*HEADING 1D TRANSIENT WAVE PROPAGATION IN AN ACOUSTIC MEDIUM WITH PRESCRIBED ACCEL IN ABAQUS/EXPLICIT [AC3D6]; ** ** 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=AC3D6 1,1,1002,2,2501,1502,2502 2,1,1001,1002,2501,1501,1502 *ELGEN,ELSET=CHANNEL 1,100,1,2 2,100,1,2 *SOLID SECTION,MATERIAL=AIR,ELSET=CHANNEL *surface,NAME=NRS 199,S4 ** *MATERIAL,NAME=AIR *DENSITY 1.21, *ACOUSTIC MEDIUM,BULK MODULUS 0.1424E6, *ELEMENT,TYPE=C3D8R,ELSET=LOAD 500,10001,10004,10008,10005,10002,10003,10007,10006 *SOLID SECTION,MATERIAL=MAT1,ELSET=LOAD *MATERIAL,NAME=MAT1 *ELASTIC 180E2,0.333333 *DENSITY 76.70, ** ********************************* *SURFACE,TYPE=ELEMENT,NAME=SECONDARY 2,S3 *SURFACE,TYPE=ELEMENT,NAME=MAIN 500,S3 *TIE,NAME=COUPLING SECONDARY,MAIN ******************** *NSET, NSET=QA_TEST ODB_NSET ** *STEP *DYNAMIC,EXPLICIT ,.0036 ** Define nonreflective boundary at x=1 *IMPEDANCE 199,I4, ** ** 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 *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 ** *ENDSTEP