*HEADING BEAM ELEMENTS: MODEL CHANGE VERIFICATION, ELASTIC MATERIAL *PREPRINT,MODEL=YES,HISTORY=NO ** ** TEST 1: PIPE31 ** *NODE,NSET=NALL 1, 20.,10. 2, 25.,15. 3, 30.,20. 11,40.,10., 0. 12,40.,15., 1. 13,40.,20., 2. *NSET,NSET=LEFT 1,11 *NSET,NSET=RLEFT 1, *NSET,NSET=TLEFT 11, *NSET,NSET=MID 12, *NSET,NSET=RIGHT 13, *NSET,NSET=TIP 3,13 *ELEMENT,TYPE=PIPE31,ELSET=TEST1 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 ** ** TEST 2: PIPE32 ** *NODE,NSET=NALL 101, 60.,10. 102, 65.,15. 103, 70.,20. 111, 80.,10., 0. 112, 80.,15., 1. 113, 80.,20., 2. *NSET,NSET=LEFT 101,111 *NSET,NSET=RLEFT 101, *NSET,NSET=TLEFT 111, *NSET,NSET=MID 112, *NSET,NSET=RIGHT 113, *NSET,NSET=TIP 103,113 *ELEMENT,TYPE=PIPE32,ELSET=TEST2 101,101,102,103 111,111,112,113 *ELSET,ELSET=REFER 101,102 *ELSET,ELSET=TEST 111,112 *ELSET,ELSET=EOUT 101,111 ** ** TEST 3: PIPE31H ** *NODE,NSET=NALL 201, 100.,10. 202, 105.,15. 203, 110.,20. 211, 120.,10., 0. 212, 120.,15., 1. 213, 120.,20., 2. *NSET,NSET=LEFT 201,211 *NSET,NSET=RLEFT 201, *NSET,NSET=TLEFT 211, *NSET,NSET=MID 212, *NSET,NSET=RIGHT 213, *NSET,NSET=TIP 203,213 *ELEMENT,TYPE=PIPE31H,ELSET=TEST3 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 ** ** TEST 4: PIPE32H ** *NODE,NSET=NALL 301, 140.,10. 302, 145.,15. 303, 150.,20. 311, 160.,10., 0. 312, 160.,15., 1. 313, 160.,20., 2. *NSET,NSET=LEFT 301,311 *NSET,NSET=RLEFT 301, *NSET,NSET=TLEFT 311, *NSET,NSET=MID 312, *NSET,NSET=RIGHT 313, *NSET,NSET=TIP 303,313 *ELEMENT,TYPE=PIPE32H,ELSET=TEST4 301, 301,302,303 311, 311,312,313 *ELSET,ELSET=REFER 301,302 *ELSET,ELSET=TEST 311,312 *ELSET,ELSET=EOUT 301,311 ** ** REMAINDER OF INPUT DECK SAME FOR ALL TESTS ** *ELSET,ELSET=EALL TEST,REFER *BEAM SECTION,SECTION=PIPE,TEMPERATURE=GRADIENTS,MATERIAL=ELAS,ELSET=EALL 1.0,.05 0.,0.,-1. *NORMAL TEST,LEFT, -1., 0.,0. TEST,MID, -1., 0.,0. TEST,RIGHT,-1., 0.,0. *AMPLITUDE, NAME=RAMP 0.,0., .004,1. *MATERIAL,NAME=ELAS *ELASTIC 1000., .3 *EXPANSION 1.E-8, *DENSITY 2.0, *INITIAL CONDITIONS,TYPE=TEMPERATURE NALL,70.,0. ** ** *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,1,5 RLEFT,6 TLEFT,6,6,-.78539816 RIGHT,1,1,10.0 RIGHT,2,2, 0.0 RIGHT,3,3,-2.0 RIGHT,4,5,0.0 RIGHT,6,6,-.78539816 MID,1,1,5.0 MID,2,2,0.0 MID,3,3,-1.0 MID,4,5,0.0 MID,6,6,-.78539816 *NODE PRINT,FREQ=999 RF, *EL PRINT,ELSET=EOUT,POSITION=CENTROID,FREQ=999 1, 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,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,TYPE=VELOCITY LEFT,1,6 *END STEP ** ** *STEP,NLGEOM,INC=11 STEP #4: APPLY LOAD TO BOTH ELEMENTS *STATIC 0.25,1. *DLOAD TEST,GRAV,15.,0.,1.,0. REFER,GRAV,15.,0.,1.,0. *END STEP ** ** *STEP,NLGEOM STEP #5: REMOVE TEST ELEMENT *STATIC .25,1.0 *MODEL CHANGE,REMOVE,TYPE=ELEMENT TEST, *END STEP ** ** *STEP,NLGEOM STEP #6: ADD TEST ELEMENTS BACK IN WITH-STRAIN *STATIC 1.0,1.0 *MODEL CHANGE,ADD=WITHSTRAIN,TYPE=ELEMENT TEST, *END STEP ** ** *STEP,NLGEOM STEP #7: APPLY THERMAL LOAD *STATIC .25,1.0 *BOUNDARY,OP=NEW,TYPE=VELOCITY TIP,1 LEFT,1,6 *TEMPERATURE NALL,100.,20.,0. *EL PRINT,POSITION=CENTROID,FREQ=999 1, S,THE,E *OUTPUT,FIELD,FREQ=999 *ELEMENT OUTPUT S,THE,E,TEMP *END STEP ** ** *STEP,NLGEOM STEP #8: FREQUENCY EXTRACTION *FREQUENCY, eigensolver=lanczos, SIM=NO 60, , *BOUNDARY,OP=NEW LEFT,1,6 *EL PRINT,FREQ=0 *NODE PRINT,FREQ=0 *OUTPUT,FIELD,FREQ=0 *END STEP ** ** *STEP,PERTURBATION STEP #9: MODAL DYNAMIC *MODAL DYNAMIC .6,6. *CLOAD TIP,1,150. *NODE PRINT,FREQ=999 RF, *EL PRINT,ELSET=EOUT,POSITION=CENTROID,FREQ=999 1, 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 .15,.2, 2 *CLOAD TIP,1,150. *NODE PRINT,FREQ=999 RF, *EL PRINT,ELSET=EOUT,POSITION=CENTROID,FREQ=999 1, 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 #11: STEADY-STATE DYNAMICS, DIRECT *STEADY STATE DYNAMICS,DIRECT .15,.2, 5 *BOUNDARY,OP=NEW LEFT,1,6 *CLOAD TIP,1,150. *NODE PRINT,FREQ=999 RF, *EL PRINT,ELSET=EOUT,POSITION=CENTROID,FREQ=999 1, 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 #12: STEADY-STATE DYNAMICS,SUBSPACE PROJECTION *STEADY STATE DYNAMICS,SUBSPACE PROJECTION,INTERVAL=RANGE .15,.2, 5 *CLOAD TIP,1,150. *NODE PRINT,FREQ=999 RF, *EL PRINT,ELSET=EOUT,POSITION=CENTROID,FREQ=999 1, 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,NLGEOM STEP #13: DYNAMICS *DYNAMIC .6,6. *BOUNDARY,OP=NEW,FIX LEFT,1,6 *EL PRINT,POSITION=CENTROID,FREQ=999 1, S,E *NODE PRINT,FREQ=999 RF, *CLOAD,AMP=RAMP TIP,1,15. *END STEP