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Question
The Airy stress function, φ =α x2 +β xy +γ y2 for a thin square panel of size l ×l automatically satisfies compatibility. If the panel is subjected to uniform tensile stress, σo on all four edges, the traction boundary conditions are satisfied by
Options:
A .  Î± =σo /2 ; β = 0; γ =σo /2.
B .  Î± =σo; β = 0; γ =σo
C .  Î± = 0; β =σo / 4; γ = 0
D .  Î± = 0; β =σo / 2; γ = 0
Answer: Option A


-NA-



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