*HEADING ** ** spherical indentation test, regular mesh 10x30 ** material: PUR60 (B), SI units ** *RESTART,WRITE,FREQ=999 *NODE 1, 0., 0. 31, 0.090, 0. *NGEN,NSET=BOT 1, 31, 1 *NODE 311, 0., 0.030 341, 0.090, 0.030 *NGEN,NSET=TOP 311, 341, 1 *NFILL BOT, TOP, 10, 31 *NSET,NSET=LFT,GEN 1, 311, 31 *ELEMENT,TYPE=CAX4R 1, 1, 2, 33, 32 *ELGEN,ELSET=FOAM 1, 30, 1, 1, 10, 31, 30 *ELSET,ELSET=TOP,GENERATE 271, 300, 1 *ELSET,ELSET=OUT 1, 271 ** *SOLID SECTION,ELSET=FOAM,MATERIAL=FOAM *MATERIAL,NAME=FOAM *ELASTIC 7.5E6, 0.0 *CRUSHABLE FOAM,HARDENING=ISOTROPIC 1.0, 0. *CRUSHABLE FOAM HARDENING 0.2000E6, 0.0000 0.2577E6, 0.0094 0.2760E6, 0.0258 0.3053E6, 0.0452 0.3267E6, 0.0655 0.3623E6, 0.1084 0.3891E6, 0.1540 0.4250E6, 0.2405 0.4568E6, 0.3812 0.4738E6, 0.4600 0.5170E6, 0.6391 0.5862E6, 0.8570 0.6503E6, 0.9857 0.7470E6, 1.1324 0.9820E6, 1.2965 1.4702E6, 1.4808 2.7262E6, 1.6609 5.3911E6, 1.9000 *RATE DEPENDENT 4638., 2.285 *DENSITY 60., ** ** SURFACE DEFINITIONS *NODE,NSET=PUNCHREF 1000, 0.0, 0.1125 *SURFACE,TYPE=SEGMENT,NAME=PUNCH START, 0.0825, 0.1125 CIRCL, 0.0, 0.0300, 0.0, 0.1125 *RIGID BODY,REF NODE=PUNCHREF,ANALYTICAL SURFACE=PUNCH *SURFACE,TYPE=ELEMENT,NAME=FOAM TOP, S3 *CONTACT PAIR,INTERACTION=INTPROP FOAM, PUNCH *SURFACE INTERACTION,NAME=INTPROP *FRICTION,TAUMAX=1.15E5 0.2, ** ** BOUNDARY CONDITIONS *BOUNDARY LFT, 1 BOT, ENCASTRE PUNCHREF, 1 PUNCHREF, 6 ** *AMPLITUDE,NAME=VEL 0., 0., 0.01, 5.4 ** STEP: Step-1 *STEP,INC=500,NLGEOM,UNSYMM=YES Step-1 *STATIC 0.00001, .01 ** ** APPLIED LOAD *BOUNDARY,TYPE=VELOCITY,AMPLITUDE=VEL PUNCHREF, 2, 2, -1. **BOUNDARY ** PUNCHREF, 2, 2, -0.0270 ** ** Relax tolerance from a default of 0.005 to 0.2 because the time and ** space averaging produce values that are very small, thus requiring ** convergence with unnecessarily small residuals. Relax displacement ** tolerance from 0.01 to 0.1 *CONTROLS,PARAMETERS=FIELD 0.2, 0.1 ** *MONITOR,NODE=PUNCHREF,DOF=2 *ENERGY PRINT,FREQUENCY=999 *NODE FILE,NSET=PUNCHREF U, RF *OUTPUT,FIELD,FREQ=100 *ELEMENT OUTPUT S, PE, PEEQ, LE *NODE OUTPUT U, *OUTPUT,HISTORY,FRE=1 *ELEMENT OUTPUT,ELSET=OUT MISES, PRESS, PEEQ *NODE OUTPUT,NSET=PUNCHREF U, RF *END STEP ******************************************* ** STEP: Step-2 *STEP,INC=500,NLGEOM,UNSYMM=YES Step-2 *STATIC 0.0001, .01 ** ** APPLIED LOAD *BOUNDARY,TYPE=VELOCITY,AMPLITUDE=VEL PUNCHREF, 2, 2, 1. **BOUNDARY ** PUNCHREF, 2, 2, 0 *END STEP