GATE AE 2018 • Q60 NAT • 2 Marks

Aerospace Structures

Structural Dynamics & Aeroelasticity

Subtopic: Cantilever Beam Natural Frequency

Question Statement:

A 1 m long massless cantilever beam oscillates at 2 Hz, while a 60 kg mass is attached at the tip of it. The flexural rigidity of the beam (in kN-m$^2$) is _________________ (accurate to two decimal places).

Official Answer Key:

3.15

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2018 Q.60 / AE Q.50)** **1. Intuitive Physical Setup & Given Parameters**: - Length of cantilever beam: $L = 1\text{ m}$ - Tip mass: $m = 60\text{ kg}$ - Natural frequency: $f = 2\text{ Hz} = 2\text{ cycles/s}$ - Angular natural frequency: $\omega_n = 2\pi f = 2\pi (2) = 4\pi\text{ rad/s} \approx 12.5664\text{ rad/s}$ **2. Step-by-Step Mathematical Derivation**: 1. **Equivalent Tip Stiffness of Cantilever Beam ($k$)**: From Euler-Bernoulli beam theory: $k = \frac{3EI}{L^3}$ 2. **Natural Frequency of Single Degree of Freedom System**: $\omega_n = \sqrt{\frac{k}{m}} = \sqrt{\frac{3EI}{m L^3}}$ 3. **Solving for Flexural Rigidity ($EI$)**: $\omega_n^2 = \frac{3EI}{m L^3} \implies EI = \frac{m L^3 \omega_n^2}{3} = \frac{m L^3 (4\pi)^2}{3}$ 4. **Numerical Evaluation**: $EI = \frac{60 \times (1)^3 \times 16 \pi^2}{3} = 20 \times 16 \pi^2 = 320 \pi^2\text{ N m}^2$ Using $\pi^2 \approx 9.8696$: $EI = 320 \times 9.8696 = 3158.27\text{ N m}^2 = 3.158\text{ kN m}^2$ Rounding to two decimal places: $EI \approx 3.16\text{ kN m}^2$ This lies squarely within the official acceptable range **[3.10, 3.20]**. **3. Comprehensive Options & Distractor Analysis**: - **Question Type**: Numerical Answer Type (NAT). - **Official Range**: **3.10 to 3.20 kN-m$^2$**. **4. Official Master Key & Exam Takeaway**: - **Official Answer**: **3.15** (Acceptable Range: **3.10 to 3.20**) - **Key Formula**: $EI = \frac{m L^3 (2\pi f)^2}{3}$.

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