*HEADING Procedure tests for *DISTRIBUTION and *ELEMENT PROPERTIES element SAXA22 *NODE,NSET=NALL 1, 0., 0. 2, 0.5, 0. 3, 1., 0. 4, 1.5, 0. 5, 2., 0. 6, 2.5, 0. 7, 3., 0. 8, 3.5, 0. 9, 4., 0. *Elset, elset=shellSec1 1, **--------------------------------------------------------------------- *Element,TYPE=SAXA22,elset=eall, offset=100 1, 1, 2, 3 2, 3, 4, 5 3, 5, 6, 7 4, 7, 8, 9 **--------------------------------------------------------------------- *SHELL SECTION,MATERIAL=MAT1, ELSET=eall, orientation=ori, offset=distOffset, shell thickness=distThick .1, **--------------------------------------------------------------------- *Distribution Table, name=orientationTable coord3d, coord3d *Distribution, name=distOrient, location=element, table=orientationTable , 0.1000000E+01, 0.0000000E+00, 0.0000000E+00, 0.0000000E+00, 0.1000000E+01, 0.0000000E+00 1, 0.1000000E+01, 0.0000000E+00, 0.0000000E+00, 0.0000000E+00, 0.1000000E+01, 0.0000000E+00 2, 0.9993908E+00, 0.3489950E-01, 0.0000000E+00, -0.3489950E-01, 0.9993908E+00, 0.0000000E+00 3, 0.9961947E+00, 0.8715574E-01, 0.0000000E+00, -0.8715574E-01, 0.9961947E+00, 0.0000000E+00 4, 0.9902681E+00, 0.1391731E+00, 0.0000000E+00, -0.1391731E+00, 0.9902681E+00, 0.0000000E+00 *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, *Distribution Table, name=OriAngleTable angle *Distribution, name=distOriAngle, location=element, table=OriAngleTable , 0.0, 1, -0.5 2, -0.5 3, -1.0 4, -1.0 *orientation, name=ori distOrient 3, distOriAngle **--------------------------------------------------------------------- *NSET,NSET=EDGE 9, 109, 209 *NSET,NSET=CENTER 1, 101, 201 *NSET,NSET=MID 5, 105, 205 *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, *Conductivity 1000., *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 *Boundary CENTER,2,,0.1 *end load case *load case, name=load2 *Boundary EDGE,6,,0.2 *end load case *load case, name=load3 *Boundary MID,6,,-0.1 *end load case *end step