*HEADING 1D TRANSIENT WAVE PROPAGATION IN AN ACOUSTIC MEDIUM WITH CLOAD IN ABAQUS/EXPLICIT [AC3D4]; 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 ** FOR EXAMPLE AT THE END OF THE SIMULATION : ** P_1(0,0.0044)=1.826 ** P_51(0.5,0.0044)=1.221 ** P_101(1.0,0.0044)=0.616 ** THE ACCELERATION IS SPECIFIED USING *CLOAD ON DOF 8 ** ** SEE CH. 3.7.7 OF ABAQUS/VERIFICATION MANUAL ** *PREPRINT,ECHO=NO,HISTORY=NO,MODEL=YES *NODE, Nset=NALL 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=QA_TEST,GEN 1,10,1 45,55,1 90,101,1 *NSET,NSET=NOUT QA_TEST, *NSET,NSET=LOADED_NODES 1,1001,1501,2501 *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 ** *MATERIAL,NAME=AIR *DENSITY 1.21, *ACOUSTIC MEDIUM,BULK MODULUS 0.1424E6, ** ** Define nonreflective boundary at x=1 ** Using user calculated constants: ** 1/k1=0, 1/c1=1/(rho*c) *IMPEDANCE PROPERTY,NAME=NONREF 0, 2.41E-3 ** *RESTART,WRITE,NUMBER=1 *STEP *DYNAMIC,EXPLICIT ,.0044 *IMPEDANCE,prop=nonref 597,I4, 596,I2, ** ** Prescribe unit particle acceleration a0, inwards, ** so that _volume_ acceleration is a0*surface area. ** Distribute 1/4 to each corner node: *CLOAD LOADED_NODES,8,.25e-4 ** ** ************************* *OUTPUT,FIELD,NUMBER INTERVAL=1 *NODE OUTPUT POR *NODE OUTPUT,NSET=QA_TEST POR, ************************* ***OUTPUT,HISTORY, TIME INTERVAL=0.00022 ***NODE OUTPUT, NSET=NOUT **POR ************************* *END STEP