smesh/src/SMESH_SWIG/SMESH_Partition1_tetra.py

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# -*- coding: iso-8859-1 -*-
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# Copyright (C) 2007-2021 CEA/DEN, EDF R&D, OPEN CASCADE
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#
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# Copyright (C) 2003-2007 OPEN CASCADE, EADS/CCR, LIP6, CEA/DEN,
# CEDRAT, EDF R&D, LEG, PRINCIPIA R&D, BUREAU VERITAS
#
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# This library is free software; you can redistribute it and/or
# modify it under the terms of the GNU Lesser General Public
# License as published by the Free Software Foundation; either
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# version 2.1 of the License, or (at your option) any later version.
#
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# This library 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
# Lesser General Public License for more details.
#
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# You should have received a copy of the GNU Lesser General Public
# License along with this library; if not, write to the Free Software
# Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
#
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# See http://www.salome-platform.org/ or email : webmaster.salome@opencascade.com
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#
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# Tetrahedrization of the geometry generated by the Python script GEOM_Partition1.py
# Hypothesis and algorithms for the mesh generation are global
# -- Rayon de la bariere
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#
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import salome
salome.salome_init()
import GEOM
from salome.geom import geomBuilder
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geompy = geomBuilder.New()
import SMESH, SALOMEDS
from salome.smesh import smeshBuilder
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smesh = smeshBuilder.New()
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from math import sqrt
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#---------------------------------------------------------------
barier_height = 7.0
barier_radius = 5.6 / 2 # Rayon de la bariere
colis_radius = 1.0 / 2 # Rayon du colis
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colis_step = 2.0 # Distance s<>parant deux colis
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cc_width = 0.11 # Epaisseur du complement de colisage
# --
cc_radius = colis_radius + cc_width
colis_center = sqrt(2.0)*colis_step/2
# --
boolean_common = 1
boolean_cut = 2
boolean_fuse = 3
boolean_section = 4
# --
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p0 = geompy.MakeVertex(0.,0.,0.)
vz = geompy.MakeVectorDXDYDZ(0.,0.,1.)
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# --
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barier = geompy.MakeCylinder(p0, vz, barier_radius, barier_height)
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# --
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colis = geompy.MakeCylinder(p0, vz, colis_radius, barier_height)
cc = geompy.MakeCylinder(p0, vz, cc_radius, barier_height)
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colis_cc = geompy.MakeCompound([colis, cc])
colis_cc = geompy.MakeTranslation(colis_cc, colis_center, 0.0, 0.0)
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colis_cc_multi = geompy.MultiRotate1D(colis_cc, vz, 4)
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# --
Compound1 = geompy.MakeCompound([colis_cc_multi, barier])
SubShape_theShape = geompy.SubShapeAll(Compound1,geompy.ShapeType["SOLID"])
alveole = geompy.MakePartition(SubShape_theShape)
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print("Analysis of the geometry to mesh (right after the Partition) :")
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subShellList = geompy.SubShapeAll(alveole, geompy.ShapeType["SHELL"])
subFaceList = geompy.SubShapeAll(alveole, geompy.ShapeType["FACE"])
subEdgeList = geompy.SubShapeAll(alveole, geompy.ShapeType["EDGE"])
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print("number of Shells in alveole : ", len(subShellList))
print("number of Faces in alveole : ", len(subFaceList))
print("number of Edges in alveole : ", len(subEdgeList))
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subshapes = geompy.SubShapeAll(alveole, geompy.ShapeType["SHAPE"])
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## there are 9 sub-shapes
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comp1 = geompy.MakeCompound( [ subshapes[0], subshapes[1] ] )
comp2 = geompy.MakeCompound( [ subshapes[2], subshapes[3] ] )
comp3 = geompy.MakeCompound( [ subshapes[4], subshapes[5] ] )
comp4 = geompy.MakeCompound( [ subshapes[6], subshapes[7] ] )
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compGOs = []
compGOs.append( comp1 )
compGOs.append( comp2 )
compGOs.append( comp3 )
compGOs.append( comp4 )
comp = geompy.MakeCompound( compGOs )
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alveole = geompy.MakeCompound( [ comp, subshapes[8] ])
idalveole = geompy.addToStudy(alveole, "alveole")
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print("Analysis of the geometry to mesh (right after the MakeCompound) :")
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subShellList = geompy.SubShapeAll(alveole, geompy.ShapeType["SHELL"])
subFaceList = geompy.SubShapeAll(alveole, geompy.ShapeType["FACE"])
subEdgeList = geompy.SubShapeAll(alveole, geompy.ShapeType["EDGE"])
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print("number of Shells in alveole : ", len(subShellList))
print("number of Faces in alveole : ", len(subFaceList))
print("number of Edges in alveole : ", len(subEdgeList))
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status = geompy.CheckShape(alveole)
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print(" check status ", status)
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# ---- init a Mesh with the alveole
shape_mesh = salome.IDToObject( idalveole )
mesh = smesh.Mesh(shape_mesh, "MeshAlveole")
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print("-------------------------- create Hypothesis (In this case global hypothesis are used)")
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print("-------------------------- NumberOfSegments")
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numberOfSegments = 10
regular1D = mesh.Segment()
hypNbSeg = regular1D.NumberOfSegments(numberOfSegments)
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print(hypNbSeg.GetName())
print(hypNbSeg.GetId())
print(hypNbSeg.GetNumberOfSegments())
smesh.SetName(hypNbSeg, "NumberOfSegments_" + str(numberOfSegments))
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print("-------------------------- MaxElementArea")
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maxElementArea = 0.1
mefisto2D = mesh.Triangle()
hypArea = mefisto2D.MaxElementArea(maxElementArea)
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print(hypArea.GetName())
print(hypArea.GetId())
print(hypArea.GetMaxElementArea())
smesh.SetName(hypArea, "MaxElementArea_" + str(maxElementArea))
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print("-------------------------- MaxElementVolume")
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maxElementVolume = 0.5
netgen3D = mesh.Tetrahedron(smeshBuilder.NETGEN)
hypVolume = netgen3D.MaxElementVolume(maxElementVolume)
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print(hypVolume.GetName())
print(hypVolume.GetId())
print(hypVolume.GetMaxElementVolume())
smesh.SetName(hypVolume, "MaxElementVolume_" + str(maxElementVolume))
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print("-------------------------- compute the mesh of alveole ")
ret = mesh.Compute()
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if ret != 0:
log=mesh.GetLog(0) # no erase trace
# for linelog in log:
# print(linelog)
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print("Information about the Mesh_mechanic:")
print("Number of nodes : ", mesh.NbNodes())
print("Number of edges : ", mesh.NbEdges())
print("Number of faces : ", mesh.NbFaces())
print("Number of triangles : ", mesh.NbTriangles())
print("Number of volumes : ", mesh.NbVolumes())
print("Number of tetrahedrons: ", mesh.NbTetras())
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else:
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print("problem when computing the mesh")
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salome.sg.updateObjBrowser()