code for fem -constrained bar

I was trying to write a code for a horizontal two step bar constrained at both ends to determine its deflection at the three nodes and reactionary forces at the ends.At node 2 an axial force of 2kN is applied.I am clueless how to go about writing the code.Everytime I run it an error pops up.Can somebody guide me
% static analysis
%material properties
E=[70e9,200e9];
%Geometry
L=700e-3;
A=[2400e-6,600e-6];
q0=0;
%Element mesh
ne=2; %no.of elements
nn=3; %no.of nodes
dof=1; %degrees of freedom per node
tdof=dof*nn; % total degree of freedom
le=[300e-3,400e-3]; %length of elements
% Initialization of Global Matrices
KG=zeros(tdof,tdof); %global stiffness matrix
FG = zeros(tdof,1); % global load vector
%assembly of global matrices
for i= 1:ne
Ke(i)=(E(i)*A(i)/le(i))*[1 -1;-1 1]; % element stiffness matrix
Fe=(q0*le(i)/2)*[1;1]; % element load vector for udl
for j=1:2
for k=1:2
KG(CONN(i,j),CONN(i,k))= KG(CONN(i,j),CONN(i,k))+Ke(i);
end
FG(CONN(i,j),1)= FG(CONN(i,j),1)+Fe(i,j);
end
end
CONN=[1 2;2 3];
KG(1,:)=0;
KG(:,1)=0;
KG(1,1)=1;
KG(3,:)=0;
KG(:,3)=0;
KG(3,3)=0;
FG(3,1)=0;
For m=[1,3];
KG(m,:)=0;
KG(:,m)=0;
KG(m,m)=1;
FG(m,1)=0;
End
UG=linsolve(KG,FG);

6 个评论

What does it mean?
constrained nodes where deflection is zero
This instruction doesn't work (somehow)
Did it work for you?
no and I am looking for clues in this forum
These two statements look familiar for me
What do you think?
The first one is for element stiffness matrix
and second is reduced or condensed global stiffness matrix after imposition of boundary conditions

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