Theory of Structures

If the normal stresses due to longitudinal and transverse loads on a bar are σ₁ and σ₂ respectively, the tangential component of the stress on an inclined plane through θ°, the longitudinal load is

A σ₁ sin θ + σ₂ cos θ

B σ₁ sin θ² + σ₂ cos² θ

C

D

ANS:C -

Agreed, Thanks @Rohan.

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