The overall structure will be built with carbon fiber and a combination of composite materials that suite the different areas of the aircraft. The airplane has a gross weight of 3200lbs. and should meet the requirements of FAR 23
Berkshire,
You are the only one who answered with sensible questions. The original design is made from spruce, birch and mahogany. It is a box spar. The spar is designed with an upper and lower superior and inferior spar with diphrams in between the upper and lower superior and inferior spars...
I am building a 3/4 P-51 mustang and the original design was of wood. I am bulding it out of composite materials and want to replace the wooden spar with a composte one, made out of carbon fiber and either a honeycomb core or foam core. I need help with the structural sizing of the spar. If...
