FEM-Course-Matlab/6.桁架结构matlab有限元编程/Truss2D/Truss2DFEA.m

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2.7 KiB
Mathematica
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2024-01-28 16:46:36 +00:00
%**************************************************************************
function [U, Strain, Stress, AxialForce]=PlaneTrussFEA(x,y,ele,Load,Constr,Scale)
Dofs=2*size(x,2); %<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ɶ<EFBFBD><EFBFBD><EFBFBD>
EleCount=size(ele,1); %<EFBFBD><EFBFBD>Ԫ<EFBFBD><EFBFBD><EFBFBD><EFBFBD>
K=zeros(Dofs,Dofs); %<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>նȾ<EFBFBD><EFBFBD><EFBFBD>
F=zeros(Dofs,1); %<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>غ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
U=zeros(Dofs,1); %<EFBFBD><EFBFBD><EFBFBD><EFBFBD>λ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
BarLength=BarsLength(x,y,ele);
figure('Name','Undeformed Truss')
RenderTruss(ele,Load,Constr,x,y,U,1,'-k',1) %<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
figure('Name','Deformed Truss')
RenderTruss(ele,Load,Constr,x,y,U,0.5,'-k',1) %<EFBFBD><EFBFBD><EFBFBD>Ʊ<EFBFBD><EFBFBD>κ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
hold on
%<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>е<EFBFBD>Ԫ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>Ԫ<EFBFBD>ն<EFBFBD><EFBFBD><EFBFBD><EFBFBD>ֿ<EFBFBD><EFBFBD><EFBFBD>װ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ն<EFBFBD><EFBFBD><EFBFBD>
for iEle =1:EleCount
%<EFBFBD>õ<EFBFBD>Ԫ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ڵ<EFBFBD><EFBFBD>ı<EFBFBD><EFBFBD><EFBFBD>
n1=ele(iEle,2);n2=ele(iEle,3);
%<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
R=CoordTransform([x(n1) x(n2)],[y(n1) y(n2)],BarLength(iEle));
%<EFBFBD><EFBFBD><EFBFBD>Ԫ<EFBFBD>նȾ<EFBFBD><EFBFBD><EFBFBD> Ke=R'*ke*R;<EFBFBD>ֲ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ϵ<EFBFBD>µĵ<EFBFBD>Ԫ<EFBFBD>ն<EFBFBD><EFBFBD><EFBFBD>ת<EFBFBD><EFBFBD>Ϊȫ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>µĵ<EFBFBD>Ԫ<EFBFBD>ն<EFBFBD><EFBFBD><EFBFBD>
ke= BarElementKe(ele(iEle,4),ele(iEle,5),R,BarLength(iEle));
%<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>Ԫ<EFBFBD>նȷֿ<EFBFBD><EFBFBD><EFBFBD>װ<EFBFBD><EFBFBD><EFBFBD>ܸ<EFBFBD><EFBFBD><EFBFBD>Ӧλ<EFBFBD><EFBFBD>
K(2*n1-1:2*n1,2*n1-1:2*n1)=K(2*n1-1:2*n1,2*n1-1:2*n1)+ke(1:2,1:2);
K(2*n1-1:2*n1,2*n2-1:2*n2)=K(2*n1-1:2*n1,2*n2-1:2*n2)+ke(1:2,3:4);
K(2*n2-1:2*n2,2*n1-1:2*n1)=K(2*n2-1:2*n2,2*n1-1:2*n1)+ke(3:4,1:2);
K(2*n2-1:2*n2,2*n2-1:2*n2)=K(2*n2-1:2*n2,2*n2-1:2*n2)+ke(3:4,3:4);
end
%<EFBFBD>γ<EFBFBD><EFBFBD>غ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>--1<EFBFBD><EFBFBD>2<EFBFBD><EFBFBD>3<EFBFBD><EFBFBD>4<EFBFBD><EFBFBD><EFBFBD>ɶȸ<EFBFBD><EFBFBD>غ<EFBFBD>ֵ
for LoadNum=1:size(Load,1)
for i=2:3
F(2*Load(LoadNum)+i-3,1)=Load(LoadNum,i);
end
end
%ʩ<EFBFBD><EFBFBD>Լ<EFBFBD><EFBFBD>--<EFBFBD>˴<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
for iConstr=1:size(Constr,1)
for j=2:3
if ~isnan(Constr(iConstr,j))
K(2*Constr(iConstr,1 )+j-3,2*Constr(iConstr,1 )+j-3)=...
1e12*K(2*Constr(iConstr,1 )+j-3,2*Constr(iConstr,1 )+j-3);
F(2*Constr(iConstr,1)+j-3)=1e12*Constr(iConstr,j)*...
K(2*Constr(iConstr,1 )+j-3,2*Constr(iConstr,1)+j-3);
end
end
end
U=K\F; %ȫ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ϵ<EFBFBD><EFBFBD>λ<EFBFBD><EFBFBD>,<EFBFBD>˴<EFBFBD>ԭ<EFBFBD><EFBFBD>Ϊ<EFBFBD><EFBFBD>Ǿ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ʸij<EFBFBD>α<EFBFBD><EFBFBD>
for iEle =1:EleCount
%<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>˾ֲ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>µ<EFBFBD>λ<EFBFBD><EFBFBD>
n1=ele(iEle,2);n2=ele(iEle,3);
R=CoordTransform([x(n1) x(n2)],[y(n1) y(n2)],BarLength(iEle));
localU = R*[U(2*n1-1:2*n1,1);U(2*n2-1:2*n2,1)];
Strain(1, iEle)=[-1/BarLength(iEle) 1/BarLength(iEle)]*localU; %Ӧ<EFBFBD><EFBFBD>
Stress(1, iEle)=ele(iEle,5)* Strain(1, iEle); %Ӧ<EFBFBD><EFBFBD>
AxialForce(1, iEle)=ele(iEle,4)* Stress(1, iEle); %<EFBFBD><EFBFBD><EFBFBD><EFBFBD>
end
%<EFBFBD><EFBFBD><EFBFBD><EFBFBD>λ<EFBFBD>ƣ<EFBFBD>Ӧ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ı<EFBFBD><EFBFBD>ļ<EFBFBD>
fp=fopen('Result.txt','a');
str = [char(13,10)','U',' ',num2str(U'),char(13,10)','Stress',' ',...
num2str(Stress),char(13,10)','AxialForce',' ',num2str(AxialForce)];
fprintf(fp,str);
fclose(fp);
RenderTruss(ele,Load,Constr,x,y,U,1,'-.b',Scale) %<EFBFBD><EFBFBD><EFBFBD>Ʊ<EFBFBD><EFBFBD>κ<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>
figure
AxisForcePlot(ele,Load,Constr,x,y,U,3,'-b',Scale,AxialForce)%<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>ͼ
end %<EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD><EFBFBD>