# *************************************************************************** # * * # * Copyright (c) 2015 - Przemo Firszt * # * Copyright (c) 2015 - Bernd Hahnebach * # * * # * This program is free software; you can redistribute it and/or modify * # * it under the terms of the GNU Lesser General Public License (LGPL) * # * as published by the Free Software Foundation; either version 2 of * # * the License, or (at your option) any later version. * # * for detail see the LICENCE text file. * # * * # * This program 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 Library General Public License for more details. * # * * # * You should have received a copy of the GNU Library General Public * # * License along with this program; if not, write to the Free Software * # * Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA 02111-1307 * # * USA * # * * # *************************************************************************** import FreeCAD import os import sys import time __title__ = "ccxInpWriter" __author__ = "Przemo Firszt, Bernd Hahnebach" __url__ = "http://www.freecadweb.org" class inp_writer: def __init__(self, analysis_obj, mesh_obj, mat_obj, fixed_obj, force_obj, pressure_obj, beamsection_obj, shellthickness_obj, analysis_type=None, eigenmode_parameters=None, dir_name=None): self.dir_name = dir_name self.analysis = analysis_obj self.mesh_object = mesh_obj self.material_objects = mat_obj self.fixed_objects = fixed_obj self.force_objects = force_obj self.pressure_objects = pressure_obj if eigenmode_parameters: self.no_of_eigenfrequencies = eigenmode_parameters[0] self.eigenfrequeny_range_low = eigenmode_parameters[1] self.eigenfrequeny_range_high = eigenmode_parameters[2] self.analysis_type = analysis_type self.beamsection_objects = beamsection_obj self.shellthickness_objects = shellthickness_obj if not dir_name: self.dir_name = FreeCAD.ActiveDocument.TransientDir.replace('\\', '/') + '/FemAnl_' + analysis_obj.Uid[-4:] if not os.path.isdir(self.dir_name): os.mkdir(self.dir_name) self.base_name = self.mesh_object.Name self.file_name = self.dir_name + '/' + self.base_name + '.inp' self.fc_ver = FreeCAD.Version() self.ccx_eall = 'Eall' self.ccx_elsets = [] def write_calculix_input_file(self): self.mesh_object.FemMesh.writeABAQUS(self.file_name) # reopen file with "append" and add the analysis definition inpfile = open(self.file_name, 'a') inpfile.write('\n\n') self.write_element_sets_material_and_femelement_type(inpfile) self.write_node_sets_constraints_fixed(inpfile) self.write_node_sets_constraints_force(inpfile) self.write_materials(inpfile) self.write_femelementsets(inpfile) self.write_step_begin(inpfile) self.write_constraints_fixed(inpfile) if self.analysis_type is None or self.analysis_type == "static": self.write_constraints_force(inpfile) self.write_constraints_pressure(inpfile) elif self.analysis_type == "frequency": self.write_frequency(inpfile) self.write_outputs_types(inpfile) self.write_step_end(inpfile) self.write_footer(inpfile) inpfile.close() return self.file_name def write_element_sets_material_and_femelement_type(self, f): if len(self.material_objects) == 1: if self.beamsection_objects and len(self.beamsection_objects) == 1: # single mat, single beam self.get_ccx_elsets_single_mat_single_beam() elif self.beamsection_objects and len(self.beamsection_objects) > 1: # single mat, multiple beams self.get_ccx_elsets_single_mat_multiple_beam() elif self.shellthickness_objects and len(self.shellthickness_objects) == 1: # single mat, single shell self.get_ccx_elsets_single_mat_single_shell() elif self.shellthickness_objects and len(self.shellthickness_objects) > 1: # single mat, multiple shells self.get_ccx_elsets_single_mat_multiple_shell() else: # single mat, solid self.get_ccx_elsets_single_mat_solid() else: if self.beamsection_objects and len(self.beamsection_objects) == 1: # multiple mats, single beam self.get_ccx_elsets_multiple_mat_single_beam() elif self.beamsection_objects and len(self.beamsection_objects) > 1: # multiple mats, multiple beams self.get_ccx_elsets_multiple_mat_multiple_beam() if self.shellthickness_objects and len(self.shellthickness_objects) == 1: # multiple mats, single shell self.get_ccx_elsets_multiple_mat_single_shell() elif self.shellthickness_objects and len(self.shellthickness_objects) > 1: # multiple mats, multiple shells self.get_ccx_elsets_multiple_mat_multiple_shell() else: # multiple mats, solid self.get_ccx_elsets_multiple_mat_solid() f.write('\n***********************************************************\n') f.write('** Element sets for materials and FEM element type (solid, shell, beam)\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) for ccx_elset in self.ccx_elsets: # print(ccx_elset) f.write('*ELSET,ELSET=' + ccx_elset['ccx_elset_name'] + '\n') if ccx_elset['ccx_elset'] == self.ccx_eall: f.write(self.ccx_eall + '\n') else: for elid in ccx_elset['ccx_elset']: f.write(str(elid) + ',\n') def write_node_sets_constraints_fixed(self, f): f.write('\n***********************************************************\n') f.write('** Node set for fixed constraint\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) for fobj in self.fixed_objects: fix_obj = fobj['Object'] f.write('*NSET,NSET=' + fix_obj.Name + '\n') for o, elem in fix_obj.References: fo = o.Shape.getElement(elem) n = [] if fo.ShapeType == 'Face': n = self.mesh_object.FemMesh.getNodesByFace(fo) elif fo.ShapeType == 'Edge': n = self.mesh_object.FemMesh.getNodesByEdge(fo) elif fo.ShapeType == 'Vertex': n = self.mesh_object.FemMesh.getNodesByVertex(fo) for i in n: f.write(str(i) + ',\n') def write_node_sets_constraints_force(self, f): f.write('\n***********************************************************\n') f.write('** Node sets for loads\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) for fobj in self.force_objects: frc_obj = fobj['Object'] f.write('*NSET,NSET=' + frc_obj.Name + '\n') NbrForceNodes = 0 for o, elem in frc_obj.References: fo = o.Shape.getElement(elem) n = [] if fo.ShapeType == 'Edge': n = self.mesh_object.FemMesh.getNodesByEdge(fo) elif fo.ShapeType == 'Vertex': n = self.mesh_object.FemMesh.getNodesByVertex(fo) for i in n: f.write(str(i) + ',\n') NbrForceNodes = NbrForceNodes + 1 # NodeSum of mesh-nodes of ALL reference shapes from force_object # calculate node load if NbrForceNodes != 0: fobj['NodeLoad'] = (frc_obj.Force) / NbrForceNodes # FIXME for loads on edges the node count is used to distribute the load on the edges. # In case of a not uniform fem mesh this could result in wrong force distribution # and thus in wrong analysis results. see def write_constraints_force() f.write('** concentrated load [N] distributed on all mesh nodes of the given shapes\n') f.write('** ' + str(frc_obj.Force) + ' N / ' + str(NbrForceNodes) + ' Nodes = ' + str(fobj['NodeLoad']) + ' N on each node\n') if frc_obj.Force == 0: print(' Warning --> Force = 0') def write_materials(self, f): f.write('\n***********************************************************\n') f.write('** Materials\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) f.write('** Young\'s modulus unit is MPa = N/mm2\n') for m in self.material_objects: mat_obj = m['Object'] # get material properties YM = FreeCAD.Units.Quantity(mat_obj.Material['YoungsModulus']) YM_in_MPa = YM.getValueAs('MPa') PR = float(mat_obj.Material['PoissonRatio']) mat_name = mat_obj.Material['Name'][:80] # write material properties f.write('*MATERIAL, NAME=' + mat_name + '\n') f.write('*ELASTIC \n') f.write('{}, \n'.format(YM_in_MPa)) f.write('{0:.3f}\n'.format(PR)) density = FreeCAD.Units.Quantity(mat_obj.Material['Density']) density_in_tone_per_mm3 = float(density.getValueAs('t/mm^3')) f.write('*DENSITY \n') f.write('{0:.3e}, \n'.format(density_in_tone_per_mm3)) def write_femelementsets(self, f): f.write('\n***********************************************************\n') f.write('** Sections\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) for ccx_elset in self.ccx_elsets: if 'beamsection_obj'in ccx_elset: # beam mesh beamsec_obj = ccx_elset['beamsection_obj'] elsetdef = 'ELSET=' + ccx_elset['ccx_elset_name'] + ', ' material = 'MATERIAL=' + ccx_elset['ccx_mat_name'] setion_def = '*BEAM SECTION, ' + elsetdef + material + ', SECTION=RECT\n' setion_geo = str(beamsec_obj.Height.getValueAs('mm')) + ', ' + str(beamsec_obj.Width.getValueAs('mm')) + '\n' f.write(setion_def) f.write(setion_geo) elif 'shellthickness_obj'in ccx_elset: # shell mesh shellth_obj = ccx_elset['shellthickness_obj'] elsetdef = 'ELSET=' + ccx_elset['ccx_elset_name'] + ', ' material = 'MATERIAL=' + ccx_elset['ccx_mat_name'] setion_def = '*SHELL SECTION, ' + elsetdef + material + '\n' setion_geo = str(shellth_obj.Thickness.getValueAs('mm')) + '\n' f.write(setion_def) f.write(setion_geo) else: # solid mesh elsetdef = 'ELSET=' + ccx_elset['ccx_elset_name'] + ', ' material = 'MATERIAL=' + ccx_elset['ccx_mat_name'] setion_def = '*SOLID SECTION, ' + elsetdef + material + '\n' f.write(setion_def) def write_step_begin(self, f): f.write('\n***********************************************************\n') f.write('** One step is needed to calculate the mechanical analysis of FreeCAD\n') f.write('** loads are applied quasi-static, means without involving the time dimension\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) f.write('*STEP\n') f.write('*STATIC\n') def write_constraints_fixed(self, f): f.write('\n***********************************************************\n') f.write('** Constaints\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) for fixed_object in self.fixed_objects: fix_obj_name = fixed_object['Object'].Name f.write('*BOUNDARY\n') f.write(fix_obj_name + ',1\n') f.write(fix_obj_name + ',2\n') f.write(fix_obj_name + ',3\n') if self.beamsection_objects or self.shellthickness_objects: f.write(fix_obj_name + ',4\n') f.write(fix_obj_name + ',5\n') f.write(fix_obj_name + ',6\n') f.write('\n') def write_constraints_force(self, f): f.write('\n***********************************************************\n') f.write('** Node loads\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) if is_shell_mesh(self.mesh_object.FemMesh) or (is_solid_mesh(self.mesh_object.FemMesh) and has_no_face_data(self.mesh_object.FemMesh)): if not hasattr(self, 'fem_element_table'): self.fem_element_table = getFemElementTable(self.mesh_object.FemMesh) for fobj in self.force_objects: frc_obj = fobj['Object'] if 'NodeLoad' in fobj: # load on edges or vertieces node_load = fobj['NodeLoad'] frc_obj_name = frc_obj.Name vec = frc_obj.DirectionVector f.write('*CLOAD\n') f.write('** force: ' + str(node_load) + ' N, direction: ' + str(vec) + '\n') v1 = "{:.13E}".format(vec.x * node_load) v2 = "{:.13E}".format(vec.y * node_load) v3 = "{:.13E}".format(vec.z * node_load) f.write(frc_obj_name + ',1,' + v1 + '\n') f.write(frc_obj_name + ',2,' + v2 + '\n') f.write(frc_obj_name + ',3,' + v3 + '\n\n') # area load on faces sum_ref_face_area = 0 sum_ref_face_node_area = 0 sum_node_load = 0 for o, elem in frc_obj.References: elem_o = o.Shape.getElement(elem) if elem_o.ShapeType == 'Face': sum_ref_face_area += elem_o.Area if sum_ref_face_area != 0: force_per_sum_ref_face_area = frc_obj.Force / sum_ref_face_area for o, elem in frc_obj.References: elem_o = o.Shape.getElement(elem) if elem_o.ShapeType == 'Face': ref_face = elem_o f.write('** ' + frc_obj.Name + '\n') f.write('*CLOAD\n') f.write('** node loads on element face: ' + o.Name + '.' + elem + '\n') face_table = {} # { meshfaceID : ( nodeID, ... , nodeID ) } if is_solid_mesh(self.mesh_object.FemMesh): if has_no_face_data(self.mesh_object.FemMesh): ref_face_volume_elements = self.mesh_object.FemMesh.getccxVolumesByFace(ref_face) # list of tupels ref_face_nodes = self.mesh_object.FemMesh.getNodesByFace(ref_face) for ve in ref_face_volume_elements: veID = ve[0] ve_ref_face_nodes = [] for nodeID in self.fem_element_table[veID]: if nodeID in ref_face_nodes: ve_ref_face_nodes.append(nodeID) face_table[veID] = ve_ref_face_nodes # { volumeID : ( facenodeID, ... , facenodeID ) } else: volume_faces = self.mesh_object.FemMesh.getVolumesByFace(ref_face) # (mv, mf) for mv, mf in volume_faces: face_table[mf] = self.mesh_object.FemMesh.getElementNodes(mf) elif is_shell_mesh(self.mesh_object.FemMesh): ref_face_nodes = self.mesh_object.FemMesh.getNodesByFace(ref_face) ref_face_elements = getFemElementsByNodes(self.fem_element_table, ref_face_nodes) for mf in ref_face_elements: face_table[mf] = self.fem_element_table[mf] # calulate the appropriate node_areas for every node of every mesh face (mf) # G. Lakshmi Narasaiah, Finite Element Analysis, p206ff # FIXME only gives exact results in case of a real triangle. If for S6 or C3D10 elements # the midnodes are not on the line between the end nodes the area will not be a triangle # see http://forum.freecadweb.org/viewtopic.php?f=18&t=10939&start=40#p91355 and ff # [ (nodeID,Area), ... , (nodeID,Area) ] some nodes will have more than one entry node_area_table = [] # { nodeID : Area, ... , nodeID:Area } AreaSum for each node, one entry for each node node_sumarea_table = {} mesh_face_area = 0 for mf in face_table: if len(face_table[mf]) == 3: # 3 node mesh face triangle # corner_node_area = mesh_face_area / 3.0 # P3 # /\ # / \ # /____\ # P1 P2 P1 = self.mesh_object.FemMesh.Nodes[face_table[mf][0]] P2 = self.mesh_object.FemMesh.Nodes[face_table[mf][1]] P3 = self.mesh_object.FemMesh.Nodes[face_table[mf][2]] mesh_face_area = getTriangleArea(P1, P2, P3) corner_node_area = mesh_face_area / 3.0 node_area_table.append((face_table[mf][0], corner_node_area)) node_area_table.append((face_table[mf][1], corner_node_area)) node_area_table.append((face_table[mf][2], corner_node_area)) elif len(face_table[mf]) == 4: # 4 node mesh face quad FreeCAD.Console.PrintError('Face load on 4 node quad faces are not supported\n') elif len(face_table[mf]) == 6: # 6 node mesh face triangle # corner_node_area = 0 # middle_node_area = mesh_face_area / 3.0 # P3 # /\ # /t3\ # / \ # P6------P5 # / \ t4 / \ # /t1 \ /t2 \ # /_____\/_____\ # P1 P4 P2 P1 = self.mesh_object.FemMesh.Nodes[face_table[mf][0]] P2 = self.mesh_object.FemMesh.Nodes[face_table[mf][1]] P3 = self.mesh_object.FemMesh.Nodes[face_table[mf][2]] P4 = self.mesh_object.FemMesh.Nodes[face_table[mf][3]] P5 = self.mesh_object.FemMesh.Nodes[face_table[mf][4]] P6 = self.mesh_object.FemMesh.Nodes[face_table[mf][5]] mesh_face_t1_area = getTriangleArea(P1, P4, P6) mesh_face_t2_area = getTriangleArea(P2, P5, P4) mesh_face_t3_area = getTriangleArea(P3, P6, P5) mesh_face_t4_area = getTriangleArea(P4, P5, P6) mesh_face_area = mesh_face_t1_area + mesh_face_t2_area + mesh_face_t3_area + mesh_face_t4_area middle_node_area = mesh_face_area / 3.0 node_area_table.append((face_table[mf][0], 0)) node_area_table.append((face_table[mf][1], 0)) node_area_table.append((face_table[mf][2], 0)) node_area_table.append((face_table[mf][3], middle_node_area)) node_area_table.append((face_table[mf][4], middle_node_area)) node_area_table.append((face_table[mf][5], middle_node_area)) elif len(face_table[mf]) == 8: # 8 node mesh face quad FreeCAD.Console.PrintError('Face load on 8 node quad faces are not supported\n') # node_sumarea_table for n, A in node_area_table: # print(n, ' --> ', A) if n in node_sumarea_table: node_sumarea_table[n] = node_sumarea_table[n] + A else: node_sumarea_table[n] = A sum_node_areas = 0 for n in node_sumarea_table: sum_node_areas = sum_node_areas + node_sumarea_table[n] sum_ref_face_node_area += sum_node_areas # write CLOAD lines to CalculiX file vec = frc_obj.DirectionVector for n in sorted(node_sumarea_table): node_load = node_sumarea_table[n] * force_per_sum_ref_face_area sum_node_load += node_load if (vec.x != 0.0): v1 = "{:.13E}".format(vec.x * node_load) f.write(str(n) + ',1,' + v1 + '\n') if (vec.y != 0.0): v2 = "{:.13E}".format(vec.y * node_load) f.write(str(n) + ',2,' + v2 + '\n') if (vec.z != 0.0): v3 = "{:.13E}".format(vec.z * node_load) f.write(str(n) + ',3,' + v3 + '\n') f.write('\n') f.write('\n') def write_constraints_pressure(self, f): f.write('\n***********************************************************\n') f.write('** Element + CalculiX face + load in [MPa]\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) for fobj in self.pressure_objects: prs_obj = fobj['Object'] f.write('*DLOAD\n') for o, e in prs_obj.References: rev = -1 if prs_obj.Reversed else 1 elem = o.Shape.getElement(e) if elem.ShapeType == 'Face': v = self.mesh_object.FemMesh.getccxVolumesByFace(elem) f.write("** Load on face {}\n".format(e)) for i in v: f.write("{},P{},{}\n".format(i[0], i[1], rev * prs_obj.Pressure)) def write_frequency(self, f): f.write('\n***********************************************************\n') f.write('** Frequency analysis\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) f.write('*FREQUENCY\n') f.write('{},{},{}\n'.format(self.no_of_eigenfrequencies, self.eigenfrequeny_range_low, self.eigenfrequeny_range_high)) def write_outputs_types(self, f): f.write('\n***********************************************************\n') f.write('** Outputs --> frd file\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) if self.beamsection_objects or self.shellthickness_objects: f.write('*NODE FILE, OUTPUT=2d\n') else: f.write('*NODE FILE\n') f.write('U\n') f.write('*EL FILE\n') f.write('S, E\n') f.write('** outputs --> dat file\n') f.write('*NODE PRINT , NSET=Nall \n') f.write('U \n') f.write('*EL PRINT , ELSET=Eall \n') f.write('S \n') def write_step_end(self, f): f.write('\n***********************************************************\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) f.write('*END STEP \n') def write_footer(self, f): f.write('\n***********************************************************\n') f.write('** CalculiX Input file\n') f.write('** written by {} function\n'.format(sys._getframe().f_code.co_name)) f.write('** written by --> FreeCAD ' + self.fc_ver[0] + '.' + self.fc_ver[1] + '.' + self.fc_ver[2] + '\n') f.write('** written on --> ' + time.ctime() + '\n') f.write('** file name --> ' + os.path.basename(FreeCAD.ActiveDocument.FileName) + '\n') f.write('** analysis name --> ' + self.analysis.Name + '\n') f.write('**\n') f.write('**\n') f.write('**\n') f.write('** Units\n') f.write('**\n') f.write('** Geometry (mesh data) --> mm\n') f.write("** Materials (Young's modulus) --> N/mm2 = MPa\n") f.write('** Loads (nodal loads) --> N\n') f.write('**\n') # self.ccx_elsets = [ { # 'beamsection_obj' : 'beamsection_obj' if exists # 'shellthickness_obj' : shellthickness_obj' if exists # 'ccx_elset' : [e1, e2, e3, ... , en] or string self.ccx_eall # 'ccx_elset_name' : 'ccx_identifier_elset' # 'mat_obj_name' : 'mat_obj.Name' # 'ccx_mat_name' : 'mat_obj.Material['Name'][:80]' !!! not unique !!! # }, # {}, ... , {} ] def get_ccx_elsets_single_mat_single_beam(self): mat_obj = self.material_objects[0]['Object'] beamsec_obj = self.beamsection_objects[0]['Object'] ccx_elset = {} ccx_elset['beamsection_obj'] = beamsec_obj ccx_elset['ccx_elset'] = self.ccx_eall ccx_elset['ccx_elset_name'] = get_ccx_elset_beam_name(mat_obj.Name, beamsec_obj.Name) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_single_mat_single_shell(self): mat_obj = self.material_objects[0]['Object'] shellth_obj = self.shellthickness_objects[0]['Object'] ccx_elset = {} ccx_elset['shellthickness_obj'] = shellth_obj ccx_elset['ccx_elset'] = self.ccx_eall ccx_elset['ccx_elset_name'] = get_ccx_elset_shell_name(mat_obj.Name, shellth_obj.Name) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_single_mat_solid(self): mat_obj = self.material_objects[0]['Object'] ccx_elset = {} ccx_elset['ccx_elset'] = self.ccx_eall ccx_elset['ccx_elset_name'] = get_ccx_elset_solid_name(mat_obj.Name) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_single_mat_multiple_beam(self): mat_obj = self.material_objects[0]['Object'] self.get_femelement_sets(self.beamsection_objects) for beamsec_data in self.beamsection_objects: beamsec_obj = beamsec_data['Object'] ccx_elset = {} ccx_elset['beamsection_obj'] = beamsec_obj ccx_elset['ccx_elset'] = beamsec_data['FEMElements'] ccx_elset['ccx_elset_name'] = get_ccx_elset_beam_name(mat_obj.Name, beamsec_obj.Name, None, beamsec_data['ShortName']) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_single_mat_multiple_shell(self): mat_obj = self.material_objects[0]['Object'] self.get_femelement_sets(self.shellthickness_objects) for shellth_data in self.shellthickness_objects: shellth_obj = shellth_data['Object'] ccx_elset = {} ccx_elset['shellthickness_obj'] = shellth_obj ccx_elset['ccx_elset'] = shellth_data['FEMElements'] ccx_elset['ccx_elset_name'] = get_ccx_elset_shell_name(mat_obj.Name, shellth_obj.Name, None, shellth_data['ShortName']) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_multiple_mat_single_beam(self): beamsec_obj = self.beamsection_objects[0]['Object'] self.get_femelement_sets(self.material_objects) for mat_data in self.material_objects: mat_obj = mat_data['Object'] ccx_elset = {} ccx_elset['beamsection_obj'] = beamsec_obj ccx_elset['ccx_elset'] = mat_data['FEMElements'] ccx_elset['ccx_elset_name'] = get_ccx_elset_beam_name(mat_obj.Name, beamsec_obj.Name, mat_data['ShortName']) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_multiple_mat_single_shell(self): shellth_obj = self.shellthickness_objects[0]['Object'] self.get_femelement_sets(self.material_objects) for mat_data in self.material_objects: mat_obj = mat_data['Object'] ccx_elset = {} ccx_elset['shellthickness_obj'] = shellth_obj ccx_elset['ccx_elset'] = mat_data['FEMElements'] ccx_elset['ccx_elset_name'] = get_ccx_elset_shell_name(mat_obj.Name, shellth_obj.Name, mat_data['ShortName']) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_multiple_mat_solid(self): self.get_femelement_sets(self.material_objects) for mat_data in self.material_objects: mat_obj = mat_data['Object'] ccx_elset = {} ccx_elset['ccx_elset'] = mat_data['FEMElements'] ccx_elset['ccx_elset_name'] = get_ccx_elset_solid_name(mat_obj.Name, None, mat_data['ShortName']) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_multiple_mat_multiple_beam(self): self.get_femelement_sets(self.beamsection_objects) self.get_femelement_sets(self.material_objects) for beamsec_data in self.beamsection_objects: beamsec_obj = beamsec_data['Object'] for mat_data in self.material_objects: mat_obj = mat_data['Object'] ccx_elset = {} ccx_elset['beamsection_obj'] = beamsec_obj elemids = [] for elemid in beamsec_data['FEMElements']: if elemid in mat_data['FEMElements']: elemids.append(elemid) ccx_elset['ccx_elset'] = elemids ccx_elset['ccx_elset_name'] = get_ccx_elset_beam_name(mat_obj.Name, beamsec_obj.Name, mat_data['ShortName'], beamsec_data['ShortName']) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_ccx_elsets_multiple_mat_multiple_shell(self): self.get_femelement_sets(self.shellthickness_objects) self.get_femelement_sets(self.material_objects) for shellth_data in self.shellthickness_objects: shellth_obj = shellth_data['Object'] for mat_data in self.material_objects: mat_obj = mat_data['Object'] ccx_elset = {} ccx_elset['shellthickness_obj'] = shellth_obj elemids = [] for elemid in shellth_data['FEMElements']: if elemid in mat_data['FEMElements']: elemids.append(elemid) ccx_elset['ccx_elset'] = elemids ccx_elset['ccx_elset_name'] = get_ccx_elset_shell_name(mat_obj.Name, shellth_obj.Name, mat_data['ShortName'], shellth_data['ShortName']) ccx_elset['mat_obj_name'] = mat_obj.Name ccx_elset['ccx_mat_name'] = mat_obj.Material['Name'][:80] self.ccx_elsets.append(ccx_elset) def get_femelement_sets(self, fem_objects): # get femelements for reference shapes of each obj.References if not hasattr(self, 'fem_element_table'): self.fem_element_table = getFemElementTable(self.mesh_object.FemMesh) count_femelements = 0 referenced_femelements = [] has_remaining_femelements = None for fem_object_i, fem_object in enumerate(fem_objects): obj = fem_object['Object'] fem_object['ShortName'] = get_ccx_elset_short_name(obj, fem_object_i) # unique short ccx_identifier if obj.References: ref_shape_femelements = [] for ref in obj.References: femnodes = [] femelements = [] r = ref[0].Shape.getElement(ref[1]) print(' ReferenceShape : ', r.ShapeType, ', ', ref[0].Name, ', ', ref[0].Label, ' --> ', ref[1]) if r.ShapeType == 'Edge': femnodes = self.mesh_object.FemMesh.getNodesByEdge(r) elif r.ShapeType == 'Face': femnodes = self.mesh_object.FemMesh.getNodesByFace(r) elif r.ShapeType == 'Solid': # femnodes = self.mesh_object.FemMesh.getNodesBySolid(r) --> TODO FreeCAD.Console.PrintError('Solid Reference Shapes, CalculiX input file may be broken!\n') fem_object['FEMElements'] = self.ccx_eall return else: print(' No Edge, Face or Solid as reference shapes!') femelements = getFemElementsByNodes(self.fem_element_table, femnodes) ref_shape_femelements += femelements referenced_femelements += femelements count_femelements += len(femelements) fem_object['FEMElements'] = ref_shape_femelements else: has_remaining_femelements = obj.Name # get remaining femelements for the fem_objects if has_remaining_femelements: remaining_femelements = [] for elemid in self.fem_element_table: if elemid not in referenced_femelements: remaining_femelements.append(elemid) count_femelements += len(remaining_femelements) for fem_object in fem_objects: obj = fem_object['Object'] if obj.Name == has_remaining_femelements: fem_object['FEMElements'] = sorted(remaining_femelements) # check if all worked out well if not femelements_count_ok(self.fem_element_table, count_femelements): FreeCAD.Console.PrintError('Error in get_femelement_sets -- > femelements_count_ok failed!\n') # Helpers def getTriangleArea(P1, P2, P3): vec1 = P2 - P1 vec2 = P3 - P1 vec3 = vec1.cross(vec2) return 0.5 * vec3.Length def getFemElementTable(fem_mesh): """ getFemElementTable(fem_mesh): { elementid : [ nodeid, nodeid, ... , nodeid ] }""" fem_element_table = {} if is_solid_mesh(fem_mesh): for i in fem_mesh.Volumes: fem_element_table[i] = fem_mesh.getElementNodes(i) elif is_shell_mesh(fem_mesh): for i in fem_mesh.Faces: fem_element_table[i] = fem_mesh.getElementNodes(i) elif is_beam_mesh(fem_mesh): for i in fem_mesh.Edges: fem_element_table[i] = fem_mesh.getElementNodes(i) else: FreeCAD.Console.PrintError('Neither solid nor shell nor beam mesh!\n') return fem_element_table def getFemElementsByNodes(fem_element_table, node_list): '''if all nodes of an fem_element are in node_list, the fem_element is added to the list which is returned e: elementlist nodes: nodelist ''' e = [] # elementlist for elementID in sorted(fem_element_table): nodecount = 0 for nodeID in fem_element_table[elementID]: if nodeID in node_list: nodecount = nodecount + 1 if nodecount == len(fem_element_table[elementID]): # all nodes of the element are in the node_list! e.append(elementID) return e def is_solid_mesh(fem_mesh): if fem_mesh.VolumeCount > 0: # solid mesh return True def has_no_face_data(fem_mesh): if fem_mesh.FaceCount == 0: # mesh has no face data, could be a beam mesh or a solid mesh without face data return True def is_shell_mesh(fem_mesh): if fem_mesh.VolumeCount == 0 and fem_mesh.FaceCount > 0: # shell mesh return True def is_beam_mesh(fem_mesh): if fem_mesh.VolumeCount == 0 and fem_mesh.FaceCount == 0 and fem_mesh.EdgeCount > 0: # beam mesh return True def femelements_count_ok(fem_element_table, count_femelements): if count_femelements == len(fem_element_table): # print('Count Elements written to CalculiX file: ', count_femelements) # print('Count Elements of the FreeCAD FEM Mesh: ', len(fem_element_table)) return True else: print('ERROR: self.fem_element_table != count_femelements') print('Count Elements written to CalculiX file: ', count_femelements) print('Count Elements of the FreeCAD FEM Mesh: ', len(fem_element_table)) return False def get_ccx_elset_beam_name(mat_name, beamsec_name, mat_short_name=None, beamsec_short_name=None): if not mat_short_name: mat_short_name = 'Mat0' if not beamsec_short_name: beamsec_short_name = 'Beam0' if len(mat_name + beamsec_name) > 20: # max identifier lenght in CalculiX for beam elsets return mat_short_name + beamsec_short_name else: return mat_name + beamsec_name def get_ccx_elset_shell_name(mat_name, shellth_name, mat_short_name=None, shellth_short_name=None): if not mat_short_name: mat_short_name = 'Mat0' if not shellth_short_name: shellth_short_name = 'Shell0' if len(mat_name + shellth_name) > 80: # standard max identifier lenght in CalculiX return mat_short_name + shellth_short_name else: return mat_name + shellth_name def get_ccx_elset_solid_name(mat_name, solid_name=None, mat_short_name=None): if not solid_name: solid_name = 'Solid' if not mat_short_name: mat_short_name = 'Mat0' if len(mat_name + solid_name) > 80: # standard max identifier lenght in CalculiX return mat_short_name + solid_name else: return mat_name + solid_name def get_ccx_elset_short_name(obj, i): if hasattr(obj, "Proxy") and obj.Proxy.Type == 'MechanicalMaterial': return 'Mat' + str(i) elif hasattr(obj, "Proxy") and obj.Proxy.Type == 'FemBeamSection': return 'Beam' + str(i) elif hasattr(obj, "Proxy") and obj.Proxy.Type == 'FemShellThickness': return 'Shell' + str(i) else: print 'Error: ', obj.Name, ' --> ', obj.Proxy.Type