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FEATool Multiphysics
v1.17.2
Finite Element Analysis Toolbox
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FEATool Multiphysics
v1.17.2
Finite Element Analysis Toolbox
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EX_LINEARELASTICITY3 Parametric study for the bracket deflection model.
[ FEA, OUT ] = EX_LINEARELASTICITY3( VARARGIN ) Example to conduct parametric study of maximum stresses for the bracket deflection model.
Input Value/{Default} Description
-----------------------------------------------------------------------------------
thickness [0.035 0.03 0.025 0.02] Plate thickness
loads [1e4 2e4 1e5 1e6] Applied loads.
.
Output Value/(Size) Description
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fea struct Problem definition struct
out struct Output struct
thickness = [ 0.035 0.03 0.025 0.02 ];
loads = [ 1e4 2e4 1e5 1e6 ];
%% Starting new model.
fea.sdim = { 'x', 'y', 'z' };
fea = addphys( fea, @linearelasticity, { 'u', 'v', 'w' } );
for i=1:length(thickness)
%% Geometry operations.
fea.geom = struct;
gobj = gobj_block( 0, 0.02, 0, 0.2, 0, 0.2, 'B1' );
fea = geom_add_gobj( fea, gobj );
gobj = gobj_block( 0, 0.2, 0, 0.2, 0.1-thickness(i)/2, 0.1+thickness(i)/2, 'B1' );
fea = geom_add_gobj( fea, gobj );
gobj = gobj_cylinder( [ 0.1, 0.1, 0.08 ], 0.08, 0.04, 3, 'C1' );
fea = geom_add_gobj( fea, gobj );
fea = geom_apply_formula( fea, 'B1+B2-C1' );
%% Grid operations.
fea.grid = gridgen( fea, 'hmax', thickness(i)/2 );
for j=1:length(loads)
%% Equation settings.
fea.phys.el.dvar = { 'u', 'v', 'w' };
fea.phys.el.sfun = { 'sflag1', 'sflag1', 'sflag1' };
fea.phys.el.eqn.coef = { 'nu_el', 'nu', 'Poissons ratio', { '0.3' };
'E_el', 'E', 'Modulus of elasticity', { '200e9' };
'Fx_el', 'F_x', 'Body load in x-direction', { '0' };
'Fy_el', 'F_y', 'Body load in y-direction', { '0' };
'Fz_el', 'F_z', 'Body load in z-direction', { '0' };
'u0_el', 'u0', 'Initial condition for u', { '0' };
'v0_el', 'v0', 'Initial condition for v', { '0' };
'w0_el', 'w0', 'Initial condition for w', { '0' } };
fea.phys.el.eqn.seqn = { 'u'' - ((E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*ux_x + (E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy_x + (E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz_x + (E_el/(1+nu_el)/2)*(uy_y+vx_y) + (E_el/(1+nu_el)/2)*(uz_z+wx_z)) = Fx_el', 'v'' - ((E_el/(1+nu_el)/2)*(uy_x+vx_x) + (E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux_y + (E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*vy_y + (E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz_y + (E_el/(1+nu_el)/2)*(vz_z+wy_z)) = Fy_el', 'w'' - ((E_el/(1+nu_el)/2)*(uz_x+wx_x) + (E_el/(1+nu_el)/2)*(vz_y+wy_y) + (E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux_z + (E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy_z + (E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*wz_z) = Fz_el' };
fea.phys.el.eqn.vars = { 'von Mieses stress', 'sqrt(((E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*ux+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz)^2+((E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux+(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*vy+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz)^2+((E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy+(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*wz)^2-((E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*ux+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz)*((E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux+(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*vy+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz)-((E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux+(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*vy+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz)*((E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy+(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*wz)-((E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*ux+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz)*((E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy+(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*wz)+3*((E_el/(1+nu_el)/2)*(uy+vx))^2+3*((E_el/(1+nu_el)/2)*(vz+wy))^2+3*((E_el/(1+nu_el)/2)*(uz+wx))^2)';
'x-displacement', 'u';
'y-displacement', 'v';
'z-displacement', 'w';
'Stress, x-component', '(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*ux+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz';
'Stress, y-component', '(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux+(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*vy+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*wz';
'Stress, z-component', '(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*ux+(E_el/((1+nu_el)*(1-2*nu_el))*nu_el)*vy+(E_el/((1+nu_el)*(1-2*nu_el))*(1-nu_el))*wz';
'Stress, xy-component', '(E_el/(1+nu_el)/2)*(uy+vx)';
'Stress, yz-component', '(E_el/(1+nu_el)/2)*(vz+wy)';
'Stress, zx-component', '(E_el/(1+nu_el)/2)*(uz+wx)';
'Displacement field', { 'u', 'v', 'w' } };
%% Constants and expressions.
fea.expr = { 'load', loads(j) };
%% Boundary settings.
n_bdr = max(fea.grid.b(3,:));
ind_fixed = findbdr( fea, 'x<0.005' );
ind_load = findbdr( fea, 'x>0.19' );
fea.phys.el.bdr.sel = ones(1,n_bdr);
% Fix right boundary (set zero Dirichlet BCs).
n_bdr = max(fea.grid.b(3,:)); % Number of boundaries.
bctype = num2cell( zeros(3,n_bdr) ); % First set homogenous Neumann BCs everywhere.
[bctype{:,ind_fixed}] = deal( 1 ); % Set Dirchlet BCs for right boundary.
fea.phys.el.bdr.coef{1,5} = bctype;
% Apply negative z-load to left outer boundary.
bccoef = num2cell( zeros(3,n_bdr) );
[bccoef{3,ind_load}] = deal( '-load' );
fea.phys.el.bdr.coef{1,end} = bccoef;
%% Solver call.
fea = parsephys( fea );
fea = parseprob( fea );
fea.sol.u = solvestat( fea );
%% Postprocessing.
s_vm = fea.phys.el.eqn.vars{1,2};
vm_stress = evalexpr( s_vm, fea.grid.p, fea );
max_vm_stress(i,j) = max(vm_stress);
end
end
%% Visualization.
[t,l] = meshgrid(thickness,loads);
surf( t, l, max_vm_stress, log(max_vm_stress) )
xlabel('Thickness')
ylabel('Load')
zlabel('Maximum stress')
view(45,30)
out = max_vm_stress;
if ( nargout==0 )
clear fea out
end