*HEADING 2 X 4 mesh for cantilever bending problem with C3D4 elements. ** *NODE 1, 0., 0. 2, 0.75, 0. 3, 1.5, 0. 4, 2.25, 0. 5, 3., 0. 6, 3.75, 0. 7, 4.5, 0. 8, 5.25, 0. 9, 6., 0. 10, 0., 0.05 11, 0.75, 0.05 12, 1.5, 0.05 13, 2.25, 0.05 14, 3., 0.05 15, 3.75, 0.05 16, 4.5, 0.05 17, 5.25, 0.05 18, 6., 0.05 19, 0., 0.1 20, 0.75, 0.1 21, 1.5, 0.1 22, 2.25, 0.1 23, 3., 0.1 24, 3.75, 0.1 25, 4.5, 0.1 26, 5.25, 0.1 27, 6., 0.1 28, 0., 0.15 29, 0.75, 0.15 30, 1.5, 0.15 31, 2.25, 0.15 32, 3., 0.15 33, 3.75, 0.15 34, 4.5, 0.15 35, 5.25, 0.15 36, 6., 0.15 37, 0., 0.2 38, 0.75, 0.2 39, 1.5, 0.2 40, 2.25, 0.2 41, 3., 0.2 42, 3.75, 0.2 43, 4.5, 0.2 44, 5.25, 0.2 45, 6., 0.2 *NODE 46, 0., 0., 0.005 47, 0.75, 0., 0.005 48, 1.5, 0., 0.005 49, 2.25, 0., 0.005 50, 3., 0., 0.005 51, 3.75, 0., 0.005 52, 4.5, 0., 0.005 53, 5.25, 0., 0.005 54, 6., 0., 0.005 55, 0., 0.05, 0.005 56, 1.5, 0.05, 0.005 57, 3., 0.05, 0.005 58, 4.5, 0.05, 0.005 59, 6., 0.05, 0.005 60, 0., 0.1, 0.005 61, 0.75, 0.1, 0.005 62, 1.5, 0.1, 0.005 63, 2.25, 0.1, 0.005 64, 3., 0.1, 0.005 65, 3.75, 0.1, 0.005 66, 4.5, 0.1, 0.005 67, 5.25, 0.1, 0.005 68, 6., 0.1, 0.005 69, 0., 0.15, 0.005 70, 1.5, 0.15, 0.005 71, 3., 0.15, 0.005 72, 4.5, 0.15, 0.005 73, 6., 0.15, 0.005 74, 0., 0.2, 0.005 75, 0.75, 0.2, 0.005 76, 1.5, 0.2, 0.005 77, 2.25, 0.2, 0.005 78, 3., 0.2, 0.005 79, 3.75, 0.2, 0.005 80, 4.5, 0.2, 0.005 81, 5.25, 0.2, 0.005 82, 6., 0.2, 0.005 *NODE 83, 0., 0., 0.01 84, 0.75, 0., 0.01 85, 1.5, 0., 0.01 86, 2.25, 0., 0.01 87, 3., 0., 0.01 88, 3.75, 0., 0.01 89, 4.5, 0., 0.01 90, 5.25, 0., 0.01 91, 6., 0., 0.01 92, 0., 0.05, 0.01 93, 0.75, 0.05, 0.01 94, 1.5, 0.05, 0.01 95, 2.25, 0.05, 0.01 96, 3., 0.05, 0.01 97, 3.75, 0.05, 0.01 98, 4.5, 0.05, 0.01 99, 5.25, 0.05, 0.01 100, 6., 0.05, 0.01 101, 0., 0.1, 0.01 102, 0.75, 0.1, 0.01 103, 1.5, 0.1, 0.01 104, 2.25, 0.1, 0.01 105, 3., 0.1, 0.01 106, 3.75, 0.1, 0.01 107, 4.5, 0.1, 0.01 108, 5.25, 0.1, 0.01 109, 6., 0.1, 0.01 110, 0., 0.15, 0.01 111, 0.75, 0.15, 0.01 112, 1.5, 0.15, 0.01 113, 2.25, 0.15, 0.01 114, 3., 0.15, 0.01 115, 3.75, 0.15, 0.01 116, 4.5, 0.15, 0.01 117, 5.25, 0.15, 0.01 118, 6., 0.15, 0.01 119, 0., 0.2, 0.01 120, 0.75, 0.2, 0.01 121, 1.5, 0.2, 0.01 122, 2.25, 0.2, 0.01 123, 3., 0.2, 0.01 124, 3.75, 0.2, 0.01 125, 4.5, 0.2, 0.01 126, 5.25, 0.2, 0.01 127, 6., 0.2, 0.01 ** ** *ELEMENT, TYPE=C3D4, ELSET=EALL 1, 1, 19, 83, 3 2, 101, 83, 19, 103 3, 21, 3, 103, 19 4, 85, 103, 3, 83 5, 3, 19, 83, 103 6, 21, 103, 3, 23 7, 85, 3, 103, 87 8, 5, 87, 23, 3 9, 105, 23, 87, 103 10, 3, 23, 103, 87 11, 5, 23, 87, 7 12, 105, 87, 23, 107 13, 25, 7, 107, 23 14, 89, 107, 7, 87 15, 7, 23, 87, 107 16, 25, 107, 7, 27 17, 89, 7, 107, 91 18, 9, 91, 27, 7 19, 109, 27, 91, 107 20, 7, 27, 107, 91 21, 37, 119, 19, 39 22, 101, 19, 119, 103 23, 21, 103, 39, 19 24, 121, 39, 103, 119 25, 19, 39, 119, 103 26, 21, 39, 103, 23 27, 121, 103, 39, 123 28, 41, 23, 123, 39 29, 105, 123, 23, 103 30, 23, 39, 103, 123 31, 41, 123, 23, 43 32, 105, 23, 123, 107 33, 25, 107, 43, 23 34, 125, 43, 107, 123 35, 23, 43, 123, 107 36, 25, 43, 107, 27 37, 125, 107, 43, 127 38, 45, 27, 127, 43 39, 109, 127, 27, 107 40, 27, 43, 107, 127 *SOLID SECTION,ELSET=EALL,MATERIAL=A1 *MATERIAL,NAME=A1 *ELASTIC 1.E8,0. ** ** step 1,Default ** *STEP, PERTURBATION *STATIC ** ** fix ** *BOUNDARY 1, 1,, 0. 1, 2,, 0. 1, 3,, 0. 19, 1,, 0. 19, 2,, 0. 19, 3,, 0. 37, 1,, 0. 37, 2,, 0. 37, 3,, 0. 83, 1,, 0. 83, 2,, 0. 83, 3,, 0. 101, 1,, 0. 101, 2,, 0. 101, 3,, 0. 119, 1,, 0. 119, 2,, 0. 119, 3,, 0. ** ** load ** *CLOAD, OP=NEW 9, 2, -0.25 45, 2, -0.25 91, 2, -0.25 127, 2, -0.25 ** *NODE FILE U, *OUTPUT,FIELD *NODE OUTPUT U, *EL PRINT S, E, *END STEP