Next: Example Model C1D2
Up: Example Models
Previous: Example Model B31BOX
This example illustrates the creation of a built-in flat plate under a uniformly distributed edge load.
PROPERTY FE-PROG ABAQUS GEOMETRY POINT P1 0 GEOMETRY POINT P2 100 GEOMETRY POINT P3 100 100 GEOMETRY POINT P4 100 PROPERTY MATERIAL MAT STEM 210E3 0.29 PROPERTY PHYSICAL THICKNESS TH1 1.0 GEOMETRY SURFACE 4POINTS P1 P2 P3 P4 MESHING TYPE S1 QU8 2 PROPERTY ATTACH S1 STEM TH1 PROPERTY BOUNDARY CONSTRAINT L4 12 PROPERTY LOAD PRESSURE L2 -100 0 MESHING GENERATE UTILITY WRITE ABAQUS cpe8.inp YES
********************************************** ** ABAQUS 5.2 INPUT DECK * ** CREATED BY FEMGEN/FEMVIEW VERSION 2.305 * ** TRANSLATED BY FEMGEN-ABAQUS VERSION 3.000 * ** FILE CREATED: DATE 06/04/94 TIME 15:29:03 * ********************************************** ** ********************************************** ** BINARY RESULT FILE FORMAT SELECTED * ** MESSAGE LOGGING IS OFF * ** DIALOG SESSION IS OFF * ** ABAQUS/Standard SELECTED * ** EXTERNAL MATERIAL DIRECTORY NOT USED * ** EXTERNAL RESULT OUTPUT FILE NOT USED * ********************************************** ** *HEADING FEMGEN MODEL CPE8 TRANSLATED BY PRE-ABAQUS 3.000 TITLE: No model title ** ********************************************** ** MODEL DEFINITION ... * ********************************************** ** ******************* ** MODEL GEOMETRY * ******************* ** *NODE, NSET=ALLNODE 1, 0.0000000 , 0.0000000 , 0.0000000 2, 50.00000 , 0.0000000 , 0.0000000 3, 100.0000 , 0.0000000 , 0.0000000 4, 0.0000000 , 50.00000 , 0.0000000 5, 50.00000 , 50.00000 , 0.0000000 6, 100.0000 , 50.00000 , 0.0000000 7, 0.0000000 , 100.0000 , 0.0000000 8, 50.00000 , 100.0000 , 0.0000000 9, 100.0000 , 100.0000 , 0.0000000 10, 25.00000 , 0.0000000 , 0.0000000 11, 75.00000 , 0.0000000 , 0.0000000 12, 0.0000000 , 25.00000 , 0.0000000 13, 50.00000 , 25.00000 , 0.0000000 14, 100.0000 , 25.00000 , 0.0000000 15, 25.00000 , 50.00000 , 0.0000000 16, 75.00000 , 50.00000 , 0.0000000 17, 0.0000000 , 75.00000 , 0.0000000 18, 50.00000 , 75.00000 , 0.0000000 19, 100.0000 , 75.00000 , 0.0000000 20, 25.00000 , 100.0000 , 0.0000000 21, 75.00000 , 100.0000 , 0.0000000 *ELEMENT, TYPE=CPS8 , ELSET=S1 1 1 2 5 4 10 13 15 12 2 2 3 6 5 11 14 16 13 3 4 5 8 7 15 18 20 17 4 5 6 9 8 16 19 21 18 ** ******************** ** SET DEFINITIONS * ******************** ** *ELSET, ELSET=PHY1 S1 , *ELSET, ELSET=ALL PHY1 , ** ************************* ** PROPERTY DEFINITIONS * ************************* ** *SOLID SECTION, ELSET=PHY1 ,MATERIAL=STEM 1.000000 , ** ************************* ** MATERIAL DEFINITIONS * ************************* ** *MATERIAL, NAME=STEM *DENSITY 0.0000000E+00, *ELASTIC, TYPE=ISO 210.0E+03,0.290 , 0.0 *EXPANSION, ZERO= 0.0.0000 0.0000000E+00, 0.0000 ** ************************** ** KINEMATIC CONSTRAINTS * ************************** ** *NSET, NSET=L4 7 17 4 12 1 *BOUNDARY L4 , 1, 1 *NSET, NSET=P1 1 *BOUNDARY P1 , 1, 2 ** ********************************************** ** HISTORY DEFINITION ... * ********************************************** ** ********************************************** ** FEMGEN LOADCASE 1 * ************************** ** *STEP, PERTURBATION *STATIC *ELSET, ELSET=FL2 2 4 *DLOAD, OP=NEW FL2 , P2 , -100.0000 ** *************************** ** RESULTS OUTPUT CONTROL * *************************** ** *NODE FILE U *EL FILE, POSITION=AVERAGED AT NODES S,E *EL FILE, POSITION=NODES S,E *EL FILE, POSITION=INTEGRATION POINTS S,COORD E,COORD *END STEP ** **********************************************