Structures·MCQ explained

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

Try it first: pick an option, then read the explanation.

Correct answer: C. (σ₁ − σ₂) sin 2θ / 2

Asked in SSC JE 24/01/2018 (Evening)

Detailed Explanation

Each normal stress produces a shear component on the inclined plane, but in opposite senses, so the shear depends on the difference σ₁ − σ₂.

\[ \tau = \sigma_1\sin\theta\cos\theta - \sigma_2\sin\theta\cos\theta = \frac{\sigma_1 - \sigma_2}{2}\sin 2\theta \]

Why “(σ₁ − σ₂) sin 2θ / 2” Is Correct

The tangential component is (σ₁ − σ₂) sin 2θ / 2. It is maximum at θ = 45°, giving (σ₁ − σ₂)/2.

σ₁σ₁σ₂σ₂θinclined plane
Biaxial normal stresses σ₁ and σ₂ with an inclined plane at θ: the shear on that plane is ((σ₁ − σ₂)/2) sin 2θ.

Why the Other Options Are Wrong

  • A. σ₁ sinθ + σ₂ cosθ: First powers of sin and cos do not appear in stress transformation.
  • B. σ₁ sin²θ + σ₂ cos²θ: This is the normal component σn.
  • D. (σ₁ + σ₂) sin 2θ / 2: The shear depends on the difference, not the sum, of the stresses.

Key Point

Biaxial: τθ = ((σ₁ − σ₂)/2) sin 2θ; zero when σ₁ = σ₂.

Key Concepts for Students

  • Equal biaxial stress ⇒ no shear on any plane.
  • σ₂ = −σ₁ ⇒ τmax = σ₁ (pure shear).
  • τmax = radius of Mohr's circle.

Practice more: this is question 11 in Principal Stress and Principal Planes MCQs – Part 1. Try the whole set and check every answer instantly.