Question: A sheet panel, 6 x 1 2 x 0 . 0 6 3 is make of 2 0 2 4 - T 3 alloy and
A sheet panel, x x is make of T alloy and has all edges clamped. The panel is subjected to a combined compression and shear loads that produce a compressive stress of psi and shear stress of psi. Will the sheet buckle under the given loads? What is the margin of safety?
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