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I've got a question regarding what the industry standard way is to apply air loads to flight control surfaces such as ailerons that have the typical sheetmetal skin/ ribs/spar design. On the project I'm working on, the loads are applied directly to the ribs/spars in the loads FEM, and nothing...

I've seen the term "bypass stress" used in threads regarding stresses around holes. What is bypass stress?

Hello, I have a question concerning end fixity of floor beams. Am I correct in interpreting end fixity as the ratio of the end rotation of the beam when subject to a unit moment (theta1 = L / 3EI) to the sum of theta1 and the rotation of the end support when subject to a unit moment (theta2 =...