*HEADING - INCOMPRESSIBLE HYPERELASTICITY (YEOH), BIAXIAL TENSION *PREPRINT,MODEL=YES *NODE,NSET=ALL 1, 2,1. 3,1.,1., 4,0.,1., 5,0.,0.,1. 6,1.,0.,1. 7,1.,1.,1. 8,0.,1.,1. *NSET,NSET=FACE1 1,2,3,4 *NSET,NSET=FACE2 5,6,7,8 *NSET,NSET=FACE3 1,2,5,6 *NSET,NSET=FACE4 2 *NSET,NSET=FACE42 3,6,7 *NSET,NSET=FACE5 3 *NSET,NSET=FACE52 4,7,8 *NSET,NSET=FACE6 4,1,8,5 *EQUATION ** Since the S11 output is Cauchy or true stress, we need to ** determine the nominal stress for post-processing. ** Nodes 3,6,7 are tied to node 2 in dof 1 so that: ** Nominal stress (dof 1) = RF1 (@ node 2) / Original area ** (w/c is 1 x 1 = 1) 2 FACE42,1,1, 2,1,-1 *EQUATION 2 FACE52,2,1,3,2,-1 *ELEMENT,TYPE=C3D8RH,ELSET=ONE 1,1,2,3,4,5,6,7,8 *SOLID SECTION,ELSET=ONE,MATERIAL=YEOH *MATERIAL,NAME=YEOH *HYPERELASTIC, YEOH 1.326,-0.326,0.1319,0.0,0.0,0.0 *MULLINS EFFECT,TEST DATA INPUT *BIAXIAL TEST DATA 483.638 , 2. 307.653 , 1.9 197.176 , 1.8 129.372 , 1.7 87.2224 , 1.6 60.1221 , 1.5 42.0717 , 1.4 29.5985 , 1.3 20.7535 , 1.2 14.3889 , 1.1 9.79593 , 1. 6.51097 , 900.E-03 4.21196 , 800.E-03 2.66104 , 700.E-03 1.67218 , 600.E-03 1.09216 , 500.E-03 788.463E-03, 400.E-03 640.653E-03, 300.E-03 533.528E-03, 200.E-03 354.571E-03, 100.E-03 0.,0. *BIAXIAL TEST DATA 2.52169E+03, 3. 1.58161E+03, 2.85 1.00121E+03, 2.7 650.501 , 2.55 435.203 , 2.4 298.236 , 2.25 207.459 , 2.1 145.069 , 1.95 100.914 , 1.8 69.3758 , 1.65 46.6858 , 1.5 30.4757 , 1.35 19.1023 , 1.2 11.363 , 1.05 6.33716 , 900.E-03 3.29594 , 750.E-03 1.64788 , 600.E-03 902.022E-03,450.E-03 635.266E-03,300.E-03 456.6E-03 ,150.E-03 0.,0. *STEP,NLGEOM,INC=20 BIAXIAL TENSION *STATIC,DIRECT 1.,20. *BOUNDARY,OP=NEW FACE1,3 FACE3,2 FACE6,1 FACE4,1,1,2. FACE5,2,2,2. *EL PRINT,F=10 S, E, *NODE PRINT,F=10 U,RF *OUTPUT,HISTORY *NODE OUTPUT,NSET=FACE4 U,RF *ELEMENT OUTPUT,ELSET=ONE S, DMENER, SENER, *END STEP *STEP,NLGEOM,INC=20 *STATIC,DIRECT 1.,20. *BOUNDARY,OP=NEW FACE1,3 FACE3,2 FACE6,1 FACE4,1,1,0.0 FACE5,2,2,0.0 *END STEP *STEP,NLGEOM,INC=20 *STATIC,DIRECT 1.,20. *BOUNDARY,OP=NEW FACE1,3 FACE3,2 FACE6,1 FACE4,1,1,3. FACE5,2,2,3. *END STEP *STEP,NLGEOM,INC=20 *STATIC,DIRECT 1.,20. *BOUNDARY,OP=NEW FACE1,3 FACE3,2 FACE6,1 FACE4,1,1,0.0 FACE5,2,2,0.0 *END STEP