*HEADING : NAFEMS TEST LE3, Hemispherical Shell with Point Loads [S4R] *ELEMENT,TYPE=S4R ,ELSET=S4_P2 1000, 8, 9, 12, 11 1001, 9, 10, 13, 12 1002, 10, 17, 19, 13 1003, 17, 18, 20, 19 1004, 11, 12, 15, 14 1005, 12, 13, 16, 15 1006, 13, 19, 21, 16 1007, 19, 20, 22, 21 1008, 15, 16, 21, 24 1009, 14, 15, 24, 23 1010, 21, 22, 26, 24 1011, 23, 24, 26, 25 *ELEMENT,TYPE=S4R ,ELSET=S4_P4 3000, 64, 65, 70, 69 3001, 65, 66, 71, 70 3002, 66, 67, 72, 71 3003, 67, 68, 73, 72 3004, 68, 89, 93, 73 3005, 89, 90, 94, 93 3006, 90, 91, 95, 94 3007, 91, 92, 96, 95 3008, 69, 70, 75, 74 3009, 70, 71, 76, 75 3010, 71, 72, 77, 76 3011, 72, 73, 78, 77 3012, 73, 93, 97, 78 3013, 93, 94, 98, 97 3014, 94, 95, 99, 98 3015, 95, 96, 100, 99 3016, 74, 75, 80, 79 3017, 75, 76, 81, 80 3018, 76, 77, 82, 81 3019, 77, 78, 83, 82 3020, 78, 97, 101, 83 3021, 97, 98, 102, 101 3022, 98, 99, 103, 102 3023, 99, 100, 104, 103 3024, 79, 80, 85, 84 3025, 80, 81, 86, 85 3026, 81, 82, 87, 86 3027, 82, 83, 88, 87 3028, 83, 101, 105, 88 3029, 101, 102, 106, 105 3030, 102, 103, 107, 106 3031, 103, 104, 108, 107 3032, 87, 88, 105, 112 3033, 84, 85, 110, 109 3034, 85, 86, 111, 110 3035, 86, 87, 112, 111 3036, 105, 106, 116, 112 3037, 106, 107, 120, 116 3038, 107, 108, 124, 120 3039, 109, 110, 114, 113 3040, 110, 111, 115, 114 3041, 111, 112, 116, 115 3042, 113, 114, 118, 117 3043, 114, 115, 119, 118 3044, 115, 116, 120, 119 3045, 117, 118, 122, 121 3046, 118, 119, 123, 122 3047, 119, 120, 124, 123 *NODE 8, 10.0000, 0.0000, 0.0000, 1.0000, 0.0000, 0.0000 9, 9.2388, 3.8268, 0.0000, 0.9239, 0.3827, 0.0000 10, 7.0711, 7.0711, 0.0000, 0.7071, 0.7071, 0.0000 11, 9.2388, 0.0000, 3.8268, 0.9239, 0.0000, 0.3827 12, 8.6038, 3.5638, 3.6434, 0.8604, 0.3564, 0.3643 13, 6.7389, 6.7389, 3.0291, 0.6739, 0.6739, 0.3029 14, 7.0711, 0.0000, 7.0711, 0.7071, 0.0000, 0.7071 15, 6.7860, 2.8108, 6.7860, 0.6786, 0.2811, 0.6786 16, 5.7735, 5.7735, 5.7735, 0.5774, 0.5774, 0.5774 17, 3.8268, 9.2388, 0.0000, 0.3827, 0.9239, 0.0000 18, 0.0000, 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0.3827, 0.0000, 0.9239 114, 3.7605, 1.8538, 9.0786, 0.3761, 0.1854, 0.9079 115, 3.5638, 3.6434, 8.6038, 0.3564, 0.3643, 0.8604 116, 3.2435, 5.3067, 7.8306, 0.3244, 0.5307, 0.7831 117, 1.9509, 0.0000, 9.8079, 0.1951, 0.0000, 0.9808 118, 1.9143, 1.9271, 9.6240, 0.1914, 0.1927, 0.9624 119, 1.8060, 3.7820, 9.0794, 0.1806, 0.3782, 0.9079 120, 1.6300, 5.4951, 8.1944, 0.1630, 0.5495, 0.8194 121, 0.0000, 0.0000, 10.0000, 0.0000, 0.0000, 1.0000 122, 0.0000, 1.9509, 9.8079, 0.0000, 0.1951, 0.9808 123, 0.0000, 3.8268, 9.2388, 0.0000, 0.3827, 0.9239 124, 0.0000, 5.5557, 8.3147, 0.0000, 0.5556, 0.8315 *ELSET,ELSET=EALL S4_P2,S4_P4 *MATERIAL,NAME=A1 *ELASTIC,TYPE=ISO 6.825E+07, 0.3000, 0.0000 **GENERAL RIGID ELEMENTS *SHELL SECTION,MATERIAL=A1,ELSET=EALL 4.000E-02, *NSET,NSET=ZCONSTR 8,64 *NSET,NSET=XSYM 18,20,22,25,26,92,96,100,104,108,121,122,123,124 *NSET,NSET=YSYM 8,11,14,23,25,64,69,74,79,84,109,113,117,121 *NSET,NSET=DISPSET 8,64 *STEP,PERTURB *STATIC *BOUNDARY,OP=NEW ZCONSTR,3 XSYM,XSYMM YSYM,YSYMM *CLOAD,OP=NEW 8, 1, 2.000E+00 18, 2, -2.000E+00 64, 1, 2.000E+00 92, 2, -2.000E+00 *NODE PRINT,NSET=DISPSET U, COORD, *NODE FILE,NSET=DISPSET U, COORD, *OUTPUT,FIELD *NODE OUTPUT,NSET=DISPSET U, COORD, *EL PRINT,FREQUENCY=0 *END STEP