*HEADING 1 X 4 mesh for cantilever bending problem with C3D10 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,NSET=MID 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=C3D10, ELSET=EALL 1, 1, 19, 51, 3, 10, 37, 28, 2, 11, 29 2, 69, 51, 19, 71, 60, 37, 42, 70, 61, 43 3, 21, 3, 71, 19, 12, 38, 44, 20, 11, 43 4, 53, 71, 3, 51, 62, 38, 30, 52, 61, 29 5, 3, 19, 51, 71, 11, 37, 29, 38, 43, 61 6, 21, 71, 3, 23, 44, 38, 12, 22, 45, 13 7, 53, 3, 71, 55, 30, 38, 62, 54, 31, 63 8, 5, 55, 23, 3, 32, 39, 14, 4, 31, 13 9, 73, 23, 55, 71, 46, 39, 64, 72, 45, 63 10, 3, 23, 71, 55, 13, 45, 38, 31, 39, 63 11, 5, 23, 55, 7, 14, 39, 32, 6, 15, 33 12, 73, 55, 23, 75, 64, 39, 46, 74, 65, 47 13, 25, 7, 75, 23, 16, 40, 48, 24, 15, 47 14, 57, 75, 7, 55, 66, 40, 34, 56, 65, 33 15, 7, 23, 55, 75, 15, 39, 33, 40, 47, 65 16, 25, 75, 7, 27, 48, 40, 16, 26, 49, 17 17, 57, 7, 75, 59, 34, 40, 66, 58, 35, 67 18, 9, 59, 27, 7, 36, 41, 18, 8, 35, 17 19, 77, 27, 59, 75, 50, 41, 68, 76, 49, 67 20, 7, 27, 75, 59, 17, 49, 40, 35, 41, 67 *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. 10, 1,, 0. 10, 2,, 0. 10, 3,, 0. 19, 1,, 0. 19, 2,, 0. 19, 3,, 0. 28, 1,, 0. 28, 2,, 0. 28, 3,, 0. 37, 1,, 0. 37, 2,, 0. 37, 3,, 0. 42, 1,, 0. 42, 2,, 0. 42, 3,, 0. 51, 1,, 0. 51, 2,, 0. 51, 3,, 0. 60, 1,, 0. 60, 2,, 0. 60, 3,, 0. 69, 1,, 0. 69, 2,, 0. 69, 3,, 0. MID, 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