I'm working with someone that is struggling with the difference between the angle of attack of an airfoil and the angle of attack of a wing. I've done a horrible job at explaining it to them and was wondering if anyone had a good definition or way of explaining the two so that I could explain it...
I'm looking for the shear stress for Grade 1 titanium
Mil-handbook 5 does not give this value but does give tensile stress allowable, 35 ksi and I know the poisson's ratio, .37
Is it possible to calculate Fsu or is there somewhere else I can find this value.