*HEADING 1 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., 0.1 11, 0.75, 0.1 12, 1.5, 0.1 13, 2.25, 0.1 14, 3., 0.1 15, 3.75, 0.1 16, 4.5, 0.1 17, 5.25, 0.1 18, 6., 0.1 19, 0., 0.2 20, 0.75, 0.2 21, 1.5, 0.2 22, 2.25, 0.2 23, 3., 0.2 24, 3.75, 0.2 25, 4.5, 0.2 26, 5.25, 0.2 27, 6., 0.2 *NODE 28, 0., 0., 0.005 29, 0.75, 0., 0.005 30, 1.5, 0., 0.005 31, 2.25, 0., 0.005 32, 3., 0., 0.005 33, 3.75, 0., 0.005 34, 4.5, 0., 0.005 35, 5.25, 0., 0.005 36, 6., 0., 0.005 37, 0., 0.1, 0.005 38, 1.5, 0.1, 0.005 39, 3., 0.1, 0.005 40, 4.5, 0.1, 0.005 41, 6., 0.1, 0.005 42, 0., 0.2, 0.005 43, 0.75, 0.2, 0.005 44, 1.5, 0.2, 0.005 45, 2.25, 0.2, 0.005 46, 3., 0.2, 0.005 47, 3.75, 0.2, 0.005 48, 4.5, 0.2, 0.005 49, 5.25, 0.2, 0.005 50, 6., 0.2, 0.005 *NODE 51, 0., 0., 0.01 52, 0.75, 0., 0.01 53, 1.5, 0., 0.01 54, 2.25, 0., 0.01 55, 3., 0., 0.01 56, 3.75, 0., 0.01 57, 4.5, 0., 0.01 58, 5.25, 0., 0.01 59, 6., 0., 0.01 60, 0., 0.1, 0.01 61, 0.75, 0.1, 0.01 62, 1.5, 0.1, 0.01 63, 2.25, 0.1, 0.01 64, 3., 0.1, 0.01 65, 3.75, 0.1, 0.01 66, 4.5, 0.1, 0.01 67, 5.25, 0.1, 0.01 68, 6., 0.1, 0.01 69, 0., 0.2, 0.01 70, 0.75, 0.2, 0.01 71, 1.5, 0.2, 0.01 72, 2.25, 0.2, 0.01 73, 3., 0.2, 0.01 74, 3.75, 0.2, 0.01 75, 4.5, 0.2, 0.01 76, 5.25, 0.2, 0.01 77, 6., 0.2, 0.01 ** ** *ELEMENT, TYPE=C3D4, ELSET=EALL 1, 1, 19, 51, 3 2, 69, 51, 19, 71 3, 21, 3, 71, 19 4, 53, 71, 3, 51 5, 3, 19, 51, 71 6, 21, 71, 3, 23 7, 53, 3, 71, 55 8, 5, 55, 23, 3 9, 73, 23, 55, 71 10, 3, 23, 71, 55 11, 5, 23, 55, 7 12, 73, 55, 23, 75 13, 25, 7, 75, 23 14, 57, 75, 7, 55 15, 7, 23, 55, 75 16, 25, 75, 7, 27 17, 57, 7, 75, 59 18, 9, 59, 27, 7 19, 77, 27, 59, 75 20, 7, 27, 75, 59 *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. 51, 1,, 0. 51, 2,, 0. 51, 3,, 0. 69, 1,, 0. 69, 2,, 0. 69, 3,, 0. ** ** load ** *CLOAD, OP=NEW 9, 2, -0.25 27, 2, -0.25 59, 2, -0.25 77, 2, -0.25 ** *NODE FILE U, *OUTPUT,FIELD *NODE OUTPUT U, *EL PRINT S, E, *END STEP