*HEADING Procedure tests for *DISTRIBUTION and *ELEMENT PROPERTIES element SAX1 *NODE,NSET=NALL 1, 0., 0. 2, 1., 0. 3, 2., 0. 4, 3., 0. 5, 4., 0. *Elset, elset=shellSec1 1, **--------------------------------------------------------------------- *Element, type=sax1,elset=eall 1, 1, 2 2, 2, 3 3, 3, 4 4, 4, 5 **--------------------------------------------------------------------- *SHELL SECTION,MATERIAL=MAT1, ELSET=eall, offset=distOffset, shell thickness=distThick .1, **--------------------------------------------------------------------- *Distribution Table, name=thicknessTable length *Distribution, name=distThick, location=element, table=thicknessTable , 0.1, 2, 0.2, 3, 0.3, 4, 0.4, *Distribution Table, name=offsetTable ratio *Distribution, name=distOffset, location=element, table=offsetTable , -0.05, 2, -0.05, 3, -0.025, 4, -0.025, **--------------------------------------------------------------------- *NSET,NSET=EDGE 5, *NSET,NSET=CENTER 1, *NSET,NSET=MID 3, *Material, name=MAT1 *Elastic, type=engineering constants 0.300E+07, 0.400E+07, 0.500E+07, 0.100E+00, 0.200E+00, 0.300E+00, 0.300E+06, 0.400E+06 0.500E+06, *Density 0.750E-03, *Damping, Alpha=0.5 **--------------------------------------------------------------------- *Boundary CENTER,1,1 EDGE,1,2 *psd-definition, name=white, type=force 1.0,0.1,0.0 1.0,0.1,60.0 *spectrum, name=spec,type=acceleration 0., 0., 0. 1.e7, 300., 0. 1.e7, 1000., 0. ** ** -------------------------------------------------- ** *step, name=step-1 frequency analysis *frequency, SIM=NO 5, *El print s, sf, ssavg, se, *Node print u, *Output, field *Node output u, *Element output s, sf, ssavg, sth, *end step ** ** -------------------------------------------------- ** *step, name=step-2 SSD mode-based *steady state dynamics, interval=eigenfrequency 60, *El print, freq=999 s, sf, ssavg, se, sth, *Node print, freq=999 u, *Output, field *Node output u, *Element output s, sf, ssavg, sth, *cload center,2,0.5 *select eigenmodes, generate 1, 5 *modal damping, rayleigh 1, 5, 0.5 *end step ** ** -------------------------------------------------- ** *step, name=step-3 modal dynamic *modal dynamic 0.1,1. *cload center,2,0.5 *select eigenmodes, generate 1, 5 *modal damping, rayleigh 1, 5, 0.5 *end step ** ** -------------------------------------------------- ** *step, name=step-4 SSD direct *steady state dynamics, direct, interval=eigenfrequency 60., *cload center,2,0.5 *end step ** ** -------------------------------------------------- ** *step, name=step-5 SSD subspace *steady state dynamics, subspace projection, interval=eigenfrequency 60., *cload center,2,0.5 *end step ** ** -------------------------------------------------- ** *step, name=step-6 random response *random response 60., *select eigenmodes, generate 1, 5 *cload, load case=1 center,2,0.5 *cload, load case=2 edge,6,0.2 *correlation, psd=white, type=uncorrelated, complex=no 1,1 2,1 *El print, freq=999 sf, se, *Node print, freq=999 u, *Output, field *Node output u, *Element output sf, *end step ** ** -------------------------------------------------- ** *step, name=step-7 response spectrum *response spectrum, sum=abs, comp=alg spec,0.,0.,1.,1. *select eigenmodes, generate 1, 5 *end step ** ** -------------------------------------------------- ** *step, nlgeom=yes, name=step-8 static *static 1.0, 1.0 *Boundary edge,6,6,0.1 *El print, freq=999 s, sf, ssavg, se, sth, *Node print, freq=999 u, *Output, field *Node output u, *Element output s, sf, ssavg, sth, *Output, history *Element output,elset=shellSec1 s11, sf1, ssavg1, se1, sk1, sth, *end step ** ** -------------------------------------------------- ** *step, perturbation, name=step-9 static *static *El print, freq=999 s, sf, ssavg, se, sth, *Node print, freq=999 u, *Output, field *Node output u, *Element output s, sf, ssavg, sth, *load case, name=load1 *dload eall, br, 1.e *end load case *load case, name=load2 *dload eall, grav, 1.e6, 0.,1.,0. *end load case *load case, name=load3 *dload eall, cent, 100.,0.,0.,0.,1.,0. *end load case *load case, name=load4 *dload eall, centrif, 1.e6,0.,0.,0.,1.,0. *end load case *end step