*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: 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 4: 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 5: 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,10., 1812,REB8B,10.,, *INITIAL CONDITIONS,TYPE=HARDENING,REBAR 1811,REB8A,0.2,20., 1812,REB8B,0.2,20., *ELSET,ELSET=TEST 1812,811 *ELSET,ELSET=REFER 1811,801 *SOLID SECTION,ELSET=TEST8,MATERIAL=ELAS ***************** ** TEST 6: CPE4R ******************* ** *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=CPE4R,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 7: CGAX4R ****************** ** *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=CGAX4R,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 8: CAXA41 ****************** ** *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 9: S4R WITH REBAR ************************** ** *NODE,NSET=NALL 1501, 0., 10. 1502, 1., 10. 1503, 1., 11. 1504, 0., 11. 1511, 0., 12. 1512, 1., 12. 1513, 1., 13. 1514, 0., 13. *NSET,NSET=LEFT 1501,1504,1511,1514 *NSET,NSET=BOT 1501,1502,1511,1512 *NSET,NSET=RIGHT 1502,1503,1512,1513 *ELEMENT,TYPE=S4R,ELSET=TEST15 1501,1501,1502,1503,1504 1511,1511,1512,1513,1514 *INITIAL CONDITIONS,TYPE=STRESS,REBAR 1501,REB9,10., 1511,REB9,10., ***INITIAL CONDITIONS,TYPE=HARDENING,REBAR **1501,,0.2,20., **1511,,0.2,20., *ELSET,ELSET=TEST 1511, *ELSET,ELSET=REFER 1501, *SHELL SECTION,ELSET=TEST15,MATERIAL=ELAS 1., *REBAR LAYER REB9,0.5,1.0,0,ELAS,30,1 ************************** ** TEST 10: M3D4R WITH REBAR ************************** ** *NODE,NSET=NALL 1601, 4., 10. 1602, 5., 10. 1603, 5., 11. 1604, 4., 11. 1611, 4., 12. 1612, 5., 12. 1613, 5., 13. 1614, 4., 13. *NSET,NSET=LEFT 1601,1604,1611,1614 *NSET,NSET=BOT 1601,1602,1611,1612 *NSET,NSET=RIGHT 1602,1603,1612,1613 *ELEMENT,TYPE=M3D4R,ELSET=TEST16 1601,1601,1602,1603,1604 1611,1611,1612,1613,1614 *INITIAL CONDITIONS,TYPE=STRESS,REBAR 1601,,10., 1611,,10., *INITIAL CONDITIONS,TYPE=HARDENING,REBAR 1601,,0.2,20., 1611,,0.2,20., *ELSET,ELSET=TEST 1611, *ELSET,ELSET=REFER 1601, *MEMBRANE SECTION,ELSET=TEST16,MATERIAL=ELAS 1., *REBAR LAYER REB10,0.5,1.0,0,ELAS,30,1 **************************** ** TEST 11: S4 WITH REBAR ************************** ** *NODE,NSET=NALL 1701, 0., 10. 1702, 1., 10. 1703, 1., 11. 1704, 0., 11. 1711, 0., 12. 1712, 1., 12. 1713, 1., 13. 1714, 0., 13. *NSET,NSET=LEFT 1701,1704,1711,1714 *NSET,NSET=BOT 1701,1702,1711,1712 *NSET,NSET=RIGHT 1702,1703,1712,1713 *ELEMENT,TYPE=S4,ELSET=TEST17 1701,1701,1702,1703,1704 1711,1711,1712,1713,1714 *INITIAL CONDITIONS,TYPE=STRESS,REBAR 1701,REB9,10., 1711,REB9,10., ***INITIAL CONDITIONS,TYPE=HARDENING,REBAR **1501,,0.2,20., **1511,,0.2,20., *ELSET,ELSET=TEST 1711, *ELSET,ELSET=REFER 1701, *SHELL SECTION,ELSET=TEST17,MATERIAL=ELAS 1., *REBAR LAYER REB11,0.5,1.0,0,ELAS,30,1 ** ** REMAINDER OF DECK SAME FOR ALL TESTS ** *ELSET,ELSET=EALL TEST,REFER *MATERIAL,NAME=ELAS *ELASTIC 200.E3,0.3 *PLASTIC,HARD=COMBINED,DATA TYPE=PARAMETERS 200.,2.222E4, 34.65, *CYCLIC HARDENING, PARAMETERS 200., 2000., 0.25, *DENSITY 1.E-4, *INITIAL CONDITIONS,TYPE=STRESS EALL,10., ***INITIAL CONDITIONS,TYPE=HARDENING **EALL,0.2,20., ** ** *STEP,,NLGEOM, INC=100 step #1: REMOVE TEST ELEMENTS *STATIC 0.1, 1.0 *BOUNDARY NALL,3,6 LEFT,1 BOT,2 *MODEL CHANGE,REMOVE,TYPE=ELEMENT TEST, *EL PRINT,POSITION=CENTROID,FREQ=99 1, S, E, PE, *EL PRINT,REBAR,FREQ=99 S,E,PE,RBANG,RBROT *EL FILE,REBAR,FREQ=99 S,E,PE,RBANG,RBROT *EL FILE,POSITION=CENTROID,FREQ=99 S,E,PE *NODE PRINT,NSET=LEFT,FREQ=99 RF , *NODE FILE,FREQ=99 RF, *EL FILE,REBAR S E *END STEP ** ** *STEP,NLGEOM, INC=100 STEP #2: ADD TEST ELEMENT BACK IN *STATIC .1,1. *MODEL CHANGE,ADD=STRAINFREE,TYPE=ELEMENT TEST, *BOUNDARY RIGHT,1,1,.02 *END STEP ** ** ** *STEP,NLGEOM,INC=100 STEP #3: STRETCH ELEMENTS FURTHER *STATIC 0.1,1. *BOUNDARY RIGHT,1,1,.05 *END STEP