+++ /dev/null
-# -*- coding: iso-8859-1 -*-
-# Copyright (C) 2007-2012 CEA/DEN, EDF R&D, OPEN CASCADE
-#
-# Copyright (C) 2003-2007 OPEN CASCADE, EADS/CCR, LIP6, CEA/DEN,
-# CEDRAT, EDF R&D, LEG, PRINCIPIA R&D, BUREAU VERITAS
-#
-# 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
-# version 2.1 of the License.
-#
-# 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.
-#
-# 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
-#
-# See http://www.salome-platform.org/ or email : webmaster.salome@opencascade.com
-#
-
-# Triangulation of the skin of the geometry from a Brep representing a plane
-# Hypothesis and algorithms for the mesh generation are global
-#
-import os
-import salome
-import geompy
-import smesh
-
-
-# ---------------------------- GEOM --------------------------------------
-
-# import a BRep
-#before running this script, please be sure about
-#the path the file fileName
-
-filePath = os.environ["DATA_DIR"]
-filePath = filePath + "/Shapes/Brep/"
-
-filename = "flight_solid.brep"
-filename = filePath + filename
-
-shape = geompy.Import(filename, "BREP")
-idShape = geompy.addToStudy(shape, "flight")
-
-print "Analysis of the geometry flight :"
-subShellList = geompy.SubShapeAll(shape, geompy.ShapeType["SHELL"])
-subFaceList = geompy.SubShapeAll(shape, geompy.ShapeType["FACE"])
-subEdgeList = geompy.SubShapeAll(shape, geompy.ShapeType["EDGE"])
-
-print "number of Shells in flight : ", len(subShellList)
-print "number of Faces in flight : ", len(subFaceList)
-print "number of Edges in flight : ", len(subEdgeList)
-
-
-### ---------------------------- SMESH --------------------------------------
-smesh.SetCurrentStudy(salome.myStudy)
-
-# ---- init a Mesh with the shell
-shape_mesh = salome.IDToObject( idShape )
-
-mesh = smesh.Mesh(shape_mesh, "MeshFlight")
-
-
-# ---- set Hypothesis and Algorithm
-
-print "-------------------------- LocalLength"
-
-lengthOfSegments = 0.3
-
-regular1D = mesh.Segment()
-hypLength = regular1D.LocalLength(lengthOfSegments)
-print hypLength.GetName()
-print hypLength.GetId()
-print hypLength.GetLength()
-smesh.SetName(hypLength, "LocalLength_" + str(lengthOfSegments))
-
-print "-------------------------- LengthFromEdges"
-
-mefisto2D = mesh.Triangle()
-hypLengthFromEdge = mefisto2D.LengthFromEdges()
-print hypLengthFromEdge.GetName()
-print hypLengthFromEdge.GetId()
-smesh.SetName(hypLengthFromEdge,"LengthFromEdge")
-
-
-salome.sg.updateObjBrowser(1)
-
-
-print "-------------------------- compute the skin flight"
-ret = mesh.Compute()
-print ret
-if ret != 0:
- log = mesh.GetLog(0) # no erase trace
- for linelog in log:
- print linelog
- print "Information about the Mesh_mechanic_tetra:"
- 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()
-else:
- print "probleme when computing the mesh"
