command: 
 .\cs_solver.exe --param ale2.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 4.0.8


  Copyright (C) 1998-2016 EDF S.A., France

  revision 4.0.8
  build 07/20/17 20:08:26
  MPI version 2.0 (MS-MPI)


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

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

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


Local case configuration:

  Date:                10/27/18 19:35:14
  Processor:           
  Directory:           D:\1-Wenjian\Gongzuomulu\CodeSaturne gongzuomulu\ALE2\2\RESU\20181027-1935
  MPI ranks:           2 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    SCOTCH 6.0.0

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              9 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              7 (Nb cell properties          )


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


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

       GX     =    0.00000E+00 (Gravity x component         )
       GY     =    0.00000E+00 (Gravity y component         )
       GZ     =   -0.98100E+01 (Gravity z component         )

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.10000E+04 (Reference density           )
       VISCL0 =    0.10000E-11 (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 =              0 (Density constant(0) or not(1)
       IVIVAR =              0 (Molec. visc cst.(0) or not(1)

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

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


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


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

 --- Continuous phase:

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

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

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

 --- Constants

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

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


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.25000E-02 (Minimum time step           )
       DTMAX  =    0.25000E+02 (Maximum time step           )
       DTREF  =    0.25000E-01 (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
 Mesh Velocity         0  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
 Mesh Velocity         0      1      1      1      0 0.00E+00 0.10E+01
-------------------------------------------------------------

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


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


 ** STOKES
    ------
       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
 Mesh Velocity       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
 Mesh Velocity         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
 Mesh Velocity     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    )


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


 ** 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 =           2000 (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
Mesh Velocity
TurbVisc
CourantNb
FourierNb
total_pressure
Mesh displacement
mesh_vi1
         --           --

 --- 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 Mesh Velocity[X]              -1
         9 Mesh Velocity[Y]              -1
        10 Mesh Velocity[Z]              -1
        12 LamVisc                       -1
        13 TurbVisc                      -1
        14 CourantNb                     -1
        15 FourierNb                     -1
        16 total_pressure                -1
        17 Mesh displacemen              -1
        20 mesh_vi1                      -1
         --           --                --

 --- Log files
       NTLIST =             10 (Output frequency     )

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

         2 Velocity                       0
         5 Pressure                       0
         6 k                              0
         7 epsilon                        0
         8 Mesh Velocity                  0
        13 TurbVisc                    -999
        14 CourantNb                   -999
        15 FourierNb                   -999
        16 total_pressure              -999
        17 Mesh displacemen            -999
        20 mesh_vi1                    -999
         --           --                --

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


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


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

       IALE   =              1 (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: transient coordinates
      output: every 10 time steps and at calculation end


 Reading file:        mesh_input
 Finished reading:    mesh_input
 No "partition_input\domain_number_2" file available;

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

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [       4740 ;       4741 ] =          2

 Partitioning finished (0.058 s)


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

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

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

 Histogram of the number of cells per rank:

    minimum value =               4740
    maximum value =               4741

      1 : [       4740 ;       4741 ] =          2

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

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

    minimum value =               4768
    maximum value =               4769

      1 : [       4768 ;       4769 ] =          2

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

 Histogram of the number of ghost cells per rank:

    minimum value =                 28
    maximum value =                 28

      1 : [         28 ;         28 ] =          2

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

 Histogram of the number of interior faces per rank:

    minimum value =               9233
    maximum value =               9240

      1 : [       9233 ;       9234 [ =          1
      2 : [       9234 ;       9235 [ =          0
      3 : [       9235 ;       9237 [ =          0
      4 : [       9237 ;       9238 [ =          0
      5 : [       9238 ;       9240 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =               9989
    maximum value =              10009

      1 : [       9989 ;       9993 [ =          1
      2 : [       9993 ;       9997 [ =          0
      3 : [       9997 ;      10001 [ =          0
      4 : [      10001 ;      10005 [ =          0
      5 : [      10005 ;      10009 ] =          1

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =          4
      2 : [          3 ;          4 ] =       9477

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  1
    maximum value =                  1

      1 : [          1 ;          1 ] =          2

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

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

 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =                181
    maximum value =               4759

      1 : [        181 ;       1096 [ =          1
      2 : [       1096 ;       2012 [ =          0
      3 : [       2012 ;       2927 [ =          0
      4 : [       2927 ;       3843 [ =          0
      5 : [       3843 ;       4759 ] =          1

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =                 19
    maximum value =                 46

      1 : [         19 ;         24 [ =          1
      2 : [         24 ;         29 [ =          0
      3 : [         29 ;         35 [ =          0
      4 : [         35 ;         40 [ =          0
      5 : [         40 ;         46 ] =          1

 Mesh coordinates:               minimum    and maximum
                       X : -2.5000000e+002 2.5000000e+002
                       Y : -5.0000001e-002 5.0000001e-002
                       Z : -5.0000000e+000 5.0000000e+000
 Mesh
     Number of cells:          9481
     Number of interior faces: 18444
     Number of boundary faces: 19998
     Number of vertices:       20000

 Groups:
    "BEHIND"
       boundary faces:         9481
    "DOWN"
       boundary faces:          499
    "FRONT"
       boundary faces:         9481
    "INLET"
       boundary faces:           19
    "OUTLET"
       boundary faces:           19
    "PART_1"
       boundary faces:         1036
    "TOP"
       boundary faces:          499

 --- Information on the volumes
       Minimum control volume      = 5.2737053e-002
       Maximum control volume      = 5.2737054e-002
       Total volume for the domain = 5.0000001e+002

  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 (0.155 s)
                                                             
       ALMAX  =    0.79206E+01 (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           0.1670E-06  0.1670E-06
  Mesh Velocity     0.0000E+00  0.0000E+00
  Mesh Velocity     0.0000E+00  0.0000E+00
  Mesh Velocity     0.0000E+00  0.0000E+00
 ---------------------------------

                dt  0.2500E-01  0.2500E-01
 ---------------------------------



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

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


ALL PHASES: COUPLING MODE FOR STRUCTURES NOT ACTIVATED 
              NBSTRU =          0


ALL PHASES: CODE_ASTER COUPLING MODE NOT ACTIVATED     
              NBASTE =          0

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



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



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


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




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


 INSTANT    0.000000000E+00   ALE INITIALIZATION 
 ============================================================= 


Warning : Formula is null for ale. Use constant value
 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1000E+04  0.1000E+04
  molecular_viscos  0.1000E-11  0.1000E-11
  turbulent_viscos  0.1940E+03  0.1940E+03
 -----------------------------------------

 --- Mesh viscosity (ALE method)
 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  mesh_viscosity_1  0.1000E+01  0.1000E+01
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          19
Smooth wall               5         499
Rough wall                6           0
Symmetry                  4       18962
Free outlet               3          19
Free inlet               13           0
Convective inlet         15           0
Free surface             14         499
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.25000E+03   0.00000E+00  -0.43672E-15



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          19         0.000000000E+00
Smooth wall               5         499         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       18962         0.000000000E+00
Free outlet               3          19         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14         499         0.000000000E+00
Undefined                 1           0         0.000000000E+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    :  0.13416E-01 0.13416E-01
   Dimensionless distance   yplus :  0.10000E+13 0.35306E+13
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :        499
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
c  Velocity[X]                                      0.00000E+00 
c  Velocity[Y]                                      0.00000E+00 
c  Velocity[Z]                                      0.00000E+00 
c  Pressure     0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
c  k            0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
c  epsilon      0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
c  Mesh Velocit 0.00000E+00       0   0.00000E+00   0.00000E+00 0.00000E+00 
c  Mesh Velocit                                     0.00000E+00 
c  Mesh Velocit                                     0.00000E+00 
c  Mesh Velocit                                     0.00000E+00 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Velocity[X]                    0               0               0               0
v  Velocity[Y]                    0               0               0               0
v  Velocity[Z]                    0               0               0               0
v  ǁVelocityǁ                   0               0               0               0
v  Pressure                       0               0               0               0
v  k                         0.0006          0.0006          0.0006          0.0006
v  epsilon                1.67e-007       1.67e-007       1.67e-007       1.67e-007
v  Mesh Velocity[X]               0               0               0               0
v  Mesh Velocity[Y]               0               0               0               0
v  Mesh Velocity[Z]               0               0               0               0
v  ǁMesh Velocityǁ               0               0               0               0
v  TurbVisc                  194.01          194.01          194.01          194.01
v  CourantNb                      0               0               0               0
v  FourierNb               0.022341        0.044681        0.042819        0.042819
v  total_pressure             54857     1.4779e+005     1.0133e+005     1.0133e+005
v  mesh_vi1                       1               1               1               1

  ** Computed fields on vertices
     ---------------------------

   field                        minimum         maximum        set mean
-  --------------------  --------------  --------------  --------------
v  Mesh displacement[X]               0               0               0
v  Mesh displacement[Y]               0               0               0
v  Mesh displacement[Z]               0               0               0
v  ǁMesh displacementǁ               0               0               0


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.022341        0.044681        0.042819        0.042819


 TIME FOR ALE INITIALIZATION:           0.57041E-01

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


 INSTANT    0.250000000E-01   TIME STEP NUMBER               1
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          19         0.000000000E+00
Smooth wall               5         499         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       18962         0.000000000E+00
Free outlet               3          19         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14         499         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


 TIME FOR THE TIME STEP                1:        0.18013E+00

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


 INSTANT    0.500000000E-01   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          19        -0.100000000E+04
Smooth wall               5         499        -0.493038066E-31
Rough wall                6           0         0.000000000E+00
Symmetry                  4       18962         0.957924090E-22
Free outlet               3          19         0.340979195E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14         499         0.861490248E-14
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


 TIME FOR THE TIME STEP                2:        0.17713E+00

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


 INSTANT    0.750000000E-01   TIME STEP NUMBER               3
 ============================================================= 



 TIME FOR THE TIME STEP                3:        0.19214E+00

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


 INSTANT    0.100000000E+00   TIME STEP NUMBER               4
 ============================================================= 



 TIME FOR THE TIME STEP                4:        0.20214E+00

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


 INSTANT    0.125000000E+00   TIME STEP NUMBER               5
 ============================================================= 



 TIME FOR THE TIME STEP                5:        0.18513E+00

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


 INSTANT    0.150000000E+00   TIME STEP NUMBER               6
 ============================================================= 



 TIME FOR THE TIME STEP                6:        0.21015E+00

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


 INSTANT    0.175000000E+00   TIME STEP NUMBER               7
 ============================================================= 



 TIME FOR THE TIME STEP                7:        0.19514E+00

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


 INSTANT    0.200000000E+00   TIME STEP NUMBER               8
 ============================================================= 



 TIME FOR THE TIME STEP                8:        0.19213E+00

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


 INSTANT    0.225000000E+00   TIME STEP NUMBER               9
 ============================================================= 



 TIME FOR THE TIME STEP                9:        0.20114E+00

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


 INSTANT    0.250000000E+00   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          19        -0.100000000E+04
Smooth wall               5         499         0.125346088E-27
Rough wall                6           0         0.000000000E+00
Symmetry                  4       18962         0.106139764E-20
Free outlet               3          19         0.191332796E+04
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14         499        -0.566623173E-13
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.36154E-13 0.13424E+01
   Friction velocity        uet   :  0.51341E-15 0.19062E-01
   Friction velocity        uk    :  0.13410E-01 0.13795E-01
   Dimensionless distance   yplus :  0.10000E+13 0.36346E+13
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :        499
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49191E+05       9   0.59051E-03   0.16603E-01 0.34752E+01 
c  Velocity[X]                                      0.81982E-02 
c  Velocity[Y]                                      0.30066E-27 
c  Velocity[Z]                                      0.84049E-02 
c  Pressure     0.10852E+02     211   0.84668E-04   0.16350E+00 0.30405E-01 
c  k            0.12339E+03       7   0.10287E-06   0.63154E-11 0.26467E-01 
c  epsilon      0.22480E+00       6   0.43852E-06   0.16815E-12 0.23989E+01 
c  Mesh Velocit 0.25752E+01      95   0.87071E-03   0.23375E-02 0.27361E+01 
c  Mesh Velocit                                     0.22143E-35 
c  Mesh Velocit                                     0.24536E-38 
c  Mesh Velocit                                     0.23375E-02 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                    minimum         maximum        set mean    spatial mean
-  ----------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -4.7488e-012          2.3964        0.032901        0.032813
v  Velocity[Y]         -1.8876e-013     2.6889e-013     6.5346e-017     6.2289e-017
v  Velocity[Z]              -4.3085          1.7039      -0.0087257       -0.009162
v  ǁVelocityǁ         4.9772e-014          4.8557        0.049548        0.049699
v  Pressure                 -7244.2           50164           48540           48546
v  k                     0.00059866      0.00072406      0.00060051      0.00060051
v  epsilon              1.6644e-007     1.8526e-005     3.8703e-007     3.8693e-007
v  Mesh Velocity[X]     -1.245e-028     4.7269e-017     6.9568e-020     7.2804e-020
v  Mesh Velocity[Y]    -8.0212e-018     6.3838e-018     -1.105e-021     1.1806e-021
v  Mesh Velocity[Z]         -2.6537          1.2951       -0.006196      -0.0067522
v  ǁMesh Velocityǁ     9.2354e-018          2.6537        0.020045        0.020285
v  TurbVisc                  2.2886          208.63          178.52          178.52
v  CourantNb                      0           0.217       0.0012366       0.0012344
v  FourierNb             0.00090091          2.0036         0.13647         0.13643
v  total_pressure             97607     1.9793e+005     1.4987e+005     1.4987e+005
v  mesh_vi1                       1               1               1               1

  ** Computed fields on vertices
     ---------------------------

   field                        minimum         maximum        set mean
-  --------------------  --------------  --------------  --------------
v  Mesh displacement[X]    -1.2018e-032     9.0431e-019     1.5478e-021
v  Mesh displacement[Y]    -5.0664e-010     5.0664e-010    -4.1273e-023
v  Mesh displacement[Z]        -0.40486          0.3579     -0.00021782
v  ǁMesh displacementǁ               0         0.40486       0.0031525


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0057335          2.0204          0.1377         0.13766


 TIME FOR THE TIME STEP               10:        0.30622E+00

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


 INSTANT    0.275000000E+00   TIME STEP NUMBER              11
 ============================================================= 



 TIME FOR THE TIME STEP               11:        0.20715E+00

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


 INSTANT    0.300000000E+00   TIME STEP NUMBER              12
 ============================================================= 



 TIME FOR THE TIME STEP               12:        0.20715E+00

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


 INSTANT    0.325000000E+00   TIME STEP NUMBER              13
 ============================================================= 



 TIME FOR THE TIME STEP               13:        0.20815E+00

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


 INSTANT    0.350000000E+00   TIME STEP NUMBER              14
 ============================================================= 



 TIME FOR THE TIME STEP               14:        0.21415E+00

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


 INSTANT    0.375000000E+00   TIME STEP NUMBER              15
 ============================================================= 



 TIME FOR THE TIME STEP               15:        0.24918E+00

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


 INSTANT    0.400000000E+00   TIME STEP NUMBER              16
 ============================================================= 



 TIME FOR THE TIME STEP               16:        0.26519E+00

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


 INSTANT    0.425000000E+00   TIME STEP NUMBER              17
 ============================================================= 


 Warning:
 --------
   _iterative_vector_gradient; variable: velocity; sweeps: 100
                               normed residual: 9.6672e+026; norm: 8.9059e+000
 Warning:
 --------
   _iterative_vector_gradient; variable: velocity; sweeps: 100
                               normed residual: 9.6672e+026; norm: 8.9059e+000
 Warning:
 --------
   _iterative_vector_gradient; variable: velocity; sweeps: 100
                               normed residual: 1.4543e+027; norm: 7.3765e+026
 Warning:
 --------
   _iterative_vector_gradient; variable: Var. 0; sweeps: 100
                               normed residual: 1.4543e+027; norm: 7.3765e+029
 Warning:
 --------
   _iterative_vector_gradient; variable: velocity; sweeps: 100
                               normed residual: 9.6672e+026; norm: 8.9059e+000
 Warning:
 --------
   _iterative_scalar_gradient; variable: k; sweeps: 100
                               normed residual: 3.3667e+027; norm: 6.2844e-004
 Warning:
 --------
   _iterative_scalar_gradient; variable: k; sweeps: 100
                               normed residual: 1.5458e+026; norm: 1.0647e-001
 Warning:
 --------
   _iterative_scalar_gradient; variable: epsilon; sweeps: 100
                               normed residual: 5.8570e+025; norm: 3.7961e-003
 Warning:
 --------
   _iterative_scalar_gradient; variable: epsilon; sweeps: 100
                               normed residual: 4.3117e+026; norm: 3.9908e-003
 --- Information on the volumes
       Minimum control volume      = -1.2742195e+127
       Maximum control volume      = 1.4503143e+127
       Total volume for the domain = 2.4742758e+125

Abort due to the detection of a negative control volume.


 Write final restart files
   checkpoint at iteration         17, Physical time    0.42500E+00


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
   End writing the ALE data                             
 End writing


 Time for restart files:    0.17212E+00



 TIME FOR THE TIME STEP               17:        0.22316E+01

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.10000E-02
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  CPU time:                   6.022 s
  Total CPU time:            12.044 s

  Elapsed time:               6.022 s
  CPU / elapsed time          1.000

Memory use summary:

  Theoretical instrumented dynamic memory:        29.120 MiB
                             local minimum:       14.209 MiB  (rank 1)
                             local maximum:       14.911 MiB  (rank 0)
