*HEADING EC36AFAS: AC3D6 & ASI4 1D transient wave propagation in an acoustic medium with prescribed acceleration on dof 1. Verification problem: Transient Dynamics Tests ** ** 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=YES,MODEL=YES ** *part,name=old *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,GENERATE 1,101 *NSET,NSET=LOAD 1,1001,1501,2501 *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 *ELEMENT,TYPE=ASI4,ELSET=LOAD 1200,1,2501,1501,1001 *INTERFACE,ELSET=LOAD *endpart *part,name=new *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,GENERATE 1,101 *NSET,NSET=LOAD 1,1001,1501,2501 *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 *ELEMENT,TYPE=ASI3d3,ELSET=LOAD 1200,1,2501,1001 1201,2501,1501,1001 *INTERFACE,ELSET=LOAD *endpart ** *assembly,name=both *instance,name=old,part=old *endinstance *instance,name=new,part=new 0,0.05,0 *endinstance *nset,nset=sample old.sample,new.sample *nset,nset=load old.load,new.load *surface,NAME=NRS old.199,S4 new.199,s4 *nset,nset=channel_nodes old.channel_nodes,new.channel_nodes *endassembly ************************************** *MATERIAL,NAME=AIR *DENSITY 1.21, *ACOUSTIC MEDIUM,BULK MODULUS,DEP=1 0.999999,10 0.1424E6,20,1 ** *RESTART,WRITE *INITIAL CONDITIONS,TYPE=FIELD CHANNEL_NODES,1 *INITIAL CONDITIONS,TYPE=TEMPERATURE CHANNEL_NODES,20 ** *STEP,INC=1000 *DYNAMIC,DIRECT,APPLICATION=TRANSIENT FIDELITY .0001,.0036 ** Define nonreflective boundary at x=1 *IMPEDANCE old.199,I4, new.199,I4 ** ** Prescribe acceleration inwards of a0=1. ** *BOUNDARY,TYPE=ACCELERATION LOAD,1,1,1. *EL PRINT,FREQ=0 *NODE PRINT,NSET=SAMPLE,FREQ=6 POR, *NODE FILE,NSET=SAMPLE,FREQ=6 POR, *OUTPUT,FIELD, OP=NEW,Frequency=6 *NODE OUTPUT POR, *OUTPUT,HISTORY,OP=ADD,Frequency=6 *NODE OUTPUT,NSET=SAMPLE POR, *ENDSTEP *********************** *STEP,INC=1000 *DYNAMIC,DIRECT,APPLICATION=TRANSIENT FIDELITY .0001,.0008 *IMPEDANCE,OP=NEW *SIMPEDANCE NRS, *BOUNDARY,TYPE=ACCELERATION LOAD,1,1,1. *EL PRINT,FREQ=0 *NODE PRINT,NSET=SAMPLE,FREQ=6 POR, *NODE FILE,NSET=SAMPLE,FREQ=6 POR, *OUTPUT,FIELD, OP=NEW,Frequency=6 *NODE OUTPUT POR, *OUTPUT,HISTORY,OP=ADD,Frequency=6 *NODE OUTPUT,NSET=SAMPLE POR, *ENDSTEP