FEATool Multiphysics
v1.17.1
Finite Element Analysis Toolbox
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EX_PLANESTRESS6 Plane stress analysis of a pressure vessel.
[ FEA, OUT ] = EX_PLANESTRESS6( VARARGIN ) Model example for plain stress approximation of a pressure vessel (annular cross section with symmetry).
Accepts the following property/value pairs.
Input Value/{Default} Description ----------------------------------------------------------------------------------- E scalar {207e9} Modulus of elasticity nu scalar {0.27} Poissons ratio sfun string {sflag1} Shape function for displacements iplot scalar 0/{1} Plot solution (=1) . Output Value/(Size) Description ----------------------------------------------------------------------------------- fea struct Problem definition struct out struct Output struct
cOptDef = { ... 'E', 207e9; ... 'nu', 0.27; ... 'sfun', 'sflag1'; ... 'iplot', 1; ... 'igrid', 1; ... 'tol', 0.1; ... 'fid', 1 }; [got,opt] = parseopt( cOptDef, varargin{:} ); fid = opt.fid; % Geometry and grid. fea.sdim = { 'x' 'y' }; % Coordinate names. fea.grid = ringgrid( 12, 216, 100e-3, 120e-3 ); fea.grid = delcells( fea.grid, selcells( fea.grid, '(x<=eps) | (y<=eps)') ); if( opt.igrid~=1 ) fea.grid = quad2tri( fea.grid ); end n_bdr = max(fea.grid.b(3,:)); % Number of boundaries. % Problem definition. fea = addphys( fea, @planestress ); fea.phys.pss.eqn.coef{1,end} = { opt.nu }; fea.phys.pss.eqn.coef{2,end} = { opt.E }; fea.phys.pss.sfun = { opt.sfun opt.sfun }; % Boundary conditions. bctype = mat2cell( zeros(2,n_bdr), [1 1], ones(1,n_bdr) ); bctype{1,4} = 1; bctype{2,3} = 1; fea.phys.pss.bdr.coef{1,5} = bctype; bccoef = mat2cell( zeros(2,n_bdr), [1 1], ones(1,n_bdr) ); bccoef{1,1} = '-nx*1e4'; bccoef{2,1} = '-ny*1e4'; fea.phys.pss.bdr.coef{1,end} = bccoef; % Parse and solve problem. fea = parsephys( fea ); fea = parseprob( fea ); % Check and parse problem struct. fea.sol.u = solvestat( fea, 'fid', fid, 'icub', 1+str2num(strrep(opt.sfun,'sflag','')) ); % Call to stationary solver. % Postprocessing. s_disp = fea.phys.pss.eqn.vars{2,end}; if( opt.iplot>0 ) figure postplot( fea, 'surfexpr', s_disp ) title( 'Total displacement' ) end % Error checking. s_sx = fea.phys.pss.eqn.vars{5,end}; s_sy = fea.phys.pss.eqn.vars{6,end}; s_sxy = fea.phys.pss.eqn.vars{7,end}; s_sp1 = fea.phys.pss.eqn.vars{8,end}; s_sp3 = fea.phys.pss.eqn.vars{10,end}; s_ez = fea.phys.pss.eqn.vars{13,end}; s_ep1 = fea.phys.pss.eqn.vars{15,end}; s_ep2 = fea.phys.pss.eqn.vars{16,end}; s_ep3 = fea.phys.pss.eqn.vars{17,end}; v_disp = evalexpr( s_disp, [100e-3 120e-3-2*sqrt(eps);0 0]+sqrt(eps), fea )'; v_dref = [2.809e-8 2.635e-8]; [v_sx(1),v_sx(2)] = minmaxsubd( s_sx, fea ); v_sxref = [-10000 55454]; [v_sy(1),v_sy(2)] = minmaxsubd( s_sy, fea ); v_syref = [-10000 55454]; [v_sxy(1),v_sxy(2)] = minmaxsubd( s_sxy, fea ); v_sxyref = [-32730 0]; [v_sp1(1),v_sp1(2)] = minmaxsubd( s_sp1, fea ); v_sp1ref = [4.5e4 55454]; [v_sp3(1),v_sp3(2)] = minmaxsubd( s_sp3, fea ); v_sp3ref = [-1e4 0]; [v_ez(1),v_ez(2)] = minmaxsubd( s_ez, fea ); v_ezref = [-5.929e-8 -5.929e-8]; [v_ep1(1),v_ep1(2)] = minmaxsubd( s_ep1, fea ); v_ep1ref = [2.196e-7 2.809e-7]; [v_ep2(1),v_ep2(2)] = minmaxsubd( s_ep2, fea ); v_ep2ref = [-5.929e-8 -5.929e-8]; [v_ep3(1),v_ep3(2)] = minmaxsubd( s_ep3, fea ); v_ep3ref = [-1.206e-7 -5.929e-8]; out.err = [ abs([v_dref-v_disp])./v_dref ; abs([v_sxref-v_sx])./v_sxref ; abs([v_syref-v_sy])./v_syref ; abs([v_sxyref(1)-v_sxy(1)])./v_sxyref(1) 0 ; abs([v_sp1ref(2)-v_sp1(2)])./v_sp1ref(2) 0 ; abs([v_sp3ref(1)-v_sp3(1)])./v_sp3ref(1) 0 ; abs([v_ezref(1)-v_ez(1)])./v_ezref(1) 0 ; abs([v_ep1ref(1)-v_ep1(1)])./v_ep1ref(1) 0 ; abs([v_ep2ref(1)-v_ep2(1)])./v_ep2ref(1) 0 ; abs([v_ep3ref(1)-v_ep3(1)])./v_ep3ref(1) 0 ]; out.pass = all( out.err(:) <= opt.tol ); if( nargout==0 ) clear fea out end