RolandW
Mechanical
- Jul 13, 2005
- 3
Hello everyone. I am pogramming some software for a 1D FEA of a thin beam with multiple pinned supports and loads. It's ends are always free.
I have managed to assemble the global stiffness matrix, but I am not sure how to set the boundary conditions which is needed to make it non-singular. The matrix form is:
F1 v1
M1 u1
F2 = K * v2
M2 u2
. .
. .
. .
where K is the stiffness matrix, F is force, M momentum, v displacement and u rotation angle. Obviously I want to solve it for v and u.
A pinned support should have the deflection v = 0, so I guess that I could at least remove these columns? But what rows should I remove so that the system is not over-constrained? Does it matter?
I am a total newbie when it comes to finite elements, so forgive me if the question is badly formulated. Thanks in advance.
I have managed to assemble the global stiffness matrix, but I am not sure how to set the boundary conditions which is needed to make it non-singular. The matrix form is:
F1 v1
M1 u1
F2 = K * v2
M2 u2
. .
. .
. .
where K is the stiffness matrix, F is force, M momentum, v displacement and u rotation angle. Obviously I want to solve it for v and u.
A pinned support should have the deflection v = 0, so I guess that I could at least remove these columns? But what rows should I remove so that the system is not over-constrained? Does it matter?
I am a total newbie when it comes to finite elements, so forgive me if the question is badly formulated. Thanks in advance.