*HEADING ABAQUS job created on 16-Aug-95 at 16:26:28 ** *NODE 1, 0., 0. 2, 20., 0. 3, 40., 0. 4, 60., 0. 5, 80., 0. 6, 0., 20. 7, 40., 20. 8, 80., 20. 9, 0., 40. 10, 20., 40. 11, 40., 40. 12, 60., 40. 13, 80., 40. 14, 0., 60. 15, 40., 60. 16, 80., 60. 17, 0., 80. 18, 20., 80. 19, 40., 80. 20, 60., 80. 21, 80., 80. ** ** *ELEMENT, TYPE=S8R, ELSET=SQUARE_P 1, 1, 3, 11, 9, 2, 7, 10, 6 2, 3, 5, 13, 11, 4, 8, 12, 7 3, 9, 11, 19, 17, 10, 15, 18, 14 4, 11, 13, 21, 19, 12, 16, 20, 15 ** ** fem_model ** *NSET, NSET=FEM_MODE 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21 ** ** fem_model ** *ELSET, ELSET=FEM_MODE 1, 2, 3, 4 ** ** square_plate ** *SHELL SECTION, ELSET=SQUARE_P, MATERIAL=STEEL 0.25, ** ** steel ** Date: 16-Aug-95 Time: 16:14:23 ** *MATERIAL, NAME=STEEL ** *DENSITY 0.1, ** *ELASTIC, TYPE=ISO 2.E11, 0.3 ** ** *MATERIAL, NAME=MAT2 ** *DENSITY 0.1, ** *ELASTIC, TYPE=LAMINA 1.42E+09, 1.03E+08, 0.27, 7.2E+8, 2.E+12, 3.E+10 ** ** *RESTART,WRITE ** ** step 1,Default ** *STEP, AMPLITUDE=RAMP Linear Static Analysis ** This load case is the default load case that always appears ** *STATIC ** ** fixed_edge ** *BOUNDARY, OP=NEW 1, 1,6, 0. 6, 1,6, 0. 9, 1,6, 0. 14, 1,6, 0. 17, 1,6, 0. ** ** force_1 ** *CLOAD, OP=NEW 21, 3, -100.E10, ** *DLOAD, OP=NEW *TEMPERATURE, OP=NEW ** *NODE PRINT, FREQ=1 U *NODE FILE, FREQ=1 U ** *EL PRINT, POSITION=INTEGRATION POINTS, FREQ=1 SF *EL PRINT, POSITION=NODES, FREQ=1 SF *EL PRINT, POSITION=AVERAGED AT NODES, FREQ=1 SF ** *OUTPUT, FIELD *ELEMENT OUTPUT, POSITION=INTEGRATION POINTS SF ** *EL PRINT, POSITION=NODES, FREQ=0 ** *EL FILE, POSITION=NODES, FREQ=0 ** *EL PRINT, POSITION=CENTROIDAL, FREQ=0 ** *EL FILE, POSITION=CENTROIDAL, FREQ=0 ** *EL PRINT, POSITION=AVERAGED AT NODES, FREQ=0 ** *EL FILE, POSITION=AVERAGED AT NODES, FREQ=0 ** *MODAL PRINT, FREQ=99999 ** *MODAL FILE, FREQ=99999 ** *ENERGY PRINT, FREQ=0 ** *ENERGY FILE, FREQ=0 ** *PRINT, FREQ=1 ** *END STEP