GATE AE 2025 • Q29 MCQ • 1 Mark Aerospace Structures

Aerospace Structures

Strength of Materials & Elasticity

Subtopic: Euler Buckling of Columns & Energy Methods

Question Statement:

A uniform symmetric cross-section cantilever beam of length $L$ is subjected to a transverse force $P$ at the free end, as shown in the figure. The Young's modulus of the material is $E$ and the moment of inertia is $I$. Ignoring the contributions due to transverse shear, the strain energy stored in the beam is:
Question figure for GATE AE 2025 Q29

Scientific schematic diagram reproduced from official IIT paper

Options:

  • (A) $\frac{P^2L^3}{6EI}$
  • (B) $\frac{PL^3}{3EI}$
  • (C) $\frac{PL^3}{6EI}$
  • (D) $\frac{P^2L^3}{3EI}$

Official Answer Key:

A

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2025 Q.29)** **1. Intuitive Physical Setup & Given Parameters**: - Cantilever beam of length $L$ fixed at $x = 0$ and free at $x = L$. - Uniform symmetric cross-section with flexural rigidity $EI$. - Transverse concentrated point force $P$ applied at the free end ($x = L$). - Transverse shear deformation contributions are ignored (pure Euler-Bernoulli bending). We need to determine the total strain energy $U$ stored in the beam. **2. Step-by-Step Structural Mechanics Derivation**: 1. **Bending Moment Distribution**: Taking coordinate $x$ from the fixed support ($0 \le x \le L$), or coordinate $\xi$ from the free tip ($0 \le \xi \le L$ where $\xi = L - x$): M(\xi) = P \xi 2. **Strain Energy Formula in Pure Bending**: The elastic bending strain energy stored in a beam is: U = \int_0^L \frac{M^2}{2EI} d\xi 3. **Evaluate the Integral**: U = \int_0^L \frac{(P\xi)^2}{2EI} d\xi = \frac{P^2}{2EI} \int_0^L \xi^2 d\xi U = \frac{P^2}{2EI} \left[ \frac{\xi^3}{3} \right]_0^L = \frac{P^2}{2EI} \left(\frac{L^3}{3}\right) = \frac{P^2 L^3}{6EI} 4. **Alternative Work-Energy Check**: By Clapeyron's theorem, the external work done by load $P$ slowly applied is: W_{\text{ext}} = \frac{1}{2} P \delta_{\text{tip}} For a cantilever beam with tip load $P$, tip deflection is $\delta_{\text{tip}} = \frac{P L^3}{3EI}$. U = W_{\text{ext}} = \frac{1}{2} P \left(\frac{P L^3}{3EI}\right) = \frac{P^2 L^3}{6EI} **3. Comprehensive Options & Distractor Analysis**: - **(A) P^2 L^3 / (6EI)**: ✅ **CORRECT**. Exactly matches $\int \frac{M^2}{2EI}dx = \frac{1}{2}P\delta_{\text{tip}}$. - **(B) P L^3 / (3EI)**: ❌ **INCORRECT**. This is the tip deflection $\delta_{\text{tip}}$, having dimensions of length, not energy. - **(C) P L^3 / (6EI)**: ❌ **INCORRECT**. Dimensional error ($P$ instead of $P^2$). - **(D) P^2 L^3 / (3EI)**: ❌ **INCORRECT**. Forgets the factor of $1/2$ in strain energy ($P \delta_{\text{tip}}$ instead of $\frac{1}{2}P\delta_{\text{tip}}$). **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **A** - **Exam Takeaway**: Elastic strain energy is $U = \frac{1}{2} P \delta = \frac{P^2 L^3}{6EI}$. Always check dimensional consistency: $[P^2 L^3 / EI] = \text{Force} \times \text{Length} = \text{Energy}$.
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