*HEADING CONTINUUM ELEMENTS: MODEL CHANGE VERIFICATION, ELASTIC MATERIAL *RESTART,WRITE *PREPRINT,MODEL=YES,HISTORY=NO ** ** TEST 45: CPS3 ** *NODE,NSET=NALL 1001, 15.0, 0.0 1002, 16.0, 0.0 1003, 16.0, -1.0 1004, 15.0, -1.0 1005, 17.0, 0.0 1006, 17.0, -1.0 1007, 15.0, -3.0 1008, 16.5, -3.1 1009, 16.5, -4.1 1010, 15.0, -4.0 1011, 18.0, -3.2 1012, 18.0, -4.2 *NSET,NSET=LEFT 1001,1004,1007,1010 *NSET,NSET=MID 1008,1009 *NSET,NSET=RIGHT 1011,1012 *NSET,NSET=TIP 1005,1006,1011,1012 *ELEMENT,TYPE=CPS3,ELSET=TEST45 1001, 1001,1004,1002 1002, 1002,1004,1003 1003, 1002,1003,1005 1004, 1005,1003,1006 1005, 1007,1010,1008 1006, 1008,1010,1009 1007, 1008,1009,1011 1008, 1011,1009,1012 *ELSET,ELSET=REFER 1001,1002,1003,1004 *ELSET,ELSET=TEST 1005,1006,1007,1008 ** ** TEST 46: CPS6 ** *NODE,NSET=NALL 4001, 25.0, 0.0 4002, 26.0, 0.0 4003, 26.0, -1.0 4004, 25.0, -1.0 4005, 27.0, 0.0 4006, 27.0, -1.0 4007, 27.0, -0.5 4008, 25.0, -0.5 4009, 25.0, -3.0 4010, 26.5, -3.1 4011, 26.5, -4.1 4012, 25.0, -4.0 4013, 28.0, -3.2 4014, 28.0, -4.2 4015, 28.0, -3.7 4016, 25.0, -3.5 4017, 26.0, -0.5 4018, 26.5, -3.6 *NSET,NSET=LEFT 4001,4004,4008,4009,4012,4016 *NSET,NSET=MID 4010,4011,4018 *NSET,NSET=RIGHT 4013,4014,4015 *NSET,NSET=TIP 4005,4006,4007,4013,4014,4015 *ELEMENT,TYPE=CPS6,ELSET=TEST46 4001, 4001,4004,4005,4008,4017,4002 4002, 4005,4004,4006,4017,4003,4007 4003, 4009,4012,4013,4016,4018,4010 4004, 4013,4012,4014,4018,4011,4015 *ELSET,ELSET=REFER 4001,4002 *ELSET,ELSET=TEST 4003,4004 ** ** TEST 47: CPS6M ** *NODE,NSET=NALL 5001, 35.0, 0.0 5002, 36.0, 0.0 5003, 36.0, -1.0 5004, 35.0, -1.0 5005, 37.0, 0.0 5006, 37.0, -1.0 5007, 37.0, -0.5 5008, 35.0, -0.5 5009, 35.0, -3.0 5010, 36.5, -3.1 5011, 36.5, -4.1 5012, 35.0, -4.0 5013, 38.0, -3.2 5014, 38.0, -4.2 5015, 38.0, -3.7 5016, 35.0, -3.5 5017, 36.0, -0.5 5018, 36.5, -3.6 *NSET,NSET=LEFT 5001,5004,5008,5009,5012,5016 *NSET,NSET=MID 5010,5011,5018 *NSET,NSET=RIGHT 5013,5014,5015 *NSET,NSET=TIP 5005,5006,5007,5013,5014,5015 *ELEMENT,TYPE=CPS6M,ELSET=TEST47 5001, 5001,5004,5005,5008,5017,5002 5002, 5005,5004,5006,5017,5003,5007 5003, 5009,5012,5013,5016,5018,5010 5004, 5013,5012,5014,5018,5011,5015 *ELSET,ELSET=REFER 5001,5002 *ELSET,ELSET=TEST 5003,5004 ** ** REMAINDER OF INPUT DECK SAME FOR ALL TESTS ** *ELSET,ELSET=EALL TEST,REFER *SOLID SECTION,MATERIAL=ELAS,ELSET=EALL 1.0, *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 LEFT,1,2 RIGHT,1,1,-1.0 RIGHT,2,2, 0.2 MID,1,1,-0.5 MID,2,2, 0.1 *NODE PRINT,FREQ=999 RF, *EL PRINT,FREQ=999 S,E *OUTPUT,FIELD,FREQ=999 *ELEMENT OUTPUT S, *OUTPUT,FIELD,FREQ=999 *NODE OUTPUT RF, *ELEMENT OUTPUT,POSITION=CENTROID E, S, MISESONLY,PRESSONLY *OUTPUT,HISTORY,FREQ=999 *NODE OUTPUT, NSET=NALL RF, *END STEP ** ** *STEP STEP #2: REMOVE TEST ELEMENTS *STATIC 1.,1. *MODEL CHANGE,REMOVE,TYPE=ELEMENT TEST, *END STEP ** ** *STEP STEP #3: ADD TEST ELEMENTS BACK IN STRAIN-FREE *STATIC 1.,1. *MODEL CHANGE,ADD=STRAINFREE,TYPE=ELEMENT TEST, *BOUNDARY,OP=NEW LEFT,1,2 *END STEP ** ** *STEP STEP #4: APPLY LOAD TO BOTH ELEMENTS *STATIC 0.1,1. *DLOAD TEST,P3,-0.25 REFER,P3,-0.25 *END STEP ** ** *STEP STEP #5: REMOVE TEST ELEMENT *STATIC .1,1.0 *MODEL CHANGE,REMOVE,TYPE=ELEMENT TEST, *END STEP ** ** *STEP STEP #6: ADD TEST ELEMENTS BACK IN WITH-STRAIN *STATIC .1,1.0 *MODEL CHANGE,ADD=WITHSTRAIN,TYPE=ELEMENT TEST, *END STEP ** ** *STEP STEP #7: APPLY THERMAL LOAD *STATIC .1,1.0 *BOUNDARY,OP=NEW,FIXED TIP,1 LEFT,1,2 *TEMPERATURE NALL,100. *EL PRINT,FREQ=999 S,THE,TEMP *OUTPUT,FIELD,FREQ=999 *ELEMENT OUTPUT S,THE,TEMP *END STEP ** ** *STEP STEP #8: FREQUENCY EXTRACTION *FREQUENCY, eigensolver=lanczos, SIM=NO 32, , *BOUNDARY,OP=NEW LEFT,1,2 *EL PRINT,FREQ=0 *NODE PRINT,FREQ=0 *OUTPUT,FIELD,FREQ=0 *END STEP ** ** *STEP,PERTURBATION STEP #9: MODAL DYNAMIC *MODAL DYNAMIC .0004,.004 *CLOAD TIP,2,0.2 *NODE PRINT,FREQ=999 RF, *EL PRINT,FREQ=999 S,E *OUTPUT,FIELD,FREQ=999 *NODE OUTPUT RF, *OUTPUT,HISTORY,FREQ=999 *NODE OUTPUT, NSET=NALL RF, *OUTPUT,FIELD,FREQ=999 *ELEMENT OUTPUT S, *OUTPUT,FIELD,FREQ=999 *ELEMENT OUTPUT,POSITION=CENTROID E, S, MISESONLY,PRESSONLY *END STEP ** ** *STEP,PERTURBATION STEP #10: STEADY-STATE DYNAMICS, MODAL BASED *STEADY STATE DYNAMICS,INTERVAL=RANGE 1000., 10000., 5 *CLOAD TIP,2,0.2 *NODE PRINT,FREQ=999 RF, *EL PRINT,FREQ=999 S,E *OUTPUT,FIELD,FREQ=999 *NODE OUTPUT RF, *END STEP ** ** *STEP STEP #11: FREQUENCY EXTRACTION FOR SUBSPACE PROJECTION *FREQUENCY, eigensolver=lanczos, SIM=NO 124, , *BOUNDARY,OP=NEW LEFT,1,2 *EL PRINT,FREQ=0 *NODE PRINT,FREQ=0 *OUTPUT,FIELD,FREQ=0 *END STEP ** ** *STEP,PERTURBATION STEP #12: STEADY-STATE DYNAMICS, DIRECT *STEADY STATE DYNAMICS,DIRECT 1000., 10000., 5 *BOUNDARY,OP=NEW LEFT,1,2 *CLOAD TIP,2,0.2 *NODE PRINT,FREQ=999 RF, *EL PRINT,FREQ=999 S,E *OUTPUT,FIELD,FREQ=999 *NODE OUTPUT RF, *OUTPUT,HISTORY,FREQ=999 *NODE OUTPUT,NSET=NALL RF, *OUTPUT,FIELD, FREQ=0 *ELEMENT OUTPUT,POSITION=CENTROID *END STEP ** ** *STEP,PERTURBATION STEP #13: STEADY-STATE DYNAMICS,SUBSPACE PROJECTION *STEADY STATE DYNAMICS,SUBSPACE PROJECTION,INTERVAL=RANGE 1000., 10000., 5 *CLOAD TIP,2,0.2 *NODE PRINT,FREQ=999 RF, *EL PRINT,FREQ=999 S,E *OUTPUT,FIELD,FREQ=999 *NODE OUTPUT RF, *OUTPUT,HISTORY,FREQ=999 *NODE OUTPUT,NSET=NALL RF, *OUTPUT,FIELD, FREQ=0 *ELEMENT OUTPUT,POSITION=CENTROID *END STEP ** ** *STEP STEP #14: DYNAMICS *DYNAMIC .0004, .004 *BOUNDARY,OP=NEW LEFT,1,2 *EL PRINT,FREQ=999 S,E *NODE PRINT,FREQ=999 RF, *CLOAD,AMP=RAMP TIP,2,0.2 *END STEP