As a training, I would like to model a rejection of a chimney near a mountain (The puy de dome, France).
For now, I only use gui interface.
I made a simulation imposing a velocity of my chimney (normal to the inlet) and of my atmosphere (dy = 1.0, dx=dz=0.0) and it worked.
But now I would like to try to use an extern meteo file and I have a problem when I use for the atmosphere (basically a cylinder with an altitude of 2000 meters) "Meteorological profile from data" and "automatic inlet/outlet nature..." and for the chimney the velocity normal to the inlet.
This is the listing file :
Code: Select all
***************************************************************
(R)
Code_Saturne
Version 5.0.9
Copyright (C) 1998-2018 EDF S.A., France
revision 5.0.9-9b87d1bcb
build ven. 16 nov. 2018 15:19:47 CET
MPI version 3.1 (Open MPI 2.1.1)
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: ven. 14 déc. 2018 10:07:15 CET
System: Linux 4.15.0-42-generic (Ubuntu 18.04.1 LTS)
Machine: noam-VirtualBox
Processor: model name : Intel(R) Core(TM) i5-8400 CPU @ 2.80GHz
Memory: 3944 MB
User: noam (Noam)
Directory: /home/noam/Documents/Tutos_code_saturne/PdD/case1/RESU/20181214-1007
MPI ranks: 4 (appnum attribute: 0)
OpenMP threads: 1
Processors/node: 5
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:
ParMETIS 4.0.3
PT-SCOTCH 6.0.4
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 = 8 (Nb variables )
NSCAL = 2 (Nb scalars )
NSCAUS = 1 (Nb user scalars )
NSCAPP = 1 (Nb specific physics scalars )
-----------------------------------------------------------
** VOF METHOD
----------------------------------------
IVOFMT = -1 ( -1: inactive )
( 0: active )
** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION
----------------------------------------
ICAVIT = -1 (-1: single phase flow )
( 0: no vap./cond. model )
( 1: Merkle's model )
-----------------------------------------------------------
** TIME STEPPING
-------------
--- 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
PotTemp 1 0.1000E+01
No2 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 )
-----------------------------------------------------------
** STOKES
------
-- Phase continue :
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 )
-----------------------------------------------------------
** 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
PotTemp 0.1000E-07 1
No2 0.1000E-07 1
------------------------------------
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
-------------------------------------------------------------
No2 1 0 0 0.1815E-04 0.7000E+00
PotTemp 2 1 0 0.1830E-04 0.7000E+00
-------------------------------------------------------------
------------------------------------
Variable Number RVARFL
------------------------------------
No2 1 0.8000E+00
PotTemp 2 0.8000E+00
-------------------------------------------
-------------------------------------------------------
Variable Number ICLVFL SCAMIN SCAMAX
-------------------------------------------------------
No2 1 -1 -0.1000E+13 0.1000E+13
PotTemp 2 -1 0.0000E+00 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
2 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 )
--- Probe history files
NTHIST = 1 (Output frequency )
FRHIST = -.10000E+01 (Output frequency (s) )
-- -- --
--- Log files
NTLIST = 1 (Output frequency )
Number Name IWARNI verbosity level
(-999: not applicable)
Velocity 0
Pressure 0
k 0
epsilon 0
PotTemp 0
No2 0
PotTemp -999
Density -999
Boundary Density -999
CourantNb -999
FourierNb -999
RealTemp -999
Local Time Step -999
Yplus -999
-- -- --
--- Additional post-processing variables (ipstdv)
ipstfo = 1 (Force exerted by the
fluid on the boundary)
ipstyp = 1 (y+ at boundary)
ipsttp = 0 (T+ at 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:
time dependency: fixed mesh
output: every 1.00000e+00 s and at calculation end
-5: name:
directory: monitoring
format: time_plot
options:
time dependency: fixed mesh
output: every 1 time steps
-6: name:
directory: profiles
format: plot
options:
time dependency: fixed mesh
output: at calculation end
Reading file: mesh_input
Finished reading: mesh_input
No "partition_input/domain_number_4" file available;
----------------------------------------------------------
Partitioning 1217550 cells to 4 domains on 4 ranks
(SCOTCH_dgraphPart).
wall-clock time: 0.967980 s
Number of cells per domain (histogramm):
[ 297808 ; 299142 [ = 2
[ 299142 ; 300477 [ = 0
[ 300477 ; 301812 [ = 0
[ 301812 ; 303147 [ = 0
[ 303147 ; 304482 [ = 0
[ 304482 ; 305817 [ = 0
[ 305817 ; 307152 [ = 0
[ 307152 ; 308487 [ = 0
[ 308487 ; 309822 [ = 1
[ 309822 ; 311157 ] = 1
Writing file: partition_output/domain_number_4
Finished writing: partition_output/domain_number_4
Partitioning finished (1.35 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 = 297808
maximum value = 311157
1 : [ 297808 ; 300477 [ = 2
2 : [ 300477 ; 303147 [ = 0
3 : [ 303147 ; 305817 [ = 0
4 : [ 305817 ; 308487 [ = 0
5 : [ 308487 ; 311157 ] = 2
----------------------------------------------------------
Histogram of the number of standard + halo cells per rank:
minimum value = 300792
maximum value = 314393
1 : [ 300792 ; 303512 [ = 2
2 : [ 303512 ; 306232 [ = 0
3 : [ 306232 ; 308952 [ = 0
4 : [ 308952 ; 311672 [ = 0
5 : [ 311672 ; 314393 ] = 2
----------------------------------------------------------
Histogram of the number of ghost cells per rank:
minimum value = 2624
maximum value = 3236
1 : [ 2624 ; 2746 [ = 1
2 : [ 2746 ; 2868 [ = 0
3 : [ 2868 ; 2991 [ = 2
4 : [ 2991 ; 3113 [ = 0
5 : [ 3113 ; 3236 ] = 1
----------------------------------------------------------
Histogram of the number of interior faces per rank:
minimum value = 586866
maximum value = 611649
1 : [ 586866 ; 591822 [ = 2
2 : [ 591822 ; 596779 [ = 0
3 : [ 596779 ; 601735 [ = 0
4 : [ 601735 ; 606692 [ = 0
5 : [ 606692 ; 611649 ] = 2
----------------------------------------------------------
Histogram of the number of boundary faces per rank:
minimum value = 24745
maximum value = 155202
1 : [ 24745 ; 50836 [ = 3
2 : [ 50836 ; 76927 [ = 0
3 : [ 76927 ; 103019 [ = 0
4 : [ 103019 ; 129110 [ = 0
5 : [ 129110 ; 155202 ] = 1
----------------------------------------------------------
Histogram of the number of interior faces per cell:
minimum value = 1
maximum value = 4
1 : [ 1 ; 2 [ = 7
2 : [ 2 ; 3 [ = 867
3 : [ 3 ; 4 ] = 1216676
----------------------------------------------------------
Histogram of the number of neighboring domains per rank:
minimum value = 3
maximum value = 3
1 : [ 3 ; 3 ] = 4
----------------------------------------------------------
Global definition of the number of elements (cells, vertices, faces...)
Synchronizing cell families
Renumbering mesh:
renumbering for cells:
pre-numbering: none
cells adjacent to ghost cells last: no
numbering: none
renumbering for interior faces:
cell adjacency pre-ordering: lowest id first
faces adjacent to ghost cells last: no
numbering: none
renumbering for boundary faces:
numbering: none
----------------------------------------------------------
Histogram of volume mesh matrix bandwidth per rank:
minimum value = 268129
maximum value = 312162
1 : [ 268129 ; 276935 [ = 1
2 : [ 276935 ; 285742 [ = 0
3 : [ 285742 ; 294548 [ = 0
4 : [ 294548 ; 303355 [ = 1
5 : [ 303355 ; 312162 ] = 2
Histogram of volume mesh matrix profile/lines per rank:
minimum value = 3689
maximum value = 12643
1 : [ 3689 ; 5479 [ = 1
2 : [ 5479 ; 7270 [ = 0
3 : [ 7270 ; 9061 [ = 1
4 : [ 9061 ; 10852 [ = 1
5 : [ 10852 ; 12643 ] = 1
Mesh coordinates: minimum and maximum
X : -5.2468764e+03 -4.4687636e+02
Y : 8.3536515e+02 5.6353651e+03
Z : 8.4535616e+02 1.8358480e+03
Mesh
Number of cells: 1217550
Number of interior faces: 2390709
Number of boundary faces: 231176
Number of vertices: 310654
Groups:
"atmo"
boundary faces: 6776
"batiments"
boundary faces: 10801
"sol"
boundary faces: 71197
"sortie"
boundary faces: 8
"zone"
cells: 1217550
--- Information on the volumes
Minimum control volume = 5.6744883e-02
Maximum control volume = 8.6477605e+05
Total volume for the domain = 1.4561449e+10
Criterion 1: Orthogonality:
Number of bad cells detected: 0 --> 0 %
Criterion 2: Offset:
Number of bad cells detected: 20770 --> 2 %
Criterion 3: Least-Squares Gradient Quality:
Number of bad cells detected: 676 --> 0 %
Criterion 4: Cells Volume Ratio:
Number of bad cells detected: 0 --> 0 %
Criterion 5: Guilt by Association:
Number of bad cells detected: 0 --> 0 %
Warning:
--------
Mesh quality issue has been detected
The mesh should be re-considered using the listed criteria.
The calculation will run but the solution quality may be degraded...
Computing geometric quantities (0.801 s)
ALMAX = 0.24419E+04 (Characteristic length )
ALMAX is the cubic root of the domain volume.
ALMAX is the length used to initialize the turbulence.
Reading dimensions for meteo profiles
Reading meteo profiles data
===================================================
printing meteo profiles
year, quant-day, hour, minute, second:
2018 15 11 23 8.00
tmmet(itp):
0.00
zdmet, umet, vmet, ekmet, epmet:
1.00 -0.00 -3.08 0.166E+00 0.261E-01
2.00 -0.00 -3.46 0.166E+00 0.131E-01
4.00 -0.00 -3.84 0.166E+00 0.654E-02
8.00 -0.00 -4.21 0.166E+00 0.327E-02
16.00 -0.00 -4.59 0.166E+00 0.164E-02
32.00 -0.00 -4.96 0.166E+00 0.818E-03
64.00 -0.00 -5.34 0.166E+00 0.409E-03
128.00 -0.00 -5.72 0.166E+00 0.204E-03
256.00 -0.00 -6.09 0.166E+00 0.102E-03
512.00 -0.00 -6.47 0.166E+00 0.511E-04
1024.00 -0.00 -6.85 0.166E+00 0.256E-04
1524.00 -0.00 -7.06 0.166E+00 0.172E-04
2024.00 -0.00 -7.22 0.166E+00 0.129E-04
ztmet,ttmet,tpmet,rmet,phmet,qvmet:
1.00 19.22 292.08 1.1959 100350.000 0.831E-02
2.00 19.16 292.03 1.1960 100338.268 0.828E-02
4.00 19.10 291.99 1.1960 100314.802 0.825E-02
8.00 19.04 291.97 1.1957 100267.877 0.822E-02
16.00 18.98 291.98 1.1948 100174.074 0.818E-02
32.00 18.92 292.08 1.1928 99986.692 0.815E-02
64.00 18.86 292.33 1.1886 99612.900 0.812E-02
128.00 18.79 292.88 1.1800 98869.349 0.809E-02
256.00 18.73 294.06 1.1627 97398.551 0.806E-02
512.00 18.67 296.50 1.1286 94521.677 0.803E-02
1024.00 18.61 301.50 1.0631 89019.225 0.800E-02
1524.00 18.58 306.48 1.0027 83954.214 0.798E-02
2024.00 18.55 311.56 0.9458 79176.915 0.797E-02
-----------------------------------------------------------
** VARIABLES INITIALIZATION
------------------------
-----------------------------------------
Variable Min. value Max. value
-----------------------------------------
Velocity -0.0000E+00 -0.0000E+00
Velocity -0.7154E+01 -0.6723E+01
Velocity 0.0000E+00 0.0000E+00
Pressure 0.0000E+00 0.0000E+00
k 0.1660E+00 0.1660E+00
epsilon 0.1462E-04 0.3385E-04
PotTemp 0.2999E+03 0.3095E+03
No2 0.0000E+00 0.0000E+00
---------------------------------
dt 0.1000E+01 0.1000E+01
---------------------------------
-------------------------------------------------------------
-------------------------------------------------------------
===============================================================
MAIN CALCULATION
================
===============================================================
===============================================================
INSTANT 0.100000000E+01 TIME STEP NUMBER 1
=============================================================
-----------------------------------------
Property Min. value Max. value
-----------------------------------------
density 0.9682E+00 0.1084E+01
molecular_viscos 0.1830E-04 0.1830E-04
turbulent_viscos 0.7939E+02 0.1642E+03
-----------------------------------------
--- Diffusivity:
-----------------------------------------------
Scalar Number Min. value Max. value
-----------------------------------------------
No2 1 0.1815E-04 0.1815E-04
PotTemp 2 0.1830E-04 0.1830E-04
-----------------------------------------------
** INFORMATION ON BOUNDARY FACES TYPE
----------------------------------
-------------------------------------------------------------------------
Boundary type Code Nb faces
-------------------------------------------------------------------------
Inlet 2 4258
Smooth wall 5 153195
Rough wall 6 71197
Symmetry 4 0
Free outlet 3 2526
Free inlet 14 0
Convective inlet 16 0
Free surface 15 0
Undefined 1 0
-------------------------------------------------------------------------
Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
XYZP0 = -0.13109E+04 0.13914E+04 0.94102E+03
** BOUNDARY MASS FLOW INFORMATION
------------------------------
---------------------------------------------------------------
Boundary type Code Nb faces Mass flow
---------------------------------------------------------------
Inlet 2 4258 0.000000000E+00
Smooth wall 5 153195 0.000000000E+00
Rough wall 6 71197 0.000000000E+00
Symmetry 4 0 0.000000000E+00
Free outlet 3 2526 0.000000000E+00
Free inlet 14 0 0.000000000E+00
Convective inlet 16 0 0.000000000E+00
Free surface 15 0 0.000000000E+00
Undefined 1 0 0.000000000E+00
---------------------------------------------------------------
** BOUNDARY CONDITIONS FOR SMOOTH WALLS
---------------------------------------
------------------------------------------------------------
Minimum Maximum
------------------------------------------------------------
Rel velocity at the wall uiptn : 0.13441E+00 0.62178E+01
Friction velocity uet : 0.57064E-02 0.29815E+00
Friction velocity uk : 0.22313E+00 0.22313E+00
Dimensionless distance yplus : 0.17890E+04 0.21169E+06
Friction thermal sca. tstar : 0.00000E+00 0.00000E+00
Rough dim-less th. sca. tplus : 0.15235E+04 0.15315E+04
------------------------------------------------------
Nb of reversal of the velocity at the wall : 0
Nb of faces within the viscous sub-layer : 0
Total number of wall faces : 153195
------------------------------------------------------------
** BOUNDARY CONDITIONS FOR ROUGH WALLS
--------------------------------------
------------------------------------------------------------
Minimum Maximum
------------------------------------------------------------
Rel velocity at the wall uiptn : 0.47313E+01 0.68201E+01
Friction velocity uet : 0.11077E+01 0.10481E+02
Friction velocity uk : 0.22313E+00 0.22313E+00
Rough dimensionless dist yplus : 0.29978E+00 0.12007E+02
Friction thermal sca. tstar : 0.00000E+00 0.00000E+00
Rough dim-less th. sca. tplus : 0.15795E-01 0.12143E+00
------------------------------------------------------
Nb of reversal of the velocity at the wall : 0
------------------------------------------------------------
Hydrostatic pressure computation:
updating the Dirichlets at the end (CALHYD)
** INFORMATION ON CONVERGENCE
--------------------------
----------------------------------------------------------------------------
Variable Rhs norm N_iter Norm. residual Drift Time residual
----------------------------------------------------------------------------
c Velocity 0.31453E+09 566 0.98359E-03 0.11841E+01 0.15551E+00
c Velocity[X] 0.31330E+00
c Velocity[Y] 0.68656E+00
c Velocity[Z] 0.18420E+00
c Pressure 0.97051E+06 56 0.14429E+02 0.12501E+02 0.92048E+00
c k 0.74030E+07 337 0.38704E-02 0.19669E-02 0.35034E+00
c epsilon 0.36989E+05 1490 0.19796E+00 0.11492E-03 0.60438E+01
c PotTemp 0.14053E+14 77 0.19571E-04 0.23532E-03 0.88645E-04
c No2 0.29533E+04 308 0.10978E+00 0.25128E-07 0.99902E+01
----------------------------------------------------------------------------
** Clippings for computed fields
-----------------------------
field initial min initial max clips to min clips to max
- --------------- -------------- -------------- ------------ ------------
a k
a epsilon
a PotTemp
a No2
a Local Time Step 0.0010895 169409
** Computed fields on cells
------------------------
field minimum maximum set mean spatial mean
- --------------- -------------- -------------- -------------- --------------
v Velocity[X] -28.625 28.04 0.0054562 -0.052189
v Velocity[Y] -31.838 1.9119 -6.8672 -6.8895
v Velocity[Z] -12.911 14.309 -0.11959 -0.0083109
v ǁVelocityǁ 0.030364 35.259 7.0394 6.9239
v Pressure -2554.2 20630 468.87 274.89
v k 0.11046 3.2394 0.13967 0.12061
v epsilon 1.4628e-05 11.072 0.060559 0.00080488
v PotTemp 299.91 332.99 303.38 305.53
v No2 0 0.64149 1.7546e-05 1.9419e-08
v Density 0.96823 1.0842 1.0404 1.0148
v CourantNb 0 0 0 0
v FourierNb 0.14021 917.89 12.867 1.3954
v RealTemp 18.577 18.673 18.625 18.616
v Local Time Step 0.1 1.1 0.8735 1.0971
** Computed fields on boundary_faces
---------------------------------
field minimum maximum set mean spatial mean
- ---------------- -------------- -------------- -------------- --------------
v PotTemp 299.87 309.55 302.53 303.89
v Boundary Density 0.96823 1.0842 1.0507 1.0348
v Yplus 0 2.1169e+05 42801 36307
** Computed values on cells
------------------------
criterion minimum maximum set mean spatial mean
--------------- -------------- -------------- -------------- --------------
Courant/Fourier 0.14021 917.89 12.867 1.3954
INSTANT 0.200000000E+01 TIME STEP NUMBER 2
=============================================================
@
@
@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@
@ @@ WARNING: ABORT BY BOUNDARY CONDITION CHECK
@ ========
@ INCORRECT OR INCOMPLETE BOUNDARY CONDITIONS
@
@ At least one boundary face declared as inlet (or
@ outlet) with prescribed velocity with an entering
@ flow for which the value of a variable has not been
@ specified (Dirichlet condition).
@ The calculation will not be run.
@
@ Verify the boundary condition definitions in the GUI
@ or in the appropriate user subroutine.
@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@
First face with boundary condition definition error
(out of 8)
has boundary condition type 0, center (0, 0, 0)
/home/noam/Downloads/code_saturne-5.0.9/src/base/cs_boundary_conditions.c:363: Fatal error.
Some boundary condition definitions are incomplete or incorrect.
For details, read the end of the calculation log,
or visualize the error postprocessing output.
Call stack:
1: 0x7f60cd236296 <bft_error+0xc0> (libsaturne.so.5)
2: 0x7f60cc5678ac <cs_boundary_conditions_error+0x11b> (libsaturne.so.5)
3: 0x7f60cd1e087b <__cs_c_bindings_MOD_boundary_conditions_error+0x20> (libsaturne.so.5)
4: 0x7f60cc753644 <typecl_+0x11c87> (libsaturne.so.5)
5: 0x7f60cc4e2851 <condli_+0x1c2f> (libsaturne.so.5)
6: 0x7f60cc73c0c9 <tridim_+0x8f9a> (libsaturne.so.5)
7: 0x7f60cc4739be <caltri_+0x3afd> (libsaturne.so.5)
8: 0x7f60cc435004 <cs_run+0x4ba> (libsaturne.so.5)
9: 0x7f60cc4352b5 <main+0x15b> (libsaturne.so.5)
10: 0x7f60cbd7db97 <__libc_start_main+0xe7> (libc.so.6)
11: 0x55e74414c8da <_start+0x2a> (cs_solver)
End of stack
Thank you for your time !
Noam