Curved cantilever type beam (Cessna 150 Landing gear) Finite Element Calculations

[kgjuggy]

The image shown as an attachment with this post is the actual front view of the landing gear of Cessna 150. I am working on a project to calculate the stress and strain acting on the cantilever type variable cross-section beam. After dividing into 8 sections/elements, the dimensions have been jotted down. during a drop test the landing gear will tend to bend and come under stress/moment. can anyone help me how to work out the FEA calculations using the matrices based method or any other follow up.

Many thanks in advance.

 

[MiketheEngineer]

Double posting is rowned upon. Tag this doc and have the moderator remove it

 

[kgjuggy]

i am sorry but i didn't catch up that.