*HEADING *PREPRINT,MODEL=NO,HISTORY=NO ***************** ** TEST 1: CAX4 ***************** *NODE,NSET=NALL 1, 1., 0. 2, 2., 0. 3, 2., 1. 4, 1., 1. 11, 1., 2. 12, 2., 2. 13, 2., 3. 14, 1., 3. *NSET,NSET=LEFT 1,4,11,14 *NSET,NSET=BOT 1,2,11,12 *NSET,NSET=RIGHT 2,3,12,13 *ELEMENT,TYPE=CAX4,ELSET=TEST1 1,1,2,3,4 11,11,12,13,14 *ELSET,ELSET=TEST 11, *ELSET,ELSET=REFER 1, *SOLID SECTION,ELSET=TEST1,MATERIAL=ELAS ***************** ** TEST 2: CPE4 ******************* ** *NODE,NSET=NALL 101, 4., 0. 102, 5., 0. 103, 5., 1. 104, 4., 1. 111, 4., 2. 112, 5., 2. 113, 5., 3. 114, 4., 3. *NSET,NSET=LEFT 101,104,111,114 *NSET,NSET=BOT 101,102,111,112 *NSET,NSET=RIGHT 102,103,112,113 *ELEMENT,TYPE=CPE4,ELSET=TEST2 101,101,102,103,104 111,111,112,113,114 *ELSET,ELSET=TEST 111, *ELSET,ELSET=REFER 101, *SOLID SECTION,ELSET=TEST2,MATERIAL=ELAS ***************** ** TEST 3: CPS4 ******************* ** *NODE,NSET=NALL 301, 7., 0. 302, 8., 0. 303, 8., 1. 304, 7., 1. 311, 7., 2. 312, 8., 2. 313, 8., 3. 314, 7., 3. *NSET,NSET=LEFT 301,304,311,314 *NSET,NSET=BOT 301,302,311,312 *NSET,NSET=RIGHT 302,303,312,313 *ELEMENT,TYPE=CPS4,ELSET=TEST3 301,301,302,303,304 311,311,312,313,314 *ELSET,ELSET=TEST 311, *ELSET,ELSET=REFER 301, *SOLID SECTION,ELSET=TEST3,MATERIAL=ELAS ****************** ** TEST 4: CGAX4 ****************** ** *NODE,NSET=NALL 401, 10., 0. 402, 11., 0. 403, 11., 1. 404, 10., 1. 411, 10., 2. 412, 11., 2. 413, 11., 3. 414, 10., 3. *NSET,NSET=LEFT 401,404,411,414 *NSET,NSET=BOT 401,402,411,412 *NSET,NSET=RIGHT 402,403,412,413 *ELEMENT,TYPE=CGAX4,ELSET=TEST4 401,401,402,403,404 411,411,412,413,414 *ELSET,ELSET=TEST 411, *ELSET,ELSET=REFER 401, *SOLID SECTION,ELSET=TEST4,MATERIAL=ELAS ****************** ** TEST 5: M3D4 ****************** ** *NODE,NSET=NALL 501, 13., 0. 502, 14., 0. 503, 14., 1. 504, 13., 1. 511, 13., 2. 512, 14., 2. 513, 14., 3. 514, 13., 3. *NSET,NSET=LEFT 501,504,511,514 *NSET,NSET=BOT 501,502,511,512 *NSET,NSET=RIGHT 502,503,512,513 *ELEMENT,TYPE=M3D4,ELSET=TEST5 501,501,502,503,504 511,511,512,513,514 *ELSET,ELSET=TEST 511, *ELSET,ELSET=REFER 501, *MEMBRANE SECTION,ELSET=TEST5,MATERIAL=ELAS .25, ****************** ** TEST 6: S4R ****************** ** *NODE,NSET=NALL 601, 16., 0. 602, 17., 0. 603, 17., 1. 604, 16., 1. 611, 16., 2. 612, 17., 2. 613, 17., 3. 614, 16., 3. *NSET,NSET=LEFT 601,604,611,614 *NSET,NSET=BOT 601,602,611,612 *NSET,NSET=RIGHT 602,603,612,613 *ELEMENT,TYPE=S4R,ELSET=TEST6 601,601,602,603,604 611,611,612,613,614 *ELSET,ELSET=TEST 611, *ELSET,ELSET=REFER 601, *SHELL SECTION,ELSET=TEST6,MATERIAL=ELAS .25, ******************* ** TEST 7: CAXA ****************** ** *NODE,NSET=NALL 701, 19., 0. 702, 20., 0. 703, 20., 1. 704, 19., 1. 711, 19., 2. 712, 20., 2. 713, 20., 3. 714, 19., 3. *NSET,NSET=LEFT 701,704,711,714 10701,10704,10711,10714 *NSET,NSET=BOT 701,702,711,712 10701,10702,10711,10712 *NSET,NSET=RIGHT 702,703,712,713 10702,10703,10712,10713 *ELEMENT,TYPE=CAXA41,ELSET=TEST7,OFFSET=10000 701,701,702,703,704 711,711,712,713,714 *ELSET,ELSET=TEST 711, *ELSET,ELSET=REFER 701, *SOLID SECTION,ELSET=TEST7,MATERIAL=ELAS *************************** ** TEST 8: CAX4 WITH REBAR *************************** *NODE,NSET=NALL 801, 1., 5. 802, 2., 5. 803, 2., 6. 804, 1., 6. 811, 1., 7. 812, 2., 7. 813, 2., 8. 814, 1., 8. 1814, 1.3, 5. 1815, 2., 5.2 1816, 1.3, 7. 1817, 2., 7.2 *ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-1 1811,1814,1815 *SURFACE SECTION,ELSET=SFMAX1-1 *REBAR LAYER,GEOMETRY=ANGULAR REB8A,1.000000,19.188136,0.000000,ELAS,10.000000,1 *EMBEDDED ELEMENT 1811, *ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-2 1812,1816,1817 *SURFACE SECTION,ELSET=SFMAX1-2 *REBAR LAYER,GEOMETRY=ANGULAR REB8B,1.000000,19.188136,0.000000,ELAS,10.000000,1 *EMBEDDED ELEMENT 1812, *NSET,NSET=LEFT 801,804,811,814 *NSET,NSET=BOT 801,802,811,812 *NSET,NSET=RIGHT 802,803,812,813 *ELEMENT,TYPE=CAX4,ELSET=TEST8 801, 801,802,803,804 811, 811,812,813,814 *INITIAL CONDITIONS,TYPE=STRESS,REBAR 1811, REB8A, 60. 1812, REB8B, 60. *ELSET,ELSET=TEST 1812,811 *ELSET,ELSET=REFER 1811,801 *SOLID SECTION,ELSET=TEST8,MATERIAL=ELAS ***************** ** TEST 9: CPE4 ******************* ** *NODE,NSET=NALL 901, 4., 5. 902, 5., 5. 903, 5., 6. 904, 4., 6. 911, 4., 7. 912, 5., 7. 913, 5., 8. 914, 4., 8. *NSET,NSET=LEFT 901,904,911,914 *NSET,NSET=BOT 901,902,911,912 *NSET,NSET=RIGHT 902,903,912,913 *ELEMENT,TYPE=CPE4,ELSET=TEST9 901,901,902,903,904 911,911,912,913,914 *ELSET,ELSET=TEST 911, *ELSET,ELSET=REFER 901, *SOLID SECTION,ELSET=TEST9,MATERIAL=ELAS ***************** ** TEST 10: CPS4 ******************* ** *NODE,NSET=NALL 1001, 7., 5. 1002, 8., 5. 1003, 8., 6. 1004, 7., 6. 1011, 7., 7. 1012, 8., 7. 1013, 8., 8. 1014, 7., 8. *NSET,NSET=LEFT 1001,1004,1011,1014 *NSET,NSET=BOT 1001,1002,1011,1012 *NSET,NSET=RIGHT 1002,1003,1012,1013 *ELEMENT,TYPE=CPE4,ELSET=TEST10 1001,1001,1002,1003,1004 1011,1011,1012,1013,1014 *ELSET,ELSET=TEST 1011, *ELSET,ELSET=REFER 1001, *SOLID SECTION,ELSET=TEST10,MATERIAL=ELAS ****************** ** TEST 11: CGAX4 ****************** ** *NODE,NSET=NALL 1101, 10., 5. 1102, 11., 5. 1103, 11., 6. 1104, 10., 6. 1111, 10., 7. 1112, 11., 7. 1113, 11., 8. 1114, 10., 8. *NSET,NSET=LEFT 1101,1104,1111,1114 *NSET,NSET=BOT 1101,1102,1111,1112 *NSET,NSET=RIGHT 1102,1103,1112,1113 *ELEMENT,TYPE=CGAX4,ELSET=TEST11 1101,1101,1102,1103,1104 1111,1111,1112,1113,1114 *ELSET,ELSET=TEST 1111, *ELSET,ELSET=REFER 1101, *SOLID SECTION,ELSET=TEST11,MATERIAL=ELAS *************************** ** TEST 12: M3D4 WITH REBAR *************************** ** *NODE,NSET=NALL 1201, 13., 5. 1202, 14., 5. 1203, 14., 6. 1204, 13., 6. 1211, 13., 7. 1212, 14., 7. 1213, 14., 8. 1214, 13., 8. *NODAL THICKNESS 1201, .125 1202, .175 1203, .175 1204, .125 1211, .125 1212, .175 1213, .175 1214, .125 *NSET,NSET=LEFT 1201,1204,1211,1214 *NSET,NSET=BOT 1201,1202,1211,1212 *NSET,NSET=RIGHT 1202,1203,1212,1213 *ELEMENT,TYPE=M3D4,ELSET=TEST12 1201,1201,1202,1203,1204 1211,1211,1212,1213,1214 *INITIAL CONDITIONS,TYPE=STRESS,REBAR 1201, REB12, 60. 1211, REB12, 60. *ELSET,ELSET=TEST 1211, *ELSET,ELSET=REFER 1201, *MEMBRANE SECTION,ELSET=TEST12,MATERIAL=ELAS,NODAL THICKNESS .25, *REBAR LAYER REB12,1,0.5,0,ELAS,30,1 ************************** ** TEST 13: S4R WITH REBAR ************************** ** *NODE,NSET=NALL 1301, 16., 5. 1302, 17., 5. 1303, 17., 6. 1304, 16., 6. 1311, 16., 7. 1312, 17., 7. 1313, 17., 8. 1314, 16., 8. 11314, 16.3, 5. 11315, 17., 5.2 11316, 16.3, 7. 11317, 17., 7.2 **ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-1 **11311,11314,11315 **SURFACE SECTION,ELSET=SFMAX1-1 **REBAR LAYER,GEOMETRY=ANGULAR **REB9,1.000000,19.188136,0.000000,ELAS,10.000000,1 **EMBEDDED ELEMENT **11311, **ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-1 **11312,11316,11317 **SURFACE SECTION,ELSET=SFMAX1-1 **REBAR LAYER,GEOMETRY=ANGULAR **REB8,1.000000,19.188136,0.000000,ELAS,10.000000,1 ***EMBEDDED ELEMENT **1812, *NSET,NSET=LEFT 1301,1304,1311,1314 *NSET,NSET=BOT 1301,1302,1311,1312 *NSET,NSET=RIGHT 1302,1303,1312,1313 *ELEMENT,TYPE=S4R,ELSET=TEST13 1301,1301,1302,1303,1304 1311,1311,1312,1313,1314 *INITIAL CONDITIONS,TYPE=STRESS,REBAR 1301, REB13, 60. 1311, REB13, 60. *ELSET,ELSET=TEST 1301, *ELSET,ELSET=REFER 1311, *SHELL SECTION,ELSET=TEST13,MATERIAL=ELAS .25, *REBAR LAYER REB13,1,0.5,0,ELAS,30,1 ******************* ** TEST 14: CAXA ****************** ** *NODE,NSET=NALL 1401, 19., 5. 1402, 20., 5. 1403, 20., 6. 1404, 19., 6. 1411, 19., 7. 1412, 20., 7. 1413, 20., 8. 1414, 19., 8. *NSET,NSET=LEFT 1401,1404,1411,1414 11401,11404,11411,11414 *NSET,NSET=BOT 1401,1402,1411,1412 11401,11402,11411,11412 *NSET,NSET=RIGHT 1402,1403,1412,1413 11402,11403,11412,11413 *ELEMENT,TYPE=CAXA41,ELSET=TEST14,OFFSET=10000 1401,1401,1402,1403,1404 1411,1411,1412,1413,1414 *ELSET,ELSET=TEST 1411, *ELSET,ELSET=REFER 1401, *SOLID SECTION,ELSET=TEST14,MATERIAL=ELAS ************************** ** TEST 15: S4 WITH REBAR ************************** ** *NODE,NSET=NALL 1501, 16., 5. 1502, 17., 5. 1503, 17., 6. 1504, 16., 6. 1511, 16., 7. 1512, 17., 7. 1513, 17., 8. 1514, 16., 8. *NSET,NSET=LEFT 1501,1504,1511,1514 *NSET,NSET=BOT 1501,1502,1511,1512 *NSET,NSET=RIGHT 1502,1503,1512,1513 *ELEMENT,TYPE=S4,ELSET=TEST15 1501,1501,1502,1503,1504 1511,1511,1512,1513,1514 *INITIAL CONDITIONS,TYPE=STRESS,REBAR 1501, REB13, 60. 1511, REB13, 60. *ELSET,ELSET=TEST 1511, *ELSET,ELSET=REFER 1501, *SHELL SECTION,ELSET=TEST15,MATERIAL=ELAS .25, *REBAR LAYER REB15,1,0.5,0,ELAS,30,1 ** ** ** ** REMAINDER OF DECK SAME FOR ALL TESTS ** *ELSET,ELSET=EALL TEST,REFER *INITIAL CONDITIONS,TYPE=STRESS EALL,-100., .0, 0., *MATERIAL,NAME=ELAS *ELASTIC 2000., .3 *DENSITY 1.E-4, ** ** *STEP,,NLGEOM step #1: REMOVE TEST ELEMENT *STATIC 0.1, 1.0 *BOUNDARY NALL,3,6 LEFT,1 BOT,2 RIGHT,1 *MODEL CHANGE,REMOVE,TYPE=ELEMENT TEST, *EL PRINT,POSITION=CENTROID,FREQ=99 1, S, E, *OUTPUT,FIELD,FREQ=99 *ELEMENT OUTPUT S,E *ELEMENT OUTPUT,ELSET=TEST12,REBAR S,E *NODE OUTPUT RF , *NODE PRINT,FREQ=99 RF , *EL FILE,REBAR S, E *END STEP ** ** *STEP,NLGEOM STEP #2: ADD TEST ELEMENTS BACK IN STRAIN-FREE *STATIC 1.,1. *MODEL CHANGE,ADD=STRAINFREE,TYPE=ELEMENT TEST, *BOUNDARY,OP=NEW NALL,3,6 LEFT,1 BOT,2 RIGHT,1 *OUTPUT,FIELD,FREQ=99 *ELEMENT OUTPUT S,E *ELEMENT OUTPUT,ELSET=TEST12,REBAR S,E *END STEP ** ** *STEP,NLGEOM STEP #3: STRETCH ELEMENT *STATIC 1.,1. *BOUNDARY RIGHT,1,1,.1 *OUTPUT,FIELD,FREQ=99 *ELEMENT OUTPUT S,E *ELEMENT OUTPUT,ELSET=TEST12,REBAR S,E *END STEP