Unformatted text preview: gust loading etc. The three critical load cases for this component are thought to be: Load case N x (kN/m) N y S xy 1 +250 -500 +200 2 +300 +500 -400 3 +600 -300 0 Calculate the required thickness of the wing skin for this component so that it will survive all three loading conditions. Assume that the material obeys Von Mises Yield criterion, assume that the out of plane (z direction) loading is negligible) and apply a factor of safety of 1.5 to your results....
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- Fall '05
- Fixed-wing aircraft, Yield surface, Von Mises yield criterion