*HEADING EC3KAFAD: AC3D20 ELEMENTS Acoustic test - 1D Problem, SS-DIRECT. A 4m long tube; from left to right, a sound source, 3m is air, then 1m of a highly absorbent material, followed by a rigid termination. *PREPRINT,ECHO=NO,HISTORY=NO,MODEL=NO *RESTART,WRITE *********************************************************** ** ** ** Mesh Generation ** *NODE, Nset=ODB_NSET 1, 0, 0, 0 401, 4, 0, 0 501, 0, 0, -2 901, 4, 0, -2 1001, 0, 2, 0 1401, 4, 2, 0 1501, 0, 2, -2 1901, 4, 2, -2 2001, 0, 1, 0 2401, 4, 1, 0 2501, 0, 2, -1 2901, 4, 2, -1 3001, 0, 1, -2 3401, 4, 1, -2 3501, 0, 0, -1 3901, 4, 0, -1 *NGEN,NSET=ALL 1,401 501,901 1001,1401 1501,1901 2001,2401 2501,2901 3001,3401 3501,3901 *NSET,NSET=QA_TEST,GENERATE 1,401,10 *NSET,NSET=CRNRLOAD 1,1001,1501,501 *NSET,NSET=SIDELOAD 2001,2501,3001,3501 *ELEMENT,TYPE=AC3D20 1,1,3,503,501,1001,1003,1503,1501, 2,3503,502,3501,1002,2503,1502,2501, 2001,2003,3003,3001 *ELGEN,ELSET=CHANNEL 1,150,2 *ELEMENT,TYPE=AC3D20 301,301,303,803,801,1301,1303,1803,1801, 302,3803,802,3801,1302,2803,1802,2801, 2301,2303,3303,3301 *ELGEN,ELSET=ABSORB 301,50,2 *elset,elset=one 1, ************************************************ ** ** ELEMENT PROPERTIES ** ** *SOLID SECTION,MATERIAL=AIR,ELSET=CHANNEL *SOLID SECTION,MATERIAL=ABSORB,ELSET=ABSORB ** ** *MATERIAL,NAME=AIR *DENSITY 1.21, *ACOUSTIC MEDIUM,BULK MODULUS 0.1424E6, ** ** *MATERIAL,NAME=ABSORB *DENSITY 1.21, *ACOUSTIC MEDIUM,BULK MODULUS 0.1424E6, *ACOUSTIC MEDIUM,VOLUMETRIC DRAG 1e4, ** ** ** ************************************************* ** *Elset,Elset=ODB_ESET CHANNEL, ABSORB ** ** *Nset, Nset=ODB_NSET ODB_NSET, ALL, QA_TEST ** ** *STEP *STEADY STATE DYNAMICS,DIRECT,FREQUENCY SCALE=LINEAR 10,1100,13,1 ** ** Prescribe outward acceleration of 100 at node LOAD. ** To prescribe a total outward volume acceleration ** of 1 on the face with area 4, the load must be ** distributed in the ratios (-1/12,1/3) to the ** (corner,midside) nodes, respectively: ** *CLOAD CRNRLOAD,8, .33333E2 SIDELOAD,8, -1.33333E2 *NODE PRINT, NSET=QA_TEST POR,PPOR, *EL PRINT,FREQUENCY=0 *ENERGYPRINT *OUTPUT,FIELD *NODE OUTPUT,NSET=QA_TEST POR, *ELEMENT OUTPUT ACV,INTEN,GRADP,ENER,ELEN,ELEDEN *OUTPUT,HISTORY *NODE OUTPUT,NSET=QA_TEST POR, *ENERGY OUTPUT ALLSE,ALLKE,ALLWK,ALLVD *ENDSTEP ** ** *STEP *FREQUENCY,NORM=MASS,EIGENSOLVER=LANCZOS, SIM=NO 50, , , *NODE PRINT,F=0 *EL PRINT,F=0 *OUTPUT,FIELD,Frequency=0 *END STEP ** ** *STEP *STEADY STATE DYNAMICS,SUBSPACE PROJECTION=EIGENFREQUENCY,FREQUENCY SCALE=LINEAR,INTERVAL=RANGE 100,1100,3,1 ** ** Prescribe outward acceleration of 100 at node LOAD. ** To prescribe a total outward volume acceleration ** of 1 on the face with area 4, the load must be ** distributed in the ratios (-1/12,1/3) to the ** (corner,midside) nodes, respectively: *CLOAD CRNRLOAD,8, .33333E2 SIDELOAD,8, -1.33333E2 ** *NODE PRINT, NSET=QA_TEST POR,PPOR, *EL PRINT,FREQUENCY=0 *energyprint *OUTPUT,FIELD,VARIABLE=PRESELECT,OP=ADD,FREQUENCY=9999 *OUTPUT,FIELD, OP=ADD *NODE OUTPUT,NSET=QA_TEST POR, *ELEMENT OUTPUT,ELSET=ABSORB ACV,INTEN,GRADP *OUTPUT,HISTORY *NODE OUTPUT,NSET=QA_TEST POR, *ENERGY OUTPUT ALLSE,ALLKE,ALLWK,ALLVD *ENDSTEP