*HEADING AIRSPRING -- 180 DEG MODEL *NODE, NSET = FPLANE 1,2.E-2,0.,0. 4,2.E-2,0.,20.E-2,0.,0.,1.0 6,0.,0.,20.E-2,0.,0.,1.0 26,0.,0.,40.E-2,0.,0.,-1.0 32,6.293E-2,0.,37.771E-2,-0.58431,0.,-0.81153 38,10.698E-2,0.,36.211E-2,0.,0.,-1.0 39,11.35E-2,0.,36.211E-2,0.,0.,-1.0 40,12.E-2,0.,36.211E-2,0.,0.,-1.0 41,12.E-2,0.,0. *NGEN, LINE = C, NSET = FPLANE 6, 26, 2, , 0., 0., 30.E-2, 0., 1., 0. 26, 32, 1, , 0., 0., 30.E-2 32, 38, 1, , 10.698E-2, 0., 43.211E-2 *NCOPY,OLDSET=FPLANE,CHANGE NUMBER=100,SHIFT, MULTIPLE=22,NEWSET=NALL 0., 0., 0. 0., 0., 0., 1., 0., 0., 8.18181818 *NODE, NSET = RIGID 11000, 12.E-2, 0. , 0. *NODE, NSET = CAVITY 50000, 9.E-2 , 0. , 0. ** ** RUBBER SPRING ** *ELEMENT, TYPE = S4R 2, 4, 6, 106, 104 26, 26, 27, 127, 126 *ELGEN, ELSET = SPRING1 2, 11, 2, 2, 22, 100, 100 *ELGEN, ELSET = SPRING2 26, 14, 1, 1, 22, 100, 100 *ELSET,ELSET=SPRING SPRING1,SPRING2 *SHELL SECTION, MATERIAL = RUBBER, ELSET = SPRING 6.0E-3, *MATERIAL, NAME = RUBBER *HYPERELASTIC, POLYNOMIAL, N = 1 3.2E6, 0.8E6 *DENSITY 1000., *REBAR,ELEMENT=SHELL,MATERIAL=STEEL,GEOMETRY=SKEW, NAME=PLSREBAR SPRING, 1.E-6, 3.5E-3, 0., 18.0 *REBAR,ELEMENT=SHELL,MATERIAL=STEEL,GEOMETRY=SKEW, NAME=MNSREBAR SPRING, 1.E-6, 3.5E-3, 0., -18.0 *MATERIAL, NAME = STEEL *ELASTIC 2.1E11, 0.3 *DENSITY 7.8E3, ** ** FLUID ELEMENTS ** *ELEMENT, TYPE = F3D3, ELSET = FLUID 6001, 1, 4, 104 6040, 40, 41, 140 *ELGEN, ELSET = FLUID 6001, 22, 100, 100 6040, 22, 100, 100 *ELEMENT, TYPE = F3D4, ELSET = FLUID 6002, 4, 6, 106, 104 6026, 26, 27, 127, 126 *ELGEN, ELSET = FLUID 6002, 11, 2, 2, 22, 100, 100 6026, 14, 1, 1, 22, 100, 100 *PHYSICAL CONSTANTS, ABSOLUTE ZERO=-273.16 *FLUID PROPERTY, REF NODE=50000, TYPE=PNEUMATIC, ELSET=FLUID, AMBIENT=101.36E+3 *FLUID DENSITY, PRESSURE=0.0, TEMPERATURE=27.0 1.774, ** ** RIGID BODY/SURFACE ** *NODE, NSET = RIGID 11000, 12.E-2, 0., 0. *NODE,NSET=RIGNODE 11001, 12.E-2, 0., 36.511E-2 11021, 6.5E-2, 0., 42.011E-2 12000, 12.E-2, 0., 42.011E-2 *NGEN,NSET=RIGNODE,LINE=C 11001, 11021, 1, 12000 *NCOPY,OLDSET=RIGNODE,CHANGE NUMBER=100,SHIFT, MULTIPLE=22,NEWSET=NALL 0., 0., 0. 0., 0., 0., 1., 0., 0., 8.18181818 *ELEMENT,TYPE=R3D4,ELSET=RIGELEM 11001, 11001,11101,11102,11002 *ELEMENT, TYPE=R3D3, ELSET=RIGELEM 112001, 11000, 11101, 11001 112002, 11000, 11201, 11101 112003, 11000, 11301, 11201 112004, 11000, 11401, 11301 112005, 11000, 11501, 11401 112006, 11000, 11601, 11501 112007, 11000, 11701, 11601 112008, 11000, 11801, 11701 112009, 11000, 11901, 11801 112010, 11000, 12001, 11901 112011, 11000, 12101, 12001 112012, 11000, 12201, 12101 112013, 11000, 12301, 12201 112014, 11000, 12401, 12301 112015, 11000, 12501, 12401 112016, 11000, 12601, 12501 112017, 11000, 12701, 12601 112018, 11000, 12801, 12701 112019, 11000, 12901, 12801 112020, 11000, 13001, 12901 112021, 11000, 13101, 13001 112022, 11000, 13201, 13101 *ELGEN,ELSET=RIGELEM 11001, 22,100,100, 20,1,1 *ELEMENT,TYPE=MASS,ELSET=MASS_RIGID 11000, 11000 *MASS,ELSET=MASS_RIGID .5, ** ** KINEMATIC CONSTRAINTS ** *NSET, NSET = N1M1, GENERATE 101, 2201, 100 *NSET, NSET = N4, GENERATE 4, 2204, 100 *NSET, NSET = N6, GENERATE 6, 2206, 100 *NSET, NSET = N40, GENERATE 40, 2240, 100 *NSET, NSET = N41, GENERATE 41, 2241, 100 *NSET, NSET = YPLN1, GENERATE 4, 26, 2 26, 39, 1 *NSET, NSET = YPLN2, GENERATE 2204, 2226, 2 2226, 2239, 1 *BOUNDARY 1,1,6 N4,1,6 N6,2,3 YPLN1, 2 YPLN1, 4 YPLN1, 6 YPLN2, 2 YPLN2, 4 YPLN2, 6 RIGID,1,6 ** ** STEP 1 - INFLATION STEP (5 ATMOSPHERES) ** *AMPLITUDE,NAME=RAMP,DEFINITION=SMOOTH STEP 0.,0., 1.E-2,1.0 *AMPLITUDE,NAME=RAMPSMOOTH,DEFINITION=SMOOTH STEP 0.,0., 2.E-2,1.0 *SURFACE,TYPE=ELEMENT, NAME = ASURF ASURF,SNEG *SURFACE,TYPE=ELEMENT, NAME = RSURF RIGELEM,SPOS *RIGID BODY,REFNODE=1,PINNSET=N1M1 *RIGID BODY,REFNODE=11000,ELSET=RIGELEM,TIENSET=RIG *NSET, NSET=QA_TEST 2216,2218,2220,2222, *STEP *DYNAMIC,EXPLICIT ,1.E-2 *BOUNDARY,AMPLITUDE=RAMP CAVITY,8,8, 5.066E5 ** ** CONTACT DEFINITION ** *NSET,NSET=RIG N40,N41 *ELSET,ELSET=ASURF,GEN 26,2126,100 27,2127,100 28,2128,100 29,2129,100 30,2130,100 31,2131,100 32,2132,100 33,2133,100 34,2134,100 35,2135,100 36,2136,100 37,2137,100 38,2138,100 *CONTACT PAIR, INTERACTION = SMOOTH ASURF, RSURF *SURFACE INTERACTION, NAME = SMOOTH ** ** OUTPUT REQUESTS ** *OUTPUT, FIELD, TIME MARKS=YES, NUMBER INTER=2 *NODE OUTPUT, NSET=QA_TEST U, *OUTPUT, HIST *ENERGY OUTPUT, VAR=PRESELECT *NODE OUTPUT, NSET=RIGID U, RF *OUTPUT, FIELD, TIME MARKS=YES, NUMBER INTER=4 *NODE OUTPUT U, *ELSET,ELSET=TOP 39,2139,1039 *END STEP ** ** STEP 2 - SEAL CAVITY, LOAD FURTHER ** *STEP *DYNAMIC,EXPLICIT ,2.E-2 *BOUNDARY, OP=NEW,AMPLITUDE=RAMPSMOOTH 1,1,6 N4,1,6 N6,2,3 YPLN1, 2 YPLN1, 4 YPLN1, 6 YPLN2, 2 YPLN2, 4 YPLN2, 6 RIGID,1,2 RIGID,4,6 RIGID,3,3, 2.E-2 *END STEP