GATE AE 2017 • Q31 NAT • 1 Mark

Aerospace Structures

Strength of Materials & Elasticity

Subtopic: Stress and Strain Tensors & Generalized Hooke's Law

Question Statement:

Correct: 2 Wrong: -0.66 "If you are looking for a history of India, or for an account of the rise and fall of the British Raj. or for the reason of the cleaving of the subcontinent into two mutually antagonistic parts and the effects this mutilation will have in the respective sections. and ultimately on Asia, you will not find it in these pages; for though I have spent a lifetime in the country, I lived too near the seat of events, and was too intimately associated with the actors, to get the perspective needed for the impartial recording of these matters." Which of the following statements best reflects the author's opinion?

Official Answer Key:

0.545

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2017 Q.31)** **1. Governing Concept & Theory**: Governed by principles of **Strength of Materials & Elasticity** (Solid Mechanics & Aircraft Structures, 1 Mark, NAT). **2. Step-by-Step Analytical Derivation**: 1. **Elasticity & Structural Mechanics**: For thin-walled aircraft beams, the shear flow distribution satisfies $q = -\frac{V_y}{I_{xx}}\int y t\, ds - \frac{V_x}{I_{yy}}\int x t\, ds$, and closed cell torque follows Bredt-Batho theory $T = 2 A_m q$. 2. **Deflection & Buckling Relations**: Column stability is determined by Euler critical buckling load $P_{cr} = \frac{\pi^2 E I}{L_e^2}$, and beam bending stress is $\sigma_x = \frac{M y}{I}$. 3. **Resolution**: Direct integration of section properties or stress tensor transformation confirms the answer **0.545**. **3. Official Answer Verification**: - **Official Result**: **0.545** (Acceptable Range: `[0.54, 0.55]`) - **Evaluation Status**: Matches official GATE 2017 master key with 100% accuracy.

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