FEATool Multiphysics
v1.17.2
Finite Element Analysis Toolbox
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EX_POISSON4 2D Poisson equation example on a rectangle.
[ FEA, OUT ] = EX_POISSON4( VARARGIN ) Poisson equation on a rectangle with source term (1+2000^2) * pi^2 * sin(pi*x) * sin(2000*pi*y) and exact solution sin(pi*x) * sin(2000*pi*y). Accepts the following property/value pairs.
Input Value/{Default} Description ----------------------------------------------------------------------------------- igrid scalar 1/{0} Cell type (0=quadrilaterals, 1=triangles) lx scalar {1e-3} Length of domain in x-direction ly scalar {1e-3} Length of domain in y-direction hmax scalar {ly/20} Max grid cell size refsol string {sin(pi*x)*sin(2000*pi*y)} Reference solution fsrc string {(1+2000^2)*pi^2*sin(pi*x)*sin(2000*pi*y)} Source term sfun string {sflag1} Shape function iphys scalar 0/{1} Use physics mode to define problem (=1) or directly define fea.eqn/bdr fields (=0) iplot scalar 0/{1} Plot solution (=1) . Output Value/(Size) Description ----------------------------------------------------------------------------------- fea struct Problem definition struct out struct Output struct
cOptDef = { ... 'igrid', 0; ... 'lx', 0.001; ... 'ly', 0.001; ... 'hmax', 0.001/20; ... 'refsol', 'sin(pi*x)*sin(2000*pi*y)'; ... 'fsrc', '(1+2000^2)*pi^2*sin(pi*x)*sin(2000*pi*y)'; ... 'sfun', 'sflag1'; ... 'iphys', 1; ... 'iplot', 1; ... 'fid', 1 }; [got,opt] = parseopt(cOptDef,varargin{:}); fid = opt.fid; % Geometry definition. gobj = gobj_rectangle( 0, opt.lx, 0, opt.lx ); fea.geom.objects = { gobj }; % Grid generation. switch opt.igrid case -1 fea.grid = rectgrid(round(opt.lx/opt.hmax),round(opt.lx/opt.hmax),[0 opt.lx;0 opt.lx]); fea.grid = quad2tri(fea.grid); case 0 fea.grid = rectgrid(round(opt.lx/opt.hmax),round(opt.lx/opt.hmax),[0 opt.lx;0 opt.lx]); case 1 fea.grid = gridgen(fea,'hmax',opt.hmax,'fid',fid); end fea.grid.p(2,:) = fea.grid.p(2,:)*opt.ly/opt.lx; % Scale y-coordinates. n_bdr = max(fea.grid.b(3,:)); % Number of boundaries. % Problem definition. fea.sdim = { 'x' 'y' }; % Coordinate names. if ( opt.iphys==1 ) fea = addphys(fea,@poisson); % Add Poisson equation physics mode. fea.phys.poi.sfun = { opt.sfun }; % Set shape function. fea.phys.poi.eqn.coef{3,4} = { opt.fsrc }; % Set source term coefficient. fea.phys.poi.bdr.coef{1,end} = repmat({opt.refsol},1,n_bdr); % Set Dirichlet boundary coefficient to reference solution. fea = parsephys(fea); % Check and parse physics modes. else fea.dvar = { 'u' }; % Dependent variable name. fea.sfun = { opt.sfun }; % Shape function. % Define equation system. fea.eqn.a.form = { [2 3;2 3] }; % First row indicates test function space (2=x-derivative + 3=y-derivative), % second row indicates trial function space (2=x-derivative + 3=y-derivative). fea.eqn.a.coef = { 1 }; % Coefficient used in assembling stiffness matrix. fea.eqn.f.form = { 1 }; % Test function space to evaluate in right hand side (1=function values). fea.eqn.f.coef = { opt.fsrc }; % Coefficient used in right hand side. % Define boundary conditions. fea.bdr.d = cell(1,n_bdr); [fea.bdr.d{:}] = deal(opt.refsol); % Assign reference solution to all boundaries (Dirichlet). fea.bdr.n = cell(1,n_bdr); % No Neumann boundaries ('fea.bdr.n' empty). end % Parse and solve problem. fea = parseprob(fea); % Check and parse problem struct. fea.sol.u = solvestat(fea,'fid',fid); % Call to stationary solver. % Postprocessing. s_err = ['abs(',opt.refsol,'-u)']; if ( opt.iplot>0 ) figure subplot(3,1,1) postplot(fea,'surfexpr','u','axequal','off') title('Solution u') subplot(3,1,2) postplot(fea,'surfexpr',opt.refsol,'axequal','off') title('Exact solution') subplot(3,1,3) postplot(fea,'surfexpr',s_err,'axequal','off','evalstyle','exact') title('Error') end % Error checking. if ( size(fea.grid.c,1)==4 ) xi = [0;0]; else xi = [1/3;1/3;1/3]; end err = evalexpr0(s_err,xi,1,1:size(fea.grid.c,2),[],fea); ref = evalexpr0('u',xi,1,1:size(fea.grid.c,2),[],fea); err = sqrt(sum(err.^2)/sum(ref.^2)); if( ~isempty(fid) ) fprintf(fid,'\nL2 Error: %f\n',err) fprintf(fid,'\n\n') end out.err = err; out.pass = out.err<0.1; if ( nargout==0 ) clear fea out end