GATE AE 2021 • Q20 MCQ • 1 Mark Aerospace Structures

Aerospace Structures

Aerospace Materials & Fatigue

Subtopic: Composite Materials & Laminate Theory

Question Statement:

Two cantilever beams (Beam 1 and Beam 2) are made of the same homogeneous isotropic material and have identical length $L$. Beam 1 has a solid circular cross-section of radius $R$, while Beam 2 has a hollow circular cross-section with outer radius $R$ and inner radius $R/2$. If identical tip loads $P$ are applied, the ratio of the tip deflection of Beam 2 to that of Beam 1 ($\delta_2 / \delta_1$) is:

Options:

  • (A) 16/15
  • (B) 15/16
  • (C) 4/3
  • (D) 2

Official Answer Key:

A

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2021 Q.20 / AE Q.10)** **1. Intuitive Physical Setup & Given Parameters**: - Both beams: cantilever, length $L$, modulus $E$, tip load $P$. - Beam 1: Solid circular cross-section, radius $R$. - Beam 2: Hollow circular cross-section, outer radius $R_o = R$, inner radius $R_i = R/2$. **2. Step-by-Step Structural Mechanics Derivation**: 1. **Tip Deflection of Cantilever Beam**: \delta = \frac{P L^3}{3 E I} \implies \delta \propto \frac{1}{I} \frac{\delta_2}{\delta_1} = \frac{I_1}{I_2} 2. **Area Moment of Inertia for Beam 1 (Solid)**: I_1 = \frac{\pi R^4}{4} 3. **Area Moment of Inertia for Beam 2 (Hollow)**: I_2 = \frac{\pi}{4}(R_o^4 - R_i^4) = \frac{\pi}{4}\left(R^4 - \left(\frac{R}{2}\right)^4\right) = \frac{\pi}{4} R^4 \left(1 - \frac{1}{16}\right) = \frac{15}{16} \left(\frac{\pi R^4}{4}\right) = \frac{15}{16} I_1 4. **Evaluating Deflection Ratio**: \frac{\delta_2}{\delta_1} = \frac{I_1}{I_2} = \frac{I_1}{\frac{15}{16} I_1} = \frac{16}{15} **3. Comprehensive Options & Distractor Analysis**: - **(A)** 16/15: ✅ **CORRECT**. Exactly equals $1 / (15/16) = 16/15 \approx 1.067$. - **(B)** 15/16: ❌ Incorrect. This is the ratio of stiffnesses $I_2/I_1$, not deflections. - **(C)** 4/3: ❌ Incorrect. - **(D)** 2: ❌ Incorrect. **4. Official Master Key & Exam Takeaway**: - **Official Answer**: **A** - **Exam Rule**: Deflection is inversely proportional to moment of inertia: $\frac{\delta_{hollow}}{\delta_{solid}} = \frac{I_{solid}}{I_{hollow}} = \frac{1}{1 - (R_i/R_o)^4}$.
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