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what loads are developed in the wing of a biplane.?
to determine the wall thickness of the material I need to use I need to find the force applied on each member. I can take that info to a simple column strength calculation. I have included a view of a biwing assembly.
http://www.msplinks.com/MDFodHRwOi8vczYzMy5waG90b2...
it is shown from the front. There are two sets of struts one at the front spar and another set at the rear spar. The CL of the wing is at 30 percent of chord. The gross weight of craft and payload is 500 pounds. overall length of the wing half is 17 feet. Chord is 48 inches.
sorry the inside and outside bay have a flying wire angle of 45 degrees. the middle bay has an angle of 39 degrees from horizontal
1 Answer
- 1 decade agoFavorite Answer
hi,
I was not able to open above link. i honestly have no idea with planes.
hopfully you can get the right answer from someone familiar with this field.
good luck