*HEADING COPPER ROD IMPACT (AXISYMMETRIC) SECTION CONTROLS USED (HOURGLASS=COMBINED) Johnson-Cook plasticity with Johnson-Cook rate dependency and Johnson-Cook shear failure ** ** This example simulates the high velocity impact of a copper rod ** onto a rigid wall. Similar tests have been performed to determine ** the material constants for high-pressure equations of state, and ** the test is sometimes described as the Taylor bar experiment. ** Extremely high plastic strains develop at the crushed end of the ** rod, resulting in severe local mesh distortion. ** *RESTART, WRITE, NUMBER INTERVAL=20 ** ** Generate a 10 x 36 mesh for the bar ** *NODE, NSET=CORNERS 1, .0000, .0000 11, .0032, .0000 397, .0000, .0324 407, .0032, .0324 *NGEN, NSET=HEAD 1, 11, 1 *NGEN, NSET=TAIL 397, 407, 1 *NFILL, NSET=ROD HEAD, TAIL, 36, 11 *NSET, NSET=AXIS, GENERATE 1, 397, 11 *NSET, NSET=BODY, GENERATE 12, 407, 1 *NSET,NSET=NOUT 397, *ELEMENT, TYPE=CAX4R 1, 1, 2, 13, 12 *ELGEN, ELSET=ROD 1, 10, 1, 1, 36, 11, 10 ** ** Representative material properties for copper ** *MATERIAL, NAME=COPPER *ELASTIC 124.E9, 0.34 ** Young's unit: Pa *PLASTIC,HARDENING=JOHNSON COOK 90.E6, 292.E6, 0.31, 1.09, 1083., 25. ** A & B unit: Pa *RATE DEPENDENT,TYPE=JOHNSON COOK 0.025, 1.0 ** unit: reference strain rate has a unit of s^(-1) *SHEAR FAILURE,TYPE=JOHNSON COOK,ELEMENT DELETION=YES 0.54, 4.89, 3.03, 0.014, 1.12 *INELASTIC HEAT FRACTION 1., ** dimensionless *SPECIFIC HEAT 383., ** unit: J/kgK *EXPANSION 5.E-5, ** unit: K^(-1) *DENSITY 8.96E3, ** unit: kg/m^3 *SOLID SECTION, ELSET=ROD, MATERIAL=COPPER, CONTROL=B *SECTION CONTROLS, HOURGLASS=COMBINED, NAME=B ** ** Rigid wall *NODE 1000, 0., -0.0001 1001, 0., -0.0001 1002, 0.01, -0.0001 *ELEMENT,TYPE=RAX2,ELSET=WALL 1001,1001,1002 *BOUNDARY AXIS, 1 1000, 1, 2 1000, 6 *INITIAL CONDITIONS, TYPE=TEMPERATURE ROD, 25. *INITIAL CONDITIONS, TYPE=VELOCITY ROD, 2, -227. ** *NSET,NSET=NOUT HEAD,407 *ELSET,ELSET=EOUT,GENERATE 1,10,1 ** ** Run the problem for 80 microseconds ** *SURFACE,TYPE=ELEMENT, NAME=WALL WALL, SPOS *SURFACE,TYPE=NODE, NAME=ROD ROD, *RIGID BODY,ELSET=WALL,REF NODE=1000 *STEP *DYNAMIC, EXPLICIT, ADIABATIC ,80.E-6 ** *CONTACT PAIR WALL, ROD ** ***OUTPUT,HISTORY,TIME INTERVAL=1.E-7 ***ENERGY OUTPUT **DT, **ALLKE, ***NODE OUTPUT,NSET=NOUT **U, *OUTPUT,FIELD,VAR=PRESELECT,NUMBER INTERVAL=5 ** ** Output requests for qa testing ** *NSET,NSET=QA_TEST NOUT, *ELSET,ELSET=QA_TEST EOUT, *OUTPUT,FIELD,NUMBER INTERVAL=1 *NODE OUTPUT,NSET=QA_TEST U, *ELEMENT OUTPUT,ELSET=QA_TEST PEEQ, *OUTPUT,HISTORY,VAR=PRESELECT,TIME INTERVAL=2.E-5 *FILE OUTPUT, TIMEMARKS=YES, NUM=1 *EL FILE,ELSET=EOUT PEEQ, *NODE FILE,NSET=NOUT U, *ENERGY FILE *END STEP