*HEADING o TESTING INCREMENTAL DSA FORMULATION FOR PLANE STRAIN ELEMENTS (CPE_) ** ** o AXIAL PULLING OF A BAR ** o HYPERELASTIC MATERIAL ** ** Node/element numbering scheme: ** element test | second and subsequent node prefix label | element label ** cpe3 100_/200_ 100/200 ** cpe3h 101_/201_ 101/201 ** cpe4 102_/202_ 102/202 ** cpe4h 103_/203_ 103/203 ** cpe4i 104_/204_ 104/204 ** cpe4ih 105_/205_ 105/205 ** cpe4r 106_/206_ 106/206 ** cpe4rh 107_/207_ 107/207 ** cpe6 108_/208_ 108/208 ** cpe6h 109_/209_ 109/209 ** cpe6m 110_/210_ 110/210 ** cpe6mh 111_/211_ 111/211 ** cpe8 112_ 112 ** cpe8h 113_ 113 ** cpe8r 114_ 114 ** cpe8rh 115_ 115 ** ** The "_" is replaced by the node number for an element. All models ** are two elements except for the 8 noded elements. Nodes shared by ** both elements will be labeled as belonging to the first element. ** ** Grid of nodes: ** ** | 2 ** | ** ** A O D O G O ** ** ** ** B O E O H O ** ** ** ** C O F O I O ---- 1 ** *PARAMETER load = -10. C10 = 80. C01 = 20. D1 = 0.0001 thick = 1.0 shape = 0.0 *DESIGN PARAMETER C10,shape *DSA CONTROLS, FORMULATION=INCREMENTAL C10,CD,1.2e-05 SHAPE,CD,1.5e-06 *NODE,NSET=A 1001, 0.0, 1.0 1011, 0.0, 1.0 1021, 0.0, 1.0 1031, 0.0, 1.0 1041, 0.0, 1.0 1051, 0.0, 1.0 1061, 0.0, 1.0 1071, 0.0, 1.0 1081, 0.0, 1.0 1091, 0.0, 1.0 1101, 0.0, 1.0 1111, 0.0, 1.0 1121, 0.0, 1.0 1131, 0.0, 1.0 1141, 0.0, 1.0 1151, 0.0, 1.0 *NODE,NSET=B 1084, 0.0, 0.5 1094, 0.0, 0.5 1104, 0.0, 0.5 1114, 0.0, 0.5 1125, 0.0, 0.5 1135, 0.0, 0.5 1145, 0.0, 0.5 1155, 0.0, 0.5 *NODE,NSET=C 1002, 0.0, 0.0 1012, 0.0, 0.0 1022, 0.0, 0.0 1032, 0.0, 0.0 1042, 0.0, 0.0 1052, 0.0, 0.0 1062, 0.0, 0.0 1072, 0.0, 0.0 1082, 0.0, 0.0 1092, 0.0, 0.0 1102, 0.0, 0.0 1112, 0.0, 0.0 1122, 0.0, 0.0 1132, 0.0, 0.0 1142, 0.0, 0.0 1152, 0.0, 0.0 *NODE,NSET=D 1024, 0.5, 1.0 1034, 0.5, 1.0 1044, 0.5, 1.0 1054, 0.5, 1.0 1064, 0.5, 1.0 1074, 0.5, 1.0 2086, 0.5, 1.0 2096, 0.5, 1.0 2106, 0.5, 1.0 2116, 0.5, 1.0 1128, 0.5, 1.0 1138, 0.5, 1.0 1148, 0.5, 1.0 1158, 0.5, 1.0 *NSET,NSET=DEQ 2086, 2096, 2106, 2116, *NODE,NSET=E 1086, 0.5, 0.5 1096, 0.5, 0.5 1106, 0.5, 0.5 1116, 0.5, 0.5 *NODE,NSET=F 1023, 0.5, 0.0 1033, 0.5, 0.0 1043, 0.5, 0.0 1053, 0.5, 0.0 1063, 0.5, 0.0 1073, 0.5, 0.0 1085, 0.5, 0.0 1095, 0.5, 0.0 1105, 0.5, 0.0 1115, 0.5, 0.0 1126, 0.5, 0.0 1136, 0.5, 0.0 1146, 0.5, 0.0 1156, 0.5, 0.0 *NODE,NSET=G 2003, 1.0, 1.0 2013, 1.0, 1.0 2024, 1.0, 1.0 2034, 1.0, 1.0 2044, 1.0, 1.0 2054, 1.0, 1.0 2064, 1.0, 1.0 2074, 1.0, 1.0 2083, 1.0, 1.0 2093, 1.0, 1.0 2103, 1.0, 1.0 2113, 1.0, 1.0 1124, 1.0, 1.0 1134, 1.0, 1.0 1144, 1.0, 1.0 1154, 1.0, 1.0 *NSET,NSET=GEQ 2083, 2093, 2103, 2113, 1124, 1134, 1144, 1154, *NODE,NSET=H 2085, 1.0, 0.5 2095, 1.0, 0.5 2105, 1.0, 0.5 2115, 1.0, 0.5 1127, 1.0, 0.5 1137, 1.0, 0.5 1147, 1.0, 0.5 1157, 1.0, 0.5 *NODE,NSET=I 1003, 1.0, 0.0 1013, 1.0, 0.0 2023, 1.0, 0.0 2033, 1.0, 0.0 2043, 1.0, 0.0 2053, 1.0, 0.0 2063, 1.0, 0.0 2073, 1.0, 0.0 1083, 1.0, 0.0 1093, 1.0, 0.0 1103, 1.0, 0.0 1113, 1.0, 0.0 1123, 1.0, 0.0 1133, 1.0, 0.0 1143, 1.0, 0.0 1153, 1.0, 0.0 *PARAMETER SHAPE VARIATION, PARAMETER=shape G, 1., 1., 0. *NSET,NSET=FIXED C, *NSET,NSET=FIXED1 A,B *NSET,NSET=FIXED2 F,I ** *NSET,NSET=OUT G, ** ** ELEMENT DEFINITIONS ** *ELEMENT,ELSET=CPE3,TYPE=CPE3 100,1001,1002,1003 200,1001,1003,2003 *ELEMENT,ELSET=CPE3H,TYPE=CPE3H 101,1011,1012,1013 201,1011,1013,2013 *ELEMENT,ELSET=CPE4,TYPE=CPE4 102,1021,1022,1023,1024 202,1024,1023,2023,2024 *ELEMENT,ELSET=CPE4H,TYPE=CPE4H 103,1031,1032,1033,1034 203,1034,1033,2033,2034 *ELEMENT,ELSET=CPE4I,TYPE=CPE4I 104,1041,1042,1043,1044 204,1044,1043,2043,2044 *ELEMENT,ELSET=CPE4IH,TYPE=CPE4IH 105,1051,1052,1053,1054 205,1054,1053,2053,2054 *ELEMENT,ELSET=CPE4R,TYPE=CPE4R 106,1061,1062,1063,1064 206,1064,1063,2063,2064 *ELEMENT,ELSET=CPE4RH,TYPE=CPE4RH 107,1071,1072,1073,1074 207,1074,1073,2073,2074 *ELEMENT,ELSET=CPE6,TYPE=CPE6 108,1081,1082,1083,1084,1085,1086 208,1081,1083,2083,1086,2085,2086 *ELEMENT,ELSET=CPE6H,TYPE=CPE6H 109,1091,1092,1093,1094,1095,1096 209,1091,1093,2093,1096,2095,2096 *ELEMENT,ELSET=CPE6M,TYPE=CPE6M 110,1101,1102,1103,1104,1105,1106 210,1101,1103,2103,1106,2105,2106 *ELEMENT,ELSET=CPE6MH,TYPE=CPE6MH 111,1111,1112,1113,1114,1115,1116 211,1111,1113,2113,1116,2115,2116 *ELEMENT,ELSET=CPE8,TYPE=CPE8 112,1121,1122,1123,1124,1125,1126,1127,1128 *ELEMENT,ELSET=CPE8H,TYPE=CPE8H 113,1131,1132,1133,1134,1135,1136,1137,1138 *ELEMENT,ELSET=CPE8R,TYPE=CPE8R 114,1141,1142,1143,1144,1145,1146,1147,1148 *ELEMENT,ELSET=CPE8RH,TYPE=CPE8RH 115,1151,1152,1153,1154,1155,1156,1157,1158 *ELSET,ELSET=ALL CPE3,CPE3H,CPE4,CPE4H,CPE4I,CPE4IH,CPE4R,CPE4RH,CPE6,CPE6H,CPE6M,CPE6MH CPE8,CPE8H,CPE8R,CPE8RH *ELSET,ELSET=LOADP3 200,201,208,209,210,211 *ELSET,ELSET=LOADP4 102,202,103,203,104,204,105,205,106,206,107,207, 112,113,114,115 ** *SOLID SECTION,ELSET=ALL,MATERIAL=MAT , ** *MATERIAL,NAME=MAT *HYPERELASTIC,N=1 ,, ** *BOUNDARY FIXED,1,2 FIXED1,1,1 FIXED2,2,2 ** ** KINEMATIC CONSTRAINTS (TO MAINTAIN UNIFORM DEFORMATION) ** *NSET,NSET=EU,UNSORTED 1086,1096,1106,1116 *NSET,NSET=DEQU,UNSORTED 2086,2096,2106,2116 *NSET,NSET=FU,UNSORTED 1023,1033,1043,1053,1063,1073,1085, 1095,1105,1115,1126,1136,1146,1156 *NSET,NSET=DU,UNSORTED 1024,1034,1044,1054,1064,1074,2086, 2096,2106,2116,1128,1138,1148,1158 *NSET,NSET=HU,UNSORTED 2085,2095,2105,2115,1127,1137,1147,1157 *NSET,NSET=GEQU,UNSORTED 2083,2093,2103,2113,1124,1134,1144,1154 *NSET,NSET=IU,UNSORTED 1003,1013,2023,2033,2043,2053,2063,2073, 1083,1093,1103,1113,1123,1133,1143,1153 *NSET,NSET=GU,UNSORTED 2003,2013,2024,2034,2044,2054,2064,2074, 2083,2093,2103,2113,1124,1134,1144,1154 *EQUATION 2 EU,1,1.,DEQU,1,-1. 2 FU,1,1.,DU,1,-1. 2 HU,1,1.,GEQU,1,-1. 2 IU,1,1.,GU,1,-1. ** *DIAGNOSTICS,NONHYBRID=WARNING *STEP,NLGEOM,DSA,UNSYMM=YES STEP 1 *STATIC 0.1, 0.4 ** *DLOAD LOADP3,P3, LOADP4,P4, ** *OUTPUT,FIELD,FREQ=0 *END STEP ** *STEP,NLGEOM,DSA,UNSYMM=YES STEP 2 *STATIC 0.1, 0.4 *OUTPUT,FIELD,FREQ=0 *END STEP ** *STEP,NLGEOM,DSA,UNSYMM=YES STEP 3 *STATIC 0.1, 0.4 *DLOAD LOADP3,P3,-20.0 LOADP4,P4,-20.0 *DESIGN RESPONSE,FREQ=2 *NODE RESPONSE,NSET=G U *ELEMENT RESPONSE S,LE,SINV,SP *END STEP *STEP,NLGEOM,PERT,DSA,UNSYMM=YES PERT STEP *STATIC *DLOAD LOADP3,P3,-10.0 LOADP4,P4,-10.0 *DESIGN RESPONSE,FREQ=2 *NODE RESPONSE,NSET=G U, *ELEMENT RESPONSE S,E,SINV,SP *END STEP