command: 
 /home/ctrinca/Code_Saturne/4.0.0/code_saturne-4.0.0/arch/Linux_x86_64/libexec/code_saturne/cs_solver --param fluid.xml --mpi --app-name fluid

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

                                  (R)
                      Code_Saturne

                      Version 4.0.0


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

  revision 4.0.0
  build Wed 24 Jun 2015 11:20:03 BST
  MPI version 3.0 (Open MPI 1.8.3)


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

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

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


Local case configuration:

  Date:                Wed 24 Jun 2015 11:26:56 BST
  System:              Linux 3.13.0-32-generic
  Machine:             fermi
  Processor:           model name	: Intel(R) Core(TM) i7-2600 CPU @ 3.40GHz
  Memory:              5951 MB
  User:                ctrinca (Cosimo Trinca)
  Directory:           /home/ctrinca/Simulations/MeshTests/annular-conjugate/coupled-study2/RESU_COUPLING/20150624-1126/fluid
  MPI ranks:           1 (appnum attribute: 1)
  MPI_COMM_WORLD size: 2
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)

  External libraries for partitioning:
    ParMETIS 4.0.3
    PT-SCOTCH 6.0.3

 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   =              5 (Nb variables                )
       NSCAL  =              1 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              1 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )


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


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

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

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.13257E+01 (Reference density           )
       VISCL0 =    0.19000E-04 (Ref. molecular dyn. visc.   )
       CP0    =    0.94200E+03 (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 =              1 (0: no thermal model         )
                               (1: temperature              )
                               (2: enthalpy                 )
                               (3: total energy             )
       ITPSCL =              1 (0: none                     )
                               (1: temperature in Kelvin    )
                               (2: temperature in Celsius   )
       ISCALT =              1 (Thermal scalar number       )


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

 --- Continuous phase:

   - Commons
       ITURB  =              0 (Turbulence model            )
       IDEUCH =              0 (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)     )

 --- 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))


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


 ** 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
 TempK                 1  0.1000E+01
----------------------------

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

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

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


 ** 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
 TempK                 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
 TempK               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
 TempK                 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
 TempK             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
-------------------------------------------------------------
 TempK                 1      1      0  0.2435E+00  0.1000E+01
---------------------------------------------------------------------

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

-------------------------------------------------------
 Variable         Number ICLVFL      SCAMIN      SCAMAX
-------------------------------------------------------
 TempK                 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 =          50000 (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
TempK
CourantNb
FourierNb
total_pressure
         --           --

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              4 (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 TempK                         -1
         8 LamVisc                       -1
         9 CourantNb                     -1
        10 FourierNb                     -1
        11 total_pressure                -1
         --           --                --

 --- Log files
       NTLIST =            100 (Output frequency     )

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

         2 Velocity                       0
         5 Pressure                       0
         6 TempK                          0
         9 CourantNb                   -999
        10 FourierNb                   -999
        11 total_pressure              -999
         --           --                --

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


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


 ** SYRTHES COUPLING
    ----------------

       NBCCOU =              1 (Number of couplings         )

       with                 1 surface coupling(s)
       with                 0 volume coupling(s)


  -- Coupled scalars
-------------------------------
 Scalar           Number ICPSYR
-------------------------------
 TempK                 1      1
-----------------------

       ICPSYR = 0 or 1         (1: scalar coupled to SYRTHES)


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


 ** 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)


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


Applications accessible through MPI:
------------------------------------

  1; type:      "SYRTHES 4"
     case name: "solid"
     lead rank: 0; n_ranks: 1
     (group synchronized)

  2; type:      "Code_Saturne 4.0.0" (this instance)
     case name: "fluid"
     lead rank: 1; n_ranks: 1
     (group synchronized)

 SYRTHES coupling:
   coupling id:              0
   version:                  "SYRTHES 4"
   local name:               "solid"
   distant application name: "solid"
   MPI application id:       0
   MPI root rank:            0
   number of MPI ranks:      1

 SYRTHES coupling 0: initializing MPI communication ... [ok]
  Local ranks = [1..1], distant ranks = [0..0].


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

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


 Reading file:        mesh_input
 Finished reading:    mesh_input

 Number of cells:                                      100800

 ----------------------------------------------------------
 Number of cells + halo cells:                         100800


 ----------------------------------------------------------
 Number of interior faces:                             290948

 ----------------------------------------------------------
 Number of boundary faces:                             22904

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

 Histogram of the number of interior faces per cell:

    minimum value =                  4
    maximum value =                  6

      1 : [          4 ;          5 [ =        112
      2 : [          5 ;          6 ] =     100688

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

 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 :          72000
 Matrix profile/lines for volume mesh :      16971

 Mesh coordinates:               minimum    and maximum
                       X : -5.0000000e-02  5.0000000e-02
                       Y : -5.0000000e-02  5.0000000e-02
                       Z :  0.0000000e+00  3.5000000e+00
 Mesh
     Number of cells:          100800
     Number of interior faces: 290948
     Number of boundary faces: 22904
     Number of vertices:       112280

 Groups:
    "BLOCK6HEXAHEDRALBOTTOMBOUNDARY"
       boundary faces:          252
    "BLOCK6HEXAHEDRALINNERBOUNDARY"
       boundary faces:        11200
    "BLOCK6HEXAHEDRALOUTERBOUNDARY"
       boundary faces:        11200
    "BLOCK6HEXAHEDRALTOPBOUNDARY"
       boundary faces:          252

 --- Information on the volumes
       Minimum control volume      =  5.5631862e-08
       Maximum control volume      =  3.9839672e-07
       Total volume for the domain =  2.6986226e-02

  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 (0.153 s)
                                                             
       ALMAX  =    0.30031E+00 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.


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


 ** 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
  TempK             0.3000E+03  0.3000E+03
 ---------------------------------

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



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1326E+01  0.1326E+01
  molecular_viscos  0.1900E-04  0.1900E-04
 -----------------------------------------

 --- Diffusivity:
 -----------------------------------------------
 Scalar           Number  Min. value  Max. value
 -----------------------------------------------
 TempK                 1  0.2435E+00  0.2435E+00
 -----------------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         252
Smooth wall               5       22400
Rough wall                6           0
Symmetry                  4           0
Free outlet               3         252
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =   -0.38210E-02   0.60811E-02   0.35000E+01



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         252         0.000000000E+00
Smooth wall               5       22400         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         252         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
---------------------------------------------------------------


Application "solid" (SYRTHES 4) requested calculation stop.


 Write final restart files
   checkpoint at iteration          1, Physical time    0.50000E+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


 Time for restart files:    0.15423E-01



 TIME FOR THE TIME STEP                1:        0.27584E+01

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.71748E-04
      -----------------------                                



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




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


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

 Destroying structures and ending computation

Structures associated with SYRTHES 4 coupling freed.


Calculation time summary:

  User CPU time:              3.317 s
  System CPU time:            0.113 s

  Elapsed time:               3.291 s
  CPU / elapsed time          1.042

Memory use summary:

  Total memory used:                             557.098 MiB
  Theoretical instrumented dynamic memory:       122.579 MiB
