-02 0.32584E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.4085e-09                             3
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.046239        0.035521      0.00012996      1.0921e-05
v  Velocity[Y]          -0.032858        0.048458       0.0018012       0.0010427
v  Velocity[Z]        -2.4198e-15       2.965e-15     -2.7179e-17     -2.3676e-17
v  ǁVelocityǁ          0.00010013        0.055821        0.013678        0.013885
v  Pressure             -0.024735        0.033277     -0.00016242      1.4462e-18
v  k                   1.7133e-18       9.246e-05       4.852e-07      5.8672e-07
v  epsilon             5.0098e-12       0.0011384      5.4627e-06      6.6962e-06
v  TempC                   26.878          29.987          29.143            29.1
v  Density                 1.1652          1.1777          1.1686          1.1687
v  TurbVisc            7.3572e-27      8.5168e-07      1.3441e-08      1.4463e-08
v  CourantNb            0.0086054          4.5539          1.1107          1.1064
v  FourierNb               0.4194          2.7221         0.88514         0.83417
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  TempC                     26.785              30          29.166          29.164
v  Boundary Density          1.1652          1.1777          1.1684          1.1685
v  Yplus                          0          2.7928        0.057028         0.11392


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42963          5.7298          1.9959          1.9406


 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        -0.105879118E-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 0.22815E-01
   Friction velocity        uet   :  0.52450E-03 0.16847E-01
   Friction velocity        uk    :  0.52450E-03 0.17798E-01
   Dimensionless distance   yplus :  0.67558E-01 0.28260E+01
   Friction thermal sca.    tstar : -0.47583E+01-0.34950E-01
   Rough dim-less th. sca.  tplus :  0.50406E-01 0.21085E+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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15776E-05      52   0.53881E-01   0.66048E-05 0.21980E+00 
c  Velocity[X]                                      0.26275E-05 
c  Velocity[Y]                                      0.39773E-05 
c  Velocity[Z]                                      0.36893E-32 
c  Pressure     0.39561E-05     152   0.88528E-03   0.46192E-01 0.14535E-01 
c  k            0.32576E-08      27   0.16079E-04   0.24612E-10 0.14522E+01 
c  epsilon      0.95846E-07      17   0.29345E-05   0.17388E-08 0.90062E+00 
c  TempC        0.24327E+01      40   0.11812E-02   0.40232E-02 0.30794E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.2656e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.045817        0.035475      0.00015847      1.0754e-05
v  Velocity[Y]          -0.032708        0.044005       0.0018577       0.0010485
v  Velocity[Z]        -2.4356e-15      2.9501e-15     -2.6463e-17     -2.2815e-17
v  ǁVelocityǁ          0.00021098        0.056427        0.013685        0.013882
v  Pressure              -0.02494        0.033413      -0.0001618      4.2823e-18
v  k                   1.7701e-18      8.9188e-05      3.3745e-07      4.0597e-07
v  epsilon             4.6304e-12       0.0011935      4.6942e-06      5.7539e-06
v  TempC                   26.948          29.988           29.16          29.119
v  Density                 1.1652          1.1773          1.1685          1.1687
v  TurbVisc            1.5423e-26       8.346e-07      1.2586e-08      1.3498e-08
v  CourantNb            0.0073323          4.3612           1.106          1.1032
v  FourierNb              0.41956          2.7225         0.88414         0.83294
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  TempC                     26.878              30          29.183          29.182
v  Boundary Density          1.1652          1.1773          1.1684          1.1684
v  Yplus                          0           2.826        0.056313         0.11229


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42835          5.4969          1.9901          1.9361


 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        -0.127054942E-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 0.23153E-01
   Friction velocity        uet   :  0.20380E-03 0.16546E-01
   Friction velocity        uk    :  0.20380E-03 0.17905E-01
   Dimensionless distance   yplus :  0.26249E-01 0.28421E+01
   Friction thermal sca.    tstar : -0.65023E+01-0.33671E-01
   Rough dim-less th. sca.  tplus :  0.19584E-01 0.21205E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        375
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15734E-05      52   0.59515E-01   0.60625E-05 0.21069E+00 
c  Velocity[X]                                      0.24814E-05 
c  Velocity[Y]                                      0.35811E-05 
c  Velocity[Z]                                      0.34747E-32 
c  Pressure     0.37687E-05     152   0.83041E-03   0.43811E-01 0.14708E-01 
c  k            0.26708E-08      28   0.30134E-04   0.17538E-10 0.15460E+01 
c  epsilon      0.89151E-07      17   0.49519E-05   0.29199E-08 0.14781E+01 
c  TempC        0.24339E+01      40   0.10504E-02   0.36574E-02 0.29343E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.0023e-09                             3
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.046028         0.03547      0.00018612      1.0394e-05
v  Velocity[Y]          -0.031863        0.045387       0.0019017        0.001054
v  Velocity[Z]        -2.4454e-15      2.9379e-15     -2.5941e-17     -2.2051e-17
v  ǁVelocityǁ          0.00018073        0.059387        0.013721        0.013903
v  Pressure             -0.025141        0.033552     -0.00016113      3.6294e-18
v  k                   1.7933e-18      9.0639e-05      2.2808e-07      2.7231e-07
v  epsilon             2.3062e-12       0.0012193      3.1529e-06      3.8632e-06
v  TempC                   26.982          29.988          29.177          29.137
v  Density                 1.1652           1.177          1.1684          1.1686
v  TurbVisc            9.6523e-27      8.1661e-07      1.0624e-08      1.1162e-08
v  CourantNb            0.0025993          4.1929          1.1067          1.1043
v  FourierNb               0.4196          2.7228         0.88396         0.83271
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  TempC                     26.948              30            29.2          29.199
v  Boundary Density          1.1652           1.177          1.1683          1.1683
v  Yplus                          0          2.8421        0.055491         0.11037


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42362          5.3899          1.9907          1.9371


 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         0.635274710E-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 0.23732E-01
   Friction velocity        uet   :  0.29973E-03 0.16347E-01
   Friction velocity        uk    :  0.29973E-03 0.17666E-01
   Dimensionless distance   yplus :  0.38589E-01 0.28037E+01
   Friction thermal sca.    tstar : -0.30151E+01-0.32886E-01
   Rough dim-less th. sca.  tplus :  0.28792E-01 0.20919E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        379
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15693E-05      52   0.52583E-01   0.54436E-05 0.19959E+00 
c  Velocity[X]                                      0.23085E-05 
c  Velocity[Y]                                      0.31351E-05 
c  Velocity[Z]                                      0.32644E-32 
c  Pressure     0.36896E-05     148   0.81728E-03   0.42698E-01 0.13733E-01 
c  k            0.20668E-08      28   0.32371E-04   0.18239E-10 0.21906E+01 
c  epsilon      0.83511E-07      18   0.39341E-05   0.19503E-08 0.14565E+01 
c  TempC        0.24351E+01      40   0.10687E-02   0.32985E-02 0.27850E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.8362e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.046821        0.035326      0.00021308      9.6596e-06
v  Velocity[Y]          -0.031272        0.047539       0.0019363       0.0010604
v  Velocity[Z]        -2.4671e-15      2.9279e-15     -2.5524e-17      -2.153e-17
v  ǁVelocityǁ          0.00017486        0.060259        0.013759        0.013926
v  Pressure             -0.025362        0.033683     -0.00016038      2.9555e-18
v  k                   1.9024e-18      8.9979e-05      1.3504e-07      1.5861e-07
v  epsilon             3.1554e-12       0.0011894      2.1776e-06      2.6669e-06
v  TempC                   27.008          29.988          29.194          29.155
v  Density                 1.1652          1.1769          1.1684          1.1685
v  TurbVisc            6.0639e-27      7.9775e-07      9.3483e-09      9.6572e-09
v  CourantNb             0.001589           4.052          1.1118           1.109
v  FourierNb              0.41959          2.7231          0.8838          0.8325
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  TempC                     26.982              30          29.216          29.216
v  Boundary Density          1.1652          1.1769          1.1682          1.1683
v  Yplus                          0          2.8037        0.054855         0.10884


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42833          5.3593          1.9956          1.9415


 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         0.211758237E-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 0.23853E-01
   Friction velocity        uet   :  0.31186E-03 0.15015E-01
   Friction velocity        uk    :  0.31186E-03 0.17794E-01
   Dimensionless distance   yplus :  0.40151E-01 0.28235E+01
   Friction thermal sca.    tstar : -0.28024E+01-0.32653E-01
   Rough dim-less th. sca.  tplus :  0.29957E-01 0.21067E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        379
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15656E-05      52   0.52830E-01   0.45780E-05 0.18282E+00 
c  Velocity[X]                                      0.19996E-05 
c  Velocity[Y]                                      0.25784E-05 
c  Velocity[Z]                                      0.29705E-32 
c  Pressure     0.34838E-05     145   0.83322E-03   0.40135E-01 0.14032E-01 
c  k            0.21318E-08      29   0.20135E-04   0.72147E-11 0.13195E+01 
c  epsilon      0.79923E-07      19   0.30551E-05   0.20393E-08 0.17188E+01 
c  TempC        0.24362E+01      40   0.10723E-02   0.30386E-02 0.26715E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -9.9841e-11                             2
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.045973         0.03584      0.00023447       7.169e-06
v  Velocity[Y]           -0.03096        0.048228       0.0019575       0.0010656
v  Velocity[Z]        -2.4725e-15      2.9262e-15     -2.5411e-17     -2.1193e-17
v  ǁVelocityǁ          0.00022135        0.060625        0.013793        0.013949
v  Pressure             -0.025629        0.033813     -0.00015957      3.9173e-18
v  k                   1.5148e-18      9.1883e-05      1.2237e-07      1.4342e-07
v  epsilon             2.4344e-12       0.0012221      1.4115e-06      1.7277e-06
v  TempC                   27.081          29.989          29.209          29.172
v  Density                 1.1652          1.1768          1.1683          1.1684
v  TurbVisc            3.9564e-27      7.1608e-07      8.2104e-09      8.3128e-09
v  CourantNb            0.0037456          4.0681          1.1168          1.1133
v  FourierNb              0.41972          2.7234         0.88363         0.83229
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  TempC                     27.008              30          29.232          29.232
v  Boundary Density          1.1652          1.1768          1.1682          1.1682
v  Yplus                          0          2.8235        0.054096          0.1071


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42974          5.3503          2.0005          1.9456


 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         0.952912066E-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 0.23922E-01
   Friction velocity        uet   :  0.67384E-03 0.15780E-01
   Friction velocity        uk    :  0.67384E-03 0.17816E-01
   Dimensionless distance   yplus :  0.99214E-01 0.28290E+01
   Friction thermal sca.    tstar : -0.56987E+01-0.31936E-01
   Rough dim-less th. sca.  tplus :  0.74025E-01 0.21108E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        379
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15625E-05      52   0.51215E-01   0.38718E-05 0.16816E+00 
c  Velocity[X]                                      0.17405E-05 
c  Velocity[Y]                                      0.21313E-05 
c  Velocity[Z]                                      0.29013E-32 
c  Pressure     0.31677E-05     143   0.79144E-03   0.36344E-01 0.12484E-01 
c  k            0.21858E-08      29   0.89437E-05   0.74684E-11 0.13153E+01 
c  epsilon      0.78195E-07      19   0.12694E-05   0.11608E-08 0.12654E+01 
c  TempC        0.24373E+01      41   0.10406E-02   0.28296E-02 0.25766E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.6274e-09                             3
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.044933        0.035828      0.00025165      4.9146e-06
v  Velocity[Y]          -0.030581        0.048907        0.001969       0.0010714
v  Velocity[Z]        -2.4688e-15      2.9363e-15     -2.5472e-17     -2.0961e-17
v  ǁVelocityǁ          0.00020289        0.060231        0.013806        0.013955
v  Pressure              -0.02589        0.033931     -0.00015862      3.0187e-19
v  k                   1.1037e-18      9.2382e-05      1.2246e-07      1.4374e-07
v  epsilon             2.3365e-12       0.0012263      1.3262e-06      1.6234e-06
v  TempC                   27.137          29.989          29.225          29.188
v  Density                 1.1652          1.1765          1.1682          1.1684
v  TurbVisc            2.5627e-27        7.32e-07      8.0284e-09      8.1256e-09
v  CourantNb            0.0042943          4.1053          1.1208          1.1169
v  FourierNb              0.41972          2.7237         0.88334         0.83192
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  TempC                     27.081              30          29.247          29.247
v  Boundary Density          1.1652          1.1765          1.1681          1.1682
v  Yplus                          0           2.829        0.053396         0.10553


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43081          5.3725          2.0041          1.9488


 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 0.23890E-01
   Friction velocity        uet   :  0.42434E-03 0.16601E-01
   Friction velocity        uk    :  0.42434E-03 0.17840E-01
   Dimensionless distance   yplus :  0.64615E-01 0.28302E+01
   Friction thermal sca.    tstar : -0.32031E+01-0.31101E-01
   Rough dim-less th. sca.  tplus :  0.48210E-01 0.21116E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        378
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15569E-05      52   0.55780E-01   0.33936E-05 0.15772E+00 
c  Velocity[X]                                      0.15314E-05 
c  Velocity[Y]                                      0.18622E-05 
c  Velocity[Z]                                      0.28137E-32 
c  Pressure     0.29173E-05     142   0.72745E-03   0.33340E-01 0.11284E-01 
c  k            0.23140E-08      29   0.62148E-05   0.77532E-11 0.13243E+01 
c  epsilon      0.77403E-07      20   0.91396E-06   0.11693E-08 0.12407E+01 
c  TempC        0.24383E+01      41   0.89442E-03   0.26364E-02 0.24857E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.2731e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.044129        0.035339       0.0002643      2.5717e-06
v  Velocity[Y]          -0.030286        0.049009       0.0019714       0.0010753
v  Velocity[Z]         -2.458e-15      2.9588e-15     -2.5612e-17     -2.0818e-17
v  ǁVelocityǁ          9.8535e-05        0.060155        0.013793        0.013935
v  Pressure             -0.026136        0.034039     -0.00015764     -3.5101e-20
v  k                    7.989e-19      9.2885e-05      1.2292e-07      1.4446e-07
v  epsilon             6.3881e-13        0.001234      1.3474e-06      1.6495e-06
v  TempC                   27.232           29.99           29.24          29.204
v  Density                 1.1652          1.1763          1.1682          1.1683
v  TurbVisc            1.5891e-27      7.4068e-07       7.932e-09      8.0336e-09
v  CourantNb            0.0078124          4.1107          1.1228          1.1188
v  FourierNb              0.41975           2.724         0.88354         0.83216
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  TempC                     27.137              30          29.262          29.262
v  Boundary Density          1.1652          1.1763          1.1681          1.1681
v  Yplus                          0          2.8302        0.052791         0.10422


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42884          5.3781          2.0063           1.951


 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         0.635274710E-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 0.23912E-01
   Friction velocity        uet   :  0.19920E-03 0.14129E-01
   Friction velocity        uk    :  0.19920E-03 0.17843E-01
   Dimensionless distance   yplus :  0.31542E-01 0.28306E+01
   Friction thermal sca.    tstar : -0.31381E+01-0.30816E-01
   Rough dim-less th. sca.  tplus :  0.23534E-01 0.21119E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        377
   Total number of wall faces                   :        384
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15471E-05      52   0.44943E-01   0.29635E-05 0.14806E+00 
c  Velocity[X]                                      0.12945E-05 
c  Velocity[Y]                                      0.16690E-05 
c  Velocity[Z]                                      0.25381E-32 
c  Pressure     0.28790E-05     142   0.64926E-03   0.32800E-01 0.99850E-02 
c  k            0.25076E-08      34   0.12184E-04   0.10639E-10 0.12837E+01 
c  epsilon      0.77635E-07      24   0.22407E-05   0.20132E-08 0.14312E+01 
c  TempC        0.24393E+01      41   0.75236E-03   0.23465E-02 0.23439E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -8.4681e-10                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.042983        0.034429      0.00027129     -4.5482e-07
v  Velocity[Y]          -0.029838        0.050041        0.001968       0.0010791
v  Velocity[Z]        -2.4449e-15      2.9929e-15     -2.5832e-17     -2.0709e-17
v  ǁVelocityǁ          1.2394e-05        0.059754        0.013744        0.013877
v  Pressure             -0.026357        0.034135     -0.00015659     -3.9383e-18
v  k                   5.4738e-19      9.3364e-05       1.652e-07       1.964e-07
v  epsilon             3.3441e-14       0.0012353      1.6887e-06       2.068e-06
v  TempC                   27.297           29.99          29.255          29.219
v  Density                 1.1652          1.1759          1.1681          1.1683
v  TurbVisc            9.7598e-28      7.4698e-07      7.8678e-09       7.974e-09
v  CourantNb              0.00318          4.0366          1.1214          1.1174
v  FourierNb              0.41975          2.7243         0.88358         0.83221
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  TempC                     27.232              30          29.276          29.276
v  Boundary Density          1.1652          1.1759           1.168           1.168
v  Yplus                          0          2.8306         0.05242         0.10342


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42421          5.3932           2.005          1.9496


 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         0.635274710E-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 0.23866E-01
   Friction velocity        uet   :  0.45997E-03 0.15679E-01
   Friction velocity        uk    :  0.45997E-03 0.17732E-01
   Dimensionless distance   yplus :  0.72832E-01 0.28144E+01
   Friction thermal sca.    tstar : -0.52347E+01-0.30363E-01
   Rough dim-less th. sca.  tplus :  0.54341E-01 0.20999E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        377
   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      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15367E-05      52   0.40365E-01   0.26761E-05 0.14163E+00 
c  Velocity[X]                                      0.11554E-05 
c  Velocity[Y]                                      0.15206E-05 
c  Velocity[Z]                                      0.25441E-32 
c  Pressure     0.24559E-05     144   0.54748E-03   0.27895E-01 0.89768E-02 
c  k            0.26115E-08      29   0.75738E-05   0.69589E-11 0.10196E+01 
c  epsilon      0.78180E-07      19   0.14160E-05   0.96040E-09 0.96073E+00 
c  TempC        0.24403E+01      41   0.78045E-03   0.20602E-02 0.21951E-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]          -0.042046        0.033701      0.00027199     -2.7636e-06
v  Velocity[Y]          -0.029236        0.051386       0.0019602        0.001082
v  Velocity[Z]        -2.4322e-15      3.0383e-15     -2.6175e-17     -2.0591e-17
v  ǁVelocityǁ          0.00023486        0.060054        0.013669        0.013792
v  Pressure             -0.026578         0.03422     -0.00015539     -8.0732e-19
v  k                   3.5911e-19      9.1623e-05      1.7014e-07      2.0256e-07
v  epsilon             1.1237e-12       0.0011954      1.8376e-06       2.251e-06
v  TempC                   27.325          29.991          29.269          29.234
v  Density                 1.1652          1.1757          1.1681          1.1682
v  TurbVisc            5.5022e-28      7.5833e-07      8.2292e-09      8.4323e-09
v  CourantNb            0.0022669          4.1201          1.1165          1.1122
v  FourierNb              0.41983          2.7246         0.88381         0.83247
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  TempC                     27.297              30           29.29           29.29
v  Boundary Density          1.1652          1.1757          1.1679           1.168
v  Yplus                          0          2.8144        0.052167         0.10288


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4233          5.4709          2.0003          1.9447


 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        -0.635274710E-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 0.23886E-01
   Friction velocity        uet   :  0.53300E-03 0.16355E-01
   Friction velocity        uk    :  0.53300E-03 0.17873E-01
   Dimensionless distance   yplus :  0.68639E-01 0.28366E+01
   Friction thermal sca.    tstar : -0.38812E+01-0.29021E-01
   Rough dim-less th. sca.  tplus :  0.51212E-01 0.21164E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        378
   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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15240E-05      53   0.42538E-01   0.24597E-05 0.13704E+00 
c  Velocity[X]                                      0.10578E-05 
c  Velocity[Y]                                      0.14019E-05 
c  Velocity[Z]                                      0.24951E-32 
c  Pressure     0.23490E-05     143   0.48171E-03   0.26606E-01 0.82781E-02 
c  k            0.25453E-08      32   0.19275E-04   0.75561E-11 0.10361E+01 
c  epsilon      0.78112E-07      23   0.34716E-05   0.11043E-08 0.10002E+01 
c  TempC        0.24412E+01      41   0.73263E-03   0.18138E-02 0.20587E-02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.0736e-09                             1
a  TempC  


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.040368        0.032237      0.00026627     -4.5182e-06
v  Velocity[Y]           -0.02883        0.051935       0.0019516       0.0010859
v  Velocity[Z]        -2.4205e-15      3.0936e-15     -2.6507e-17     -2.0546e-17
v  ǁVelocityǁ          7.0772e-05        0.059516        0.013574         0.01368
v  Pressure              -0.02678        0.034296     -0.00015408       8.003e-19
v  k                   2.4182e-19      9.3963e-05      1.7572e-07      2.0946e-07
v  epsilon             2.7317e-12       0.0011748      1.9253e-06      2.3584e-06
v  TempC                   27.373          29.991          29.283          29.249
v  Density                 1.1652          1.1756           1.168          1.1681
v  TurbVisc            2.8894e-28      7.6566e-07      8.2458e-09       8.466e-09
v  CourantNb            0.0065789          4.4347          1.1099           1.105
v  FourierNb              0.41988          2.7248         0.88384          0.8325
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  TempC                     27.325              30          29.303          29.304
v  Boundary Density          1.1652          1.1756          1.1679          1.1679
v  Yplus                          0          2.8366        0.051887         0.10233


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42945          5.7287          1.9938          1.9375



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



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


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





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




                      END OF CALCULATION                     
                      ==================                     


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

 Destroying structures and ending computation

