*HEADING BUCKLING OF X SHAPED CROSS SECTION WITH GENERAL CONTACT MODEL WITH SHEAR FAILURE AND EROSION *PREPRINT,MODEL=YES,HISTORY=YES,CONTACT=YES *NODE 601,0.,-.2,0.0 611,0., .2,0.0 106,0., 0.,-.2 1106,0., 0., .2 ** 10601,0.05,-.2,0.0 10611,0.05, .2,0.0 10106,0.05, 0.,-.2 11106,0.05, 0., .2 *NGEN,NSET=A 601,611,1 106,1106,100 *NGEN,NSET=A1 10601,10611,1 10106,11106,100 *NODE 200601,1.,-.2,0.0 200611,1., .2,0.0 200106,1., 0.,-.2 201106,1., 0., .2 ** 190601,0.95,-.2,0.0 190611,0.95, .2,0.0 190106,0.95, 0.,-.2 191106,0.95, 0., .2 *NGEN,NSET=B 200601,200611,1 200106,201106,100 *NGEN,NSET=B1 190601,190611,1 190106,191106,100 *NFILL,NSET=ALL1 A1,B1,18,10000 *ELEMENT,TYPE=S4R 1, 601,602,10602,10601 101, 606,607,10607,10606 201, 106,206,10206,10106 301, 606,706,10706,10606 *ELGEN,ELSET=FIN1 1, 5,1,1, 20,10000,5 *ELGEN,ELSET=FIN2 101, 5,1,1, 20,10000,5 *ELGEN,ELSET=FIN3 201, 5,100,1, 20,10000,5 *ELGEN,ELSET=FIN4 301, 5,100,1, 20,10000,5 *ELSET,ELSET=SHELLS FIN1,FIN2,FIN3,FIN4 *SHELL SECTION, SECTION INT=GAUSS,ELSET=SHELLS,MATERIAL=STEEL .003, *NODE 500001,0.,-.45,-.45 500002,0., .0,-.45 500003,0., .45,-.45 500004,0.,-.45,0. 500005,0., .0,0. 500006,0., .45,0. 500007,0.,-.45,.45 500008,0., .0,.45 500009,0., .45, .45 599995,0.,0.,0. *ELEMENT,TYPE=R3D4,ELSET=WALL1 500001, 500001,500002,500005,500004 500002, 500002,500003,500006,500005 500003, 500004,500005,500008,500007 500004, 500005,500006,500009,500008 *NODE 600001,1.,-.45,-.45 600002,1., .0,-.45 600003,1., .45,-.45 600004,1.,-.45,0. 600005,1., .0,0. 600006,1., .45,0. 600007,1.,-.45,.45 600008,1., .0,.45 600009,1., .45, .45 699995,1.,0.,0. *ELEMENT,TYPE=R3D4,ELSET=WALL2 600001, 600001,600002,600005,600004 600002, 600002,600003,600006,600005 600003, 600004,600005,600008,600007 600004, 600005,600006,600009,600008 *MATERIAL,NAME=STEEL *DENSITY 7850., *ELASTIC 200.E9,.3 *PLASTIC 250.E6,0. 700.E6,1. *SHEAR FAILURE 0.4, *BOUNDARY 599995,2,3 599995,4,4 599995,6,6 699995,1,6 *INITIAL CONDITIONS,TYPE=VELOCITY 599995, 1,1, 50. 599995, 5,5, 78.54 *RESTART,TIMEMARKS=NO,WRITE,NUM=10 ** *SURFACE,TYPE=ELEMENT, NAME=WALL1 WALL1,SPOS *SURFACE,TYPE=ELEMENT, NAME=WALL2 WALL2,SNEG *SURFACE,TYPE=NODE,NAME=A A, *SURFACE,TYPE=NODE,NAME=B B, ** *RIGID BODY, ELSET=WALL1, REF NODE=599995 *RIGID BODY, ELSET=WALL2, REF NODE=699995 *NSET,NSET=NRIGID 599995,699995 *TIE, NAME=TIE1,POSITION TOLERANCE=1.E-4 A, WALL1 *TIE, NAME=TIE2,POSITION TOLERANCE=1.E-4 B, WALL2 *ELSET,ELSET=QA_TESTEL,GEN 101,130 *NSET,NSET=QA_TESTN,GEN 121106,201106 *NSET,NSET=QA_TESTRB NRIGID, *STEP *DYNAMIC,EXPLICIT ,0.7E-2 *BOUNDARY,TYPE=VEL ** compress 35 percent axially and rotate 31 degrees during the step 599995, 1,1, 50. 599995, 5,5, 78.54 ** *CONTACT *CONTACT INCLUSIONS,ALL ELEMENT BASED ** ** Output requests for postprocessing ** *FILE OUTPUT,NUMBER=4,TIMEMARKS=YES *ENERGY FILE *NODE FILE U,RF *OUTPUT,FIELD,VAR=PRESELECT *OUTPUT,HISTORY,TIME INTERVAL=2.E-5 *NODE OUTPUT, NSET=NRIGID U, RF ** ** Output requests for qa testing ** *OUTPUT,FIELD,NUMBER INTERVAL=1 *ELEMENT OUTPUT,ELSET=QA_TESTEL STATUS, *END STEP