*HEADING ** ** Creep analysis of a rod. ** Verification of *HYPERELASTIC, MARLOW and *VISCOELASTIC ** incompressible ** *PREPRINT, MODEL=YES *NODE,NSET=ALL 1, 2,1. 11,0.0,0.0,1.0 12,1.0,0.0,1.0 13,1.0,1.0,1.0 14,0.0,1.0,1.0 15,0.0,0.0,2.0 16,1.0,0.0,2.0 17,1.0,1.0,2.0 18,0.0,1.0,2.0 *nset,nset=nx0 11,14,15,18 *nset,nset=nx1 12,13,16,17 *nset,nset=ny0 11,12,15,16 *nset,nset=nz0 11,12,13,14 *NSET, NSET=NDISP 2,12,13,16,17 *ELEMENT,TYPE=T3D2,ELSET=ONE 1, 1,2 *ELEMENT,TYPE=c3d8r,ELSET=two 2, 11,12,13,14,15,16,17,18 *elset,elset=eall 1,2 *SOLID SECTION,ELSET=ONE,MATERIAL=MAT1 *SOLID SECTION,ELSET=two,MATERIAL=MAT1 *MATERIAL,NAME=MAT1 *HYPERELASTIC,MARLOW, MODULI = INSTANTANEOUS *UNIAXIAL TEST DATA 0.0, 0.0 1.5506E5, 0.1338 2.4367E5, 0.2675 3.1013E5, 0.3567 4.2089E5, 0.6242 5.3165E5, 0.8917 5.9810E5, 1.1592 6.8671E5, 1.4268 8.8608E5, 2.0510 10.6329E5, 2.5860 12.4051E5, 3.0318 16.1709E5, 3.7898 19.9367E5, 4.3694 23.4810E5, 4.8153 27.4684E5, 5.1720 31.0127E5, 5.4395 34.5570E5, 5.7070 38.3228E5, 5.9299 42.0886E5, 6.0637 45.6329E5, 6.1975 49.3987E5, 6.3312 53.1646E5, 6.4650 56.9304E5, 6.5541 64.2405E5, 6.6433 *VOLUMETRIC TEST DATA 0.0, 1.0000 60.E5, .9703 118.2E5,.9412 175.2E5,.9127 231.1E5,.8847 *VISCOELASTIC,TIME=RELAXATION TEST DATA *COMBINED TEST DATA,SHRINF=0.50,VOLINF=0.50 0.99256 , 0.99256 , 0.10000 0.98525 , 0.98525 , 0.20000 0.97805 , 0.97805 , 0.30000 0.96402 , 0.96402 , 0.50000 0.93730 , 0.93730 , 0.90000 0.88886 , 0.88886 , 1.7000 0.80894 , 0.80894 , 3.3000 0.69864 , 0.69864 , 6.5000 0.58776 , 0.58776 , 12.900 0.52060 , 0.52060 , 25.700 0.50149 , 0.50149 , 51.300 0.50011 , 0.50011 , 76.900 0.50001 , 0.50001 , 100.00 *STEP, NLGEOM UNIAXIAL LOADING *STATIC 0.01,1.0,,0.05 *BOUNDARY 1,1,3 2,2,3 nx0,1,1 ny0,2,2 nz0,3,3 *CLOAD 2,1,65.0E5 nx1,1,16.25E5 *OUTPUT,FIELD, VARIABLE=PRESELECT *OUTPUT, HISTORY, VARIABLE=PRESELECT *ELEMENT OUTPUT, ELSET=eall S11, LE11, NE11, EE11, CE11, cener *NODE OUTPUT, NSET=NDISP U1 *END STEP *STEP, NLGEOM SUSTAIN LOAD *VISCO 5.,100.,2.,10., *END STEP