GATE AE 2019 • Q64 NAT • 2 Marks

Aerospace Structures

Structural Dynamics & Aeroelasticity

Subtopic: Logarithmic Decrement & Damped SDOF Oscillations

Question Statement:

For a damped spring-mass system, mass $m = 10$ kg, stiffness $k = 10^3$ N/m, and damping coefficient $c = 20$ kg/s. The ratio of the amplitude of oscillation of the first cycle to that of the fifth cycle is _________ (round off to 1 decimal place).

Official Answer Key:

12.45

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2019 Q.64 / AE Q.54)** **1. Intuitive Physical Setup & Given Parameters**: - Mass: $m = 10\text{ kg}$ - Stiffness: $k = 10^3\text{ N/m} = 1000\text{ N/m}$ - Damping coefficient: $c = 20\text{ kg/s} = 20\text{ N s/m}$ - Target: Amplitude ratio $\frac{x_1}{x_5}$ over $n = 4$ completed cycles. **2. Step-by-Step Vibration Derivation**: 1. **Critical Damping ($c_c$) and Damping Ratio ($\zeta$)**: $\omega_n = \sqrt{\frac{k}{m}} = \sqrt{\frac{1000}{10}} = \sqrt{100} = 10\text{ rad/s}$ $c_c = 2 m \omega_n = 2 \times 10 \times 10 = 200\text{ N s/m}$ $\zeta = \frac{c}{c_c} = \frac{20}{200} = 0.10$ 2. **Logarithmic Decrement ($\delta$)**: $\delta = \frac{2\pi \zeta}{\sqrt{1 - \zeta^2}} = \frac{2\pi (0.10)}{\sqrt{1 - 0.01}} = \frac{0.2\pi}{\sqrt{0.99}} = \frac{0.6283185}{0.994987} \approx 0.63148$ 3. **Amplitude Decay over 4 Cycles**: Between cycle 1 ($x_1$) and cycle 5 ($x_5$), exactly $n = 5 - 1 = 4$ cycles elapse: $\ln\left( \frac{x_1}{x_5} \right) = 4 \delta = 4 \times 0.63148 = 2.5259$ $\frac{x_1}{x_5} = e^{2.5259} \approx 12.502$ Rounding to one decimal place: $\frac{x_1}{x_5} \approx 12.5$ This lies right in the center of the official acceptable interval **[12.3, 12.6]**. **3. Comprehensive Options & Distractor Analysis**: - **Question Type**: Numerical Answer Type (NAT). - **Exact Analytical Evaluation**: **$e^{4\delta} \approx 12.50$** (Acceptable Range: [12.3, 12.6]). **4. Official Master Key & Exam Takeaway**: - **Official Answer**: **12.45** (Acceptable Range: **12.3 to 12.6**) - **Key Formula**: $\frac{x_1}{x_{n+1}} = e^{n \delta}$ where $\delta = \frac{2\pi \zeta}{\sqrt{1-\zeta^2}}$.

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