*HEADING STATIC INDENTATION OF A ELASTOMERIC FOAM WITH A HEMISPHERICAL PUNCH AND CAX4R ELEMENTS WITH ENHANCED HOURGLASS CONTROL ******************************************************** ** Measure the punch reaction force during the following 2 steps: ** Step 1: Displace punch 250 mm downwards. ** Step 2: Return punch to original position. ** (Units: N, mm, sec) ******************************************************** *PREPRINT,MODEL=YES,HISTORY=NO *RESTART,WRITE *NODE 1, 0., 300. 19, 0., 0. 481, 300., 300. 499, 300., 0. 601, 600., 300. 619, 600., 0. *NSET,NSET=N1 1, *NSET,NSET=N19 19, *NSET,NSET=N481 481, *NSET,NSET=N499 499, *NFILL,NSET=TOP,BIAS=.85 N1,N481,12,40 *NGEN,NSET=TOP 481,601,40 *NFILL,NSET=BOT,BIAS=.85 N19,N499,12,40 *NGEN,NSET=BOT 499,619,40 *NFILL,NSET=ALLN,BIAS=.9 TOP,BOT,9,2 *NSET,NSET=CENTER,GENERATE 1,19 *ELEMENT,TYPE=CAX4R 1,3,43,41,1 *ELGEN,ELSET=FOAM 1,15,40,10,9,2,1 *ELSET,ELSET=CENT,GENERATE 1,141,10 61,69 *ELSET,ELSET=ETOP,GENERATE 1,101,10 *ELSET,ELSET=UPPER,GEN 1,141,10 *NODE,NSET=PUNCH 1000,0.,510. *SOLID SECTION,ELSET=FOAM,MATERIAL=FOAM,ORIENTATION=RECT *ORIENTATION,NAME=RECT,SYSTEM=RECTANGULAR 1.,0.,0., 0.,1.,0. 3,0. **************************************************** *MATERIAL,NAME=FOAM *HYPERFOAM,N=2,TEST DATA INPUT,POISSON=0.0,MODULI=INSTANTANEOUS *UNIAXIAL TEST DATA -.0217, -.05 -.0317, -.10 -.0367, -.15 -.0402, -.20 -.0433, -.25 -.0467, -.30 -.0504, -.35 -.0542, -.40 -.0604, -.45 -.0668, -.50 -.0759, -.55 -.0909, -.60 -.1083, -.65 -.1410, -.70 -.1933, -.75 -.2896, -.80 *SIMPLE SHEAR TEST DATA .0140, .08, .0046 .0334, .16, .0166 .0533, .24, .0366 .0853, .32, .0573 .1280, .40, .0817 .1653, .48, .1098 .2080, .56, .1394 .2560, .64, .1666 .2987, .72, .1904 *VISCOELASTIC,TIME=RELAXATION TEST DATA *SHEAR TEST DATA,SHRINF=0.5000 1.0000, 0.0001 0.9695, 0.001 0.9417, 0.002 0.8722, 0.005 0.7913, 0.010 0.7043, 0.020 0.6233, 0.050 0.5736, 0.100 0.5271, 0.200 0.5013, 0.500 0.5000, 1.000 *DENSITY 1.E-11, **************************************************** *BOUNDARY BOT,1,2 CENTER,1 1000,1 1000,6 **************************************************** *SURFACE,TYPE=SEGMENTS,NAME=IMPACTOR START,141.42,641.42 CIRCL,-1.,300.,0.,500. *SURFACE,TYPE=ELEMENT,NAME=TARGET ETOP,S3 *RIGID BODY,REF NODE=1000,ANALYTICAL SURFACE=IMPACTOR *CONTACT PAIR,INTERACTION=ROUGH TARGET,IMPACTOR *SURFACE INTERACTION,NAME=ROUGH *FRICTION 0.8, **************************************************** *STEP,NLGEOM,INC=200,AMPLITUDE=RAMP,UNSYMM=YES,Convert Sdi=YES Displace punch 250 mm downwards. *STATIC .0015,1.,,.05 *BOUNDARY 1000,2,2,-250. *PRINT,CONTACT=YES *CONTACT PRINT,SLAVE=TARGET **CONTACT FILE,SLAVE=TARGET,FREQUENCY=10 *ENERGY PRINT,FREQUENCY=5 *ENERGY PRINT,ELSET=FOAM,FREQ=5 *ENERGY PRINT,ELSET=CENT,FREQ=5 *EL PRINT,FREQUENCY=50,ELSET=CENT S, E, *NODE PRINT,FREQUENCY=25 U, RF, *OUTPUT,FIELD,FREQUENCY=4 *NODE OUTPUT U,V,A,RF *ELEMENT OUTPUT S,LE,NE *CONTACT OUTPUT,VARIABLE=PRESELECT,NSET=TOP *OUTPUT,HISTORY,FREQUENCY=1 *NODE OUTPUT,NSET=PUNCH U,V,A,RF *ELEMENT OUTPUT,ELSET=CENT S,LE,NE *ENERGY OUTPUT,VARIABLE=PRESELECT *END STEP **************************************************** *STEP,NLGEOM,INC=200,AMPLITUDE=RAMP,UNSYMM=YES,Convert Sdi=YES Return punch to original position. *STATIC .0015,1.,,.05 *BOUNDARY,OP=MOD 1000,2,2,0.0 *OUTPUT,FIELD,FREQUENCY=4 *NODE OUTPUT U,V,A,RF *ELEMENT OUTPUT S,LE,NE *CONTACT OUTPUT,VARIABLE=PRESELECT,NSET=TOP *OUTPUT,HISTORY,FREQUENCY=1 *NODE OUTPUT,NSET=PUNCH U,V,A,RF *ELEMENT OUTPUT,ELSET=CENT S,LE,NE *ENERGY OUTPUT,VARIABLE=PRESELECT *END STEP