Discussion :: GATE Aeronautical Engineering
- 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
|
A.
α =σo /2 ; β = 0; γ =σo /2.
|
|
B.
α =σo; β = 0; γ =σo
|
|
C.
α = 0; β =σo / 4; γ = 0
|
|
D.
α = 0; β =σo / 2; γ = 0
|
Whatsapp
Facebook
Answer : Option A
Explanation :
-NA-
Be The First To Comment