Curved cantilever type beam (Cessna 150 Landing gear) Finite Element Calculations
Curved cantilever type beam (Cessna 150 Landing gear) Finite Element Calculations
(OP)
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.
Many thanks in advance.
RE: Curved cantilever type beam (Cessna 150 Landing gear) Finite Element Calculations
Cheers
Greg Locock
New here? Try reading these, they might help FAQ731-376: Eng-Tips.com Forum Policies http://eng-tips.com/market.cfm?
RE: Curved cantilever type beam (Cessna 150 Landing gear) Finite Element Calculations
thanks
RE: Curved cantilever type beam (Cessna 150 Landing gear) Finite Element Calculations
http://smath.info/wiki/Default.aspx?Page=Examples&...
for the whole page
Cheers
Greg Locock
New here? Try reading these, they might help FAQ731-376: Eng-Tips.com Forum Policies http://eng-tips.com/market.cfm?