A sheet of aluminum is stretched in the xy-plane. If the strains in the sheet are ϵx = 0.3 x10-3 and ϵy = 0.25 x10-3, compute σx and σy. Use E = 110 GPa and v = 0.35.

Structural Analysis
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Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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A sheet of aluminum is stretched in the xy-plane. If the strains in the sheet are ϵx = 0.3 x10-3 and ϵy = 0.25 x10-3, compute σx and σy. Use E = 110 GPa and v = 0.35.

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