*Heading Import of plane stress elements with original position -- explicit-to-explicit analysis ** *import, update=NO, state=YES DETACHED_C3D10M_Q1_ELEM, DETACHED_C3D4_Q1_ELEM, DETACHED_C3D6_Q1_ELEM, DETACHED_C3D8R_Q1_ELEM, DETACHED_C3D8_Q1_ELEM, ** *boundary DETACHED_C3D10M_Q1_FIXED, ENCASTRE DETACHED_C3D4_Q1_FIXED, ENCASTRE DETACHED_C3D6_Q1_FIXED, ENCASTRE DETACHED_C3D8R_Q1_FIXED, ENCASTRE DETACHED_C3D8_Q1_FIXED, ENCASTRE ** *amplitude, name=STEP 0., 1., 100., 1. ** ---------------------------------------------------- *Step, name=Step-2 *dynamic, explicit , 4.E-02 *cload, amplitude=STEP DETACHED_C3D10M_Q1_CLOAD, 1, 3.20e+06 DETACHED_C3D4_Q1_CLOAD, 1, 3.20e+06 DETACHED_C3D6_Q1_CLOAD, 1, 3.20e+06 DETACHED_C3D8R_Q1_CLOAD, 1, 3.20e+06 DETACHED_C3D8_Q1_CLOAD, 1, 3.20e+06 ** *output, field, numberinterval=2 *nodeoutput, nset=ASSEMBLY_Q1_ALL U, RF *elementoutput, elset=ASSEMBLY_Q1_ALL S, ** ** Activate history output if required ** ** *output, history, frequency=1, op=NEW ** *nodeoutput, nset=ASSEMBLY_Q1_ALL ** U1, U2 ** *elementoutput, elset=ASSEMBLY_Q1_ALL ** MISES, *endstep