*HEADING AXISYMMETRIC MEMBRANE ELEMENTS: MODEL CHANGE VERIFICATION *PREPRINT,MODEL=YES,HISTORY=NO ***************** ** TEST 1: MAX1 ***************** *NODE,NSET=NALL 1, 1.0, 1. 2, 1.5, 2. 3, 2.0, 3. 11, 1.0, 5. 12, 2.0, 6. 13, 3.0, 7. *NSET,NSET=BOT 1,11 *NSET,NSET=MID 12, *NSET,NSET=TOP1 13, *NSET,NSET=TOP 3,13 *ELEMENT,TYPE=MAX1,ELSET=EALL 1, 1,2 2, 2,3 11, 11,12 12, 12,13 *ELSET,ELSET=REFER 1,2 *ELSET,ELSET=TEST 11,12 *ELSET,ELSET=EOUT 1,11 *ELSET,ELSET=EALL1 1,2,11,12 *MEMBRANE SECTION,MATERIAL=ELAS,ELSET=EALL1 .25, ***************** ** TEST 2: MAX2 ***************** *NODE,NSET=NALL 101, 6.0, 1. 102, 6.5, 2. 103, 7.0, 3. 111, 6.0, 5. 112, 7.0, 6. 113, 8.0, 7. *NSET,NSET=BOT 101,111, *NSET,NSET=MID 112, *NSET,NSET=TOP1 113, *NSET,NSET=TOP 103,113 *ELEMENT,TYPE=MAX2,ELSET=EALL 101, 101,102,103 111, 111,112,113 *ELSET,ELSET=REFER 101, *ELSET,ELSET=TEST 111, *ELSET,ELSET=EOUT 101,111 *ELSET,ELSET=EALL2 101,111 *MEMBRANE SECTION,MATERIAL=ELAS,ELSET=EALL2 .25, ****************** ** TEST 3: MGAX1 ****************** *NODE,NSET=NALL 201, 11.0, 1. 202, 11.5, 2. 203, 12.0, 3. 211, 11.0, 5. 212, 12.0, 6. 213, 13.0, 7. *NSET,NSET=BOT 201,211, *NSET,NSET=MID 212, *NSET,NSET=TOP1 213, *NSET,NSET=TOP 203,213 *ELEMENT,TYPE=MGAX1,ELSET=EALL 201, 201,202 202, 202,203 211, 211,212 212, 212,213 *ELSET,ELSET=REFER 201,202 *ELSET,ELSET=TEST 211,212 *ELSET,ELSET=EOUT 201,211 *ELSET,ELSET=EALL3 201,202,211,212 *MEMBRANE SECTION,MATERIAL=ELAS,ELSET=EALL3 .25, ****************** ** TEST 4: MGAX2 ****************** *NODE,NSET=NALL 301, 16.0, 1. 302, 16.5, 2. 303, 17.0, 3. 311, 16.0, 5. 312, 17.0, 6. 313, 18.0, 7. *NSET,NSET=BOT 301,311, *NSET,NSET=MID 312, *NSET,NSET=TOP1 313, *NSET,NSET=TOP 303,313 *ELEMENT,TYPE=MGAX2,ELSET=EALL 301, 301,302,303 311, 311,312,313 *ELSET,ELSET=REFER 301, *ELSET,ELSET=TEST 311, *ELSET,ELSET=EOUT 301,311 *ELSET,ELSET=EALL4 301,311 *MEMBRANE SECTION,MATERIAL=ELAS,ELSET=EALL4 .25, **************************** ** TEST 5: MAX1 WITH REBAR **************************** *NODE,NSET=NALL 401, 1.0, 10. 402, 1.5, 11. 403, 2.0, 12. 411, 1.0, 14. 412, 2.0, 15. 413, 3.0, 16. *NSET,NSET=BOT 401,411, *NSET,NSET=MID 412, *NSET,NSET=TOP1 413, *NSET,NSET=TOP 403,413 *ELEMENT,TYPE=MAX1,ELSET=EALL 401, 401,402 402, 402,403 411, 411,412 412, 412,413 *ELSET,ELSET=REFER 401,402 *ELSET,ELSET=TEST 411,412 *ELSET,ELSET=EOUT 401,411 *ELSET,ELSET=EALL5 401,402,411,412 *MEMBRANE SECTION,MATERIAL=ELAS,ELSET=EALL5 .25, *REBAR LAYER,GEOMETRY=ANGULAR REB5,0.1,180,0,ELAS,30,1 **************************** ** TEST 6: MAX2 WITH REBAR **************************** *NODE,NSET=NALL 501, 6.0, 10. 502, 6.5, 11. 503, 7.0, 12. 511, 6.0, 14. 512, 7.0, 15. 513, 8.0, 16. *NSET,NSET=BOT 501,511, *NSET,NSET=MID 512, *NSET,NSET=TOP1 513, *NSET,NSET=TOP 503,513 *ELEMENT,TYPE=MAX2,ELSET=EALL 501, 501,502,503 511, 511,512,513 *ELSET,ELSET=REFER 501, *ELSET,ELSET=TEST 511, *ELSET,ELSET=EOUT 501,511 *ELSET,ELSET=EALL6 501,511 *MEMBRANE SECTION,MATERIAL=ELAS,ELSET=EALL6 .25, *REBAR LAYER,GEOMETRY=ANGULAR REB6,0.1,19.2,0,ELAS,30,1 ***************************** ** TEST 7: MGAX1 WITH REBAR ***************************** *NODE,NSET=NALL 601, 11.0, 10. 602, 11.5, 11. 603, 12.0, 12. 611, 11.0, 14. 612, 12.0, 15. 613, 13.0, 16. *NSET,NSET=BOT 601,611, *NSET,NSET=MID 612, *NSET,NSET=TOP1 613, *NSET,NSET=TOP 603,613 *ELEMENT,TYPE=MGAX1,ELSET=EALL 601, 601,602 602, 602,603 611, 611,612 612, 612,613 *ELSET,ELSET=REFER 601,602 *ELSET,ELSET=TEST 611,612 *ELSET,ELSET=EOUT 601,611 *ELSET,ELSET=EALL7 601,602,611,612 *MEMBRANE SECTION,MATERIAL=ELAS,ELSET=EALL7 .25, *REBAR LAYER,GEOMETRY=ANGULAR REB7,0.1,10.43,0,ELAS,30,1 ***************************** ** TEST 8: MGAX2 WITH REBAR ***************************** *NODE,NSET=NALL 701, 16.0, 10. 702, 16.5, 11. 703, 17.0, 12. 711, 16.0, 14. 712, 17.0, 15. 713, 18.0, 16. *NSET,NSET=BOT 701,711, *NSET,NSET=MID 712, *NSET,NSET=TOP1 713, *NSET,NSET=TOP 703,713 *ELEMENT,TYPE=MGAX2,ELSET=EALL 701, 701,702,703 711, 711,712,713 *ELSET,ELSET=REFER 701, *ELSET,ELSET=TEST 711, *ELSET,ELSET=EOUT 701,711 *ELSET,ELSET=EALL8 701,711 *MEMBRANE SECTION,MATERIAL=ELAS,ELSET=EALL8 .25, *REBAR LAYER,GEOMETRY=ANGULAR REB8,0.1,7.17,0,ELAS,30,1 ************************************************ ** REMAINDER OF INPUT DECK SAME FOR ALL TESTS ************************************************ *ELSET,ELSET=EALL TEST,REFER *MATERIAL,NAME=ELAS *ELASTIC 1000., .25 *EXPANSION 1.E-3, *DENSITY 1.E-3, *INITIAL CONDITIONS,TYPE=TEMPERATURE NALL,70. *AMPLITUDE,NAME=RAMP 0.,0.,1.,1. ** ** *STEP,NLGEOM STEP #1: DISPLACE TEST SPECIMEN SO FINAL SHAPE IS IDENTICAL TO INITIAL SHAPE OF REFERENCE ELEMENT *STATIC 0.25,1. *PRINT,MODEL CHANGE=YES *BOUNDARY,OP=NEW NALL,2 NALL,5 BOT,1 MID,1,1,-.5 TOP1,1,1,-1. *NODE PRINT,NSET=BOT,FREQ=999 RF, *EL PRINT,ELSET=EOUT,POSITION=CENTROID,FREQ=999 S,E *EL PRINT,ELSET=EOUT,REBAR,FREQ=99 S,E,IVOL,RBANG,RBROT *EL FILE,ELSET=EOUT,REBAR,FREQ=99 S,E,IVOL,RBANG,RBROT *NODE FILE,NSET=BOT,FREQ=999 RF, *EL FILE,ELSET=EOUT,POSITION=CENTROID,FREQ=999 E, S *END STEP ** ** *STEP,NLGEOM STEP #2: REMOVE TEST ELEMENTS *STATIC 1.,1. *MODEL CHANGE,REMOVE,TYPE=ELEMENT TEST, *END STEP ** ** *STEP,NLGEOM STEP #3: ADD TEST ELEMENTS BACK IN STRAIN-FREE *STATIC 1.,1. *MODEL CHANGE,ADD=STRAINFREE,TYPE=ELEMENT TEST, *BOUNDARY,OP=NEW BOT,2 BOT,5 TOP,2 *END STEP ** ** *STEP,NLGEOM,INC=100 STEP #4: BOUNDARY DISPLACEMENT *STATIC 0.025,1. *BOUNDARY,TYPE=VELOCITY NALL,1,1,.05 *END STEP ** ** *STEP,NLGEOM STEP #5: FREEZE BOUNDARY DISPLACEMENT *STATIC .25,1.0 *BOUNDARY,OP=NEW,FIXED NALL,1 BOT,2 BOT,5 TOP,2 *END STEP ** ** *STEP,NLGEOM STEP #5: REMOVE TEST ELEMENTS *STATIC .25,1.0 *MODEL CHANGE,REMOVE,TYPE=ELEMENT TEST, *END STEP ** ** *STEP,NLGEOM,INC=100 STEP #6: ADD TEST ELEMENTS BACK IN WITH-STRAIN *STATIC .025,1.0 *MODEL CHANGE,ADD=WITHSTRAIN,TYPE=ELEMENT TEST, *END STEP ** ** *STEP,NLGEOM STEP #7: APPLY THERMAL LOAD *STATIC .25,1.0 *TEMPERATURE NALL,100. *NODE PRINT,FREQ=0 *EL PRINT,ELSET=EOUT,POSITION=CENTROID,FREQ=999 S,THE, E,TEMP *EL PRINT,ELSET=EOUT,REBAR,FREQ=99 1, S,E,THE,RBANG,RBROT *EL FILE,ELSET=EOUT,POSITION=CENTROID,FREQ=999 S,THE,E,TEMP *EL FILE,REBAR,FREQ=99 1, S,E,RBANG,RBROT *END STEP