*Heading AXISYMMETRIC TIRE-AIR INTERACTION REFERENCE SOLUTION USING *IMPORT USE RESTART FROM am_tire_acax8.inp *preprint,model=yes,HIST=yes *IMPORT,UPDATE=YES,STEP=1 TIRE *Node 1,132.894,17.4105 2,110,14.9999 3,110,12.1921 4,130.075,14.5615 5,110,0 6,132.111,5.69E-07 7,137.975,1.44E-04 8,127.27,20.3983 9,120.191,19.7686 10,114.404,17.4459 11,115.287,13.2969 12,120.927,14.643 13,126.104,14.9759 14,110,8.45017 15,110,4.31845 16,115.533,-5.12E-22 17,121.031,1.20E-16 18,126.519,-9.90E-12 19,131.763,5.48552 20,131.022,10.6113 21,137.506,6.19659 22,136.075,12.2761 23,115.419,8.96462 24,115.482,4.52289 25,120.859,9.62803 26,120.934,4.81361 27,126.087,10.0798 28,126.326,5.09469 51,136.315,11.8069 52,143.129,14.6038 53,110,19.919 54,110,15 55,140.992,-4.67E-33 56,138,-9.71E-33 57,144.996,-2.15E-36 58,139.596,13.1394 59,140.279,19.5501 60,135.585,22.9577 61,130.166,24.8095 62,124.455,25.4037 63,118.87,24.495 64,114.029,22.3233 65,110,18.2748 66,114.766,17.6431 67,119.534,19.6523 68,124.193,20.6544 69,128.626,20.3288 70,132.202,18.3006 71,134.673,15.2945 72,137.283,7.97499 73,137.755,4.0078 74,144.804,4.64455 75,144.339,9.47249 76,137.421,17.0905 77,134.022,20.2284 78,129.458,22.2244 79,124.345,22.7201 80,119.366,21.8218 81,114.646,19.8935 82,140.692,8.66072 83,141.145,4.3004 84,130.068,18.9118 85,126.709,17.7874 86,128.089,14.7687 87,131.535,16.037 88,123.729,20.5066 89,120.553,17.2463 90,123.515,14.8095 91,117.277,18.6879 92,114.845,15.3734 93,118.107,13.97 94,112.217,16.1707 95,110,13.5961 96,112.644,12.7445 97,110,10.3211 98,112.71,8.7074 99,115.353,11.1308 100,110,6.38431 101,112.741,4.42067 102,115.451,6.74375 103,110,2.15923 104,112.767,-2.56E-22 105,115.507,2.26144 106,118.139,9.29632 107,120.893,12.1355 108,118.208,4.66824 109,120.897,7.22082 110,118.282,5.98E-17 111,120.983,2.4068 112,123.473,9.85391 113,126.096,12.5279 114,123.63,4.95415 115,126.207,7.58724 116,123.775,-4.95E-12 117,126.422,2.54735 118,128.555,10.3455 119,130.549,12.5864 120,129.045,5.29011 121,131.393,8.04839 122,129.315,2.84E-07 123,131.937,2.74276 124,135.053,7.27E-05 125,137.803,3.09812 126,134.651,5.84303 127,136.966,9.27632 128,133.579,11.4538 129,134.751,15.0282 130,137.958,12.4727 131,138.508,15.1142 132,136.048,16.1919 133,135.492,13.5505 134,141.364,13.873 135,141.703,17.0759 136,138.85,18.3202 137,135.722,18.6589 138,133.113,19.2662 139,133.435,16.7967 140,137.931,21.2543 141,134.805,21.5942 142,131.739,21.2265 143,129.042,21.2761 144,130.412,19.3114 145,132.874,23.8842 146,129.813,23.5165 147,126.9,22.471 148,124.268,21.6885 149,126.412,20.4837 150,127.307,25.1028 151,124.4,24.0627 152,121.857,22.2655 153,119.452,20.7341 154,121.869,20.1393 155,121.661,24.9369 156,119.119,23.156 157,117.012,20.8596 158,114.708,18.773 159,117.155,18.6255 160,116.449,23.3945 161,114.337,21.1086 162,112.333,19.101 163,109.992,16.631 164,112.396,16.2698 165,112.013,21.1242 166,109.997,19.0981 167,140.142,10.8994 168,142.515,9.065 169,143.732,12.037 170,136.796,9.89042 171,138.986,8.318 172,140.92,6.48105 173,142.976,4.47411 174,144.569,7.0577 175,137.513,5.99123 176,139.453,4.16003 177,141.075,2.15522 178,142.996,-1.06E-02 179,144.901,2.32074 180,137.864,2.005 181,139.497,-1.38E-02 *Element, type=ACAX8 1, 1, 8, 13, 4, 84, 85, 86, 87 2, 8, 9, 12, 13, 88, 89, 90, 85 3, 9, 10, 11, 12, 91, 92, 93, 89 4, 10, 2, 3, 11, 94, 95, 96, 92 5, 3, 14, 23, 11, 97, 98, 99, 96 6, 14, 15, 24, 23, 100, 101, 102, 98 7, 15, 5, 16, 24, 103, 104, 105, 101 8, 11, 23, 25, 12, 99, 106, 107, 93 9, 23, 24, 26, 25, 102, 108, 109, 106 10, 24, 16, 17, 26, 105, 110, 111, 108 11, 12, 25, 27, 13, 107, 112, 113, 90 12, 25, 26, 28, 27, 109, 114, 115, 112 13, 26, 17, 18, 28, 111, 116, 117, 114 14, 13, 27, 20, 4, 113, 118, 119, 86 15, 27, 28, 19, 20, 115, 120, 121, 118 16, 28, 18, 6, 19, 117, 122, 123, 120 17, 6, 7, 21, 19, 124, 125, 126, 123 18, 19, 21, 22, 20, 126, 127, 128, 121 19, 20, 22, 1, 4, 128, 129, 87, 119 *Elset, elset=AIR, generate 1, 19, 1 *Solid Section, elset=AIR, material=AIR 1., *Nset, nset=CENT 53, 54, 65 *Nset, nset=NOUT 53, 54, 65, 69, 70 *Nset, nset=SYMM, generate 55, 57, 1 *Nset, nset=TIRE, generate 51, 83, 1 *Elset, elset=AIR_S1, generate 1, 4, 1 *Elset, elset=AIR_S2, generate 17, 19, 1 *Elset, elset=LINER_S2, generate 66, 70, 2 *Elset, elset=LINER_S4, generate 51, 63, 2 *Elset, elset=Set-1, generate 1, 19, 1 *Elset, elset=air-el, generate 1, 19, 1 *Surface, type=ELEMENT, name=air air_S2, S2 air_S1, S1 ** Constraint: air-liner *Tie, name=air_liner, adjust=yes,position=3 air, liner ** ** MATERIALS ** *Material, name=AIR *Acoustic Medium 14200., *Density 0.0012, ** ** INTERACTION PROPERTIES ** ** ** BOUNDARY CONDITIONS ** ** Name: Disp-BC-1 Type: Displacement/Rotation *Boundary SYMM, 2, 2 ** Name: Disp-BC-2 Type: Displacement/Rotation *Boundary CENT, 1, 1 ** Name: Disp-BC-3 Type: Symmetry/Antisymmetry/Encastre *Boundary 54, YSYMM ** Name: Disp-BC-4 Type: Symmetry/Antisymmetry/Encastre *Boundary 56, XSYMM ** ---------------------------------------------------------------- ** ** STEP: Step-1 ** *Step, name=Step-1, nlgeom, inc=200 *Static 0.1, 1., 1e-05, 1. ** **ADAPTIVE MESH,ELSET=AIR-el,FREQ=1,MESH SWEEPS=20 **PRINT,ADAPT=YES ** LOADS ** ** Name: SURFFORCE-1 Type: Pressure *Dsload LINER, P, -1.5 ** ** OUTPUT REQUESTS ** *Restart, write, frequency=1 ** ** FIELD OUTPUT: F-Output-1 ** *Output, field *Node Output U, ** ** HISTORY OUTPUT: H-Output-1 ** *Output, history *El Print, freq=999999 *Node Print, freq=999999 *End Step ******* step for frequency extraction. *step *frequency, sim, acousticCoupling=ON, norm=mass 10 *print eigval *end step *step *STEADY STATE DYNAMICS,interval=range 5.0,6.5,10 *CLOAD,load case=1 60,1,1,100 *CLOAD,load case=2 60,2,2,100 *OUTPUT, FIELD, FREQ=0 *OUTPUT,HISTORY *NODE OUTPUT,NSET=nout u, *END STEP *step *STEADY STATE DYNAMICS,SUBSPACE,interval=range 5.0,6.5,10 *CLOAD,load case=1 60,1,1,100 *CLOAD,load case=2 60,2,2,100 *OUTPUT, FIELD, FREQ=0 *OUTPUT,HISTORY *NODE OUTPUT,NSET=nout u, *END STEP *step *STEADY STATE DYNAMICS,DIRECT,interval=range 5.0,6.5,10 *CLOAD,load case=1 60,1,1,100 *CLOAD,load case=2 60,2,2,100 *OUTPUT, FIELD, FREQ=0 *OUTPUT,HISTORY *NODE OUTPUT,NSET=nout u, *END STEP