*HEADING 1D TRANSIENT WAVE PROPAGATION IN AN ACOUSTIC MEDIUM WITH PRESCRIBED ACCEL IN ABAQUS/EXPLICIT [AC3D4]; ** ** C = root (K/rho)= 343.05 m/s K=bulk mod, rho=density. ** ** Analytic solution to prescribed constant acceleration of a0 at x=0 ** ** p(x,t) = (K a0 / c^2) (ct - x) for x < ct ** = 0 for x > ct ** *PREPRINT,ECHO=NO,HISTORY=NO,MODEL=no *NODE, Nset=ODB_NSET 1, 0, 101, 1, 1001, 0, 1e-2 1101, 1, 1e-2 1501, 0, 1e-2, -1e-2 1601, 1, 1e-2, -1e-2 2501, 0, 0, -1e-2 2601, 1, 0, -1e-2 *NGEN,NSET=CHANNEL_NODES 1,101 1001,1101 1501,1601 2501,2601 *NSET,NSET=SAMPLE_NODES,GENERATE 1,101 *NSET,NSET=NALL ODB_NSET, CHANNEL_NODES, SAMPLE_NODES *NODE,NSET=LOAD 10001, 0, 10002, 0, 1e-2 10003, 0, 1e-2, -1e-2 10004, 0, 0, -1e-2 10005, -0.1e-2, 10006, -0.1e-2, 1e-2 10007, -0.1e-2, 1e-2, -1e-2 10008, -0.1e-2, 0, -1e-2 *ELEMENT,TYPE=AC3D4 1, 1, 1002, 2, 2501 2, 1002, 2, 2501, 1502 3, 2, 2501, 1502, 2502 4, 1, 1001, 1002, 2501 5, 1001, 1002, 2501, 1501 6, 1002, 2501, 1501, 1502 *ELGEN,ELSET=CHANNEL 1,100,1,6 2,100,1,6 3,100,1,6 4,100,1,6 5,100,1,6 6,100,1,6 ** *SOLID SECTION,MATERIAL=AIR,ELSET=CHANNEL *surface,NAME=NRS 597,S4 596,S2 ** *MATERIAL,NAME=AIR *DENSITY 1.21, *ACOUSTIC MEDIUM,BULK MODULUS 0.1424E6, *ELEMENT,TYPE=C3D6,ELSET=LOAD 800, 10001, 10002, 10004, 10005, 10006, 10008 900, 10002, 10003, 10004, 10006, 10007, 10008 *SOLID SECTION,MATERIAL=MAT1,ELSET=LOAD *MATERIAL,NAME=MAT1 *ELASTIC 180E2,0.333333 *DENSITY 76.70, ** ********************************* *SURFACE,TYPE=ELEMENT,NAME=SECONDARY 4, S2 5, S4 *SURFACE,TYPE=ELEMENT,NAME=MAIN 800, S1 900, S1 *TIE,NAME=COUPLING SECONDARY,MAIN ******************** *NSET, NSET=QA_TEST ODB_NSET ** *STEP *DYNAMIC,EXPLICIT ,.0036 ** Define nonreflective boundary at x=1 *IMPEDANCE 597,I4, 596,I2, ** ** Prescribe volume acceleration a0=1. ** Acceleration of interface element specified. ** In order to run single precision, the reference ** magnitude is increased to 1000. ** *BOUNDARY,TYPE=ACCELERATION LOAD,1,1,1.0E3 ** *OUTPUT,FIELD,NUMBER INTERVAL=1 *NODE OUTPUT POR *OUTPUT,HISTORY, FREQ=1 *NODE OUTPUT, NSET=QA_TEST POR *ENDSTEP *STEP *DYNAMIC,EXPLICIT ,.0008 ** Define nonreflective boundary at x=1 *IMPEDANCE,OP=NEW *SIMPEDANCE NRS ** *BOUNDARY,TYPE=ACCELERATION LOAD,1,1,1.0E3 ** *OUTPUT,FIELD,NUMBER INTERVAL=1 *NODE OUTPUT POR *OUTPUT,HISTORY, FREQ=1 *NODE OUTPUT, NSET=QA_TEST POR *ENDSTEP