FEATool Multiphysics
v1.17.0
Finite Element Analysis Toolbox
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EX_AXISTRESSSTRAIN5 Axisymmetric vibration modes of a hollow cylinder.
[ FEA, OUT ] = EX_AXISTRESSSTRAIN5( VARARGIN ) Axisymmetric vibration modes of a hollow cylinder (NAFEMS Free Vibration Benchmark 41).
[1] F. Abassian, D.J. Dawswell, and N.C. Knowles, Free Vibration Benchmarks, Volume 3, NAFEMS, Glasgow, 1987.
Accepts the following property/value pairs.
Input Value/{Default} Description ----------------------------------------------------------------------------------- igrid scalar 0/{2} Cell type (>0=quadrilaterals, <0=triangles) sfun string {sflag1} Shape function iplot scalar 0/{1} Plot solution (=1) . Output Value/(Size) Description ----------------------------------------------------------------------------------- fea struct Problem definition struct out struct Output struct
cOptDef = { 'igrid', 2; 'sfun', 'sflag1'; 'iplot', 1; 'tol', 0.01; 'fid', 1 }; [got,opt] = parseopt(cOptDef,varargin{:}); fid = opt.fid; E = 2e11; nu = 0.3; rho = 8000; % Geometry definition. fea.sdim = {'r' 'z'}; gobj = gobj_rectangle( 1.8, 2.2, 0, 10, 'R1' ); fea.geom.objects = { gobj }; fea.grid = rectgrid( abs(opt.igrid)*2, abs(opt.igrid)*50, [ 1.8, 2.2; 0, 10 ]); if( opt.igrid<0 ) fea.grid = quad2tri( fea.grid ); end % Equations and problem definition. fea = addphys( fea, @axistressstrain ); fea.phys.css.eqn.coef{1,end} = { nu }; fea.phys.css.eqn.coef{2,end} = { E }; fea.phys.css.eqn.coef{3,end} = { rho }; fea.phys.css.sfun = { opt.sfun, opt.sfun }; % Solve problem. fea = parsephys( fea ); fea = parseprob( fea ); [fea.sol.u,fea.sol.l] = solveeig( fea, 'fid', fid ); % Postprocessing. if( opt.iplot>0 ) postplot( fea, 'surfexpr', 'sqrt((r*u)^2+w^2)', 'solnum', 2 ) end out = []; f = sqrt(max(0,fea.sol.l))/(2*pi); f_ref = [ 0; 243.773387; 378.534723; 394.046384; 397.467494; 405.041753 ]; out.err = norm(f_ref-f)/norm(f_ref); out.pass = out.err < opt.tol; if( nargout==0 ) clear fea out end