*HEADING 1D TRANSIENT WAVE PROPAGATION IN AN ACOUSTIC MEDIUM WITH PRESCRIBED ACCEL IN ABAQUS/EXPLICIT [AC3D8R]; VERIFICATION PROBLEM: TRANSIENT DYNAMICS TESTS ** ** C=SQRT(K/RHO)= 343.05 M/S K=BULK MODULUS, 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 ** THE ACCELERATION IS SPECIFIED USING *BOUNDARY, TYPE=ACCELERATION ** *PREPRINT,ECHO=NO,HISTORY=NO,MODEL=NO *NODE, Nset=QA_TEST 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=NALL 1,101 1001,1101 1501,1601 2501,2601 *NSET,NSET=NALL NALL, QA_TEST *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=AC3D8R 1,1,2,2502,2501,1001,1002,1502,1501 *ELGEN,ELSET=CHANNEL 1,100 *SOLID SECTION,MATERIAL=AIR,ELSET=CHANNEL *surface, NAME=NRS 100,S4 *ELEMENT,TYPE=C3D8R,ELSET=LOAD 200,10001,10004,10008,10005,10002,10003,10007,10006 *SOLID SECTION,MATERIAL=MAT1,ELSET=LOAD *MATERIAL,NAME=MAT1 *ELASTIC 180E2,0.333333 *DENSITY 76.70, *MATERIAL,NAME=AIR *DENSITY 1.21, *ACOUSTIC MEDIUM,BULK MODULUS 0.1424E6, ********************************* *SURFACE,TYPE=ELEMENT,NAME=SECONDARY 1,S6 *SURFACE,TYPE=ELEMENT,NAME=MAIN 200,S3 *TIE,NAME=COUPLING SECONDARY,MAIN ******************* *STEP *DYNAMIC,EXPLICIT,ELEMENT BY ELEMENT ,.0036 ** Define nonreflective boundary at x=1 *IMPEDANCE 100,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.E3 **** *************************** *OUTPUT,FIELD,NUMBER INTERVAL=1 *NODE OUTPUT POR *NODE OUTPUT,NSET=QA_TEST POR, *************************** ***OUTPUT,HISTORY, FREQ=10 ***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.E3 *ENDSTEP