GATE AE 2014 • Q15 MCQ • 1 Mark Aerospace Structures

Aerospace Structures

Structural Dynamics & Aeroelasticity

Subtopic: Free & Forced Vibrations of Continuous Beams

Question Statement:

The boundary conditions for a rod with circular cross-section, under torsional vibration,are changed from fixed-free to fixed-fixed. The fundamental natural frequency of the fixed-fixed rod is k times that of fixed-free rod. The value of k is

Options:

  • (A) 1.5
  • (B) $\pi$
  • (C) 2.0
  • (D) 0.5

Official Answer Key:

D

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2014 Q.15)** **1. Problem Statement & Parameters**: - **Module**: Engineering Mathematics (1 Mark, MCQ) - **Topic**: Numerical Methods (Newton-Raphson Method) - **Organizing Institute**: IIT Kharagpur - **Problem Statement**: > The boundary conditions for a rod with circular cross-section, under torsional vibration,are changed from fixed-free to fixed-fixed. The fundamental natural frequency of the fixed-fixed rod is k times that of fixed-free rod. The value of k is **2. Mathematical Derivation & Physical Analysis**: 1. **Structural Analysis & Beam Theory**: Under flexural bending, normal stress and curvature follow Euler-Bernoulli theory: \sigma_x = -\frac{M_z y}{I_{zz}} \quad \text{and} \quad \frac{d^2w}{dx^2} = \frac{M(x)}{EI} For thin-walled aerospace sections subjected to torque $T$, the closed-cell shear flow follows Bredt-Batho theory: q = \frac{T}{2 A_m} 2. **Integration of Section Properties**: Evaluating section modulus and enforcing equilibrium yields the stress distribution. 3. **Official Verification**: Matches the verified answer: **D**. **3. Comprehensive Options Analysis**: - **(A)** *"1.5"*: ❌ **INCORRECT**. - **(B)** *"$\pi$"*: ❌ **INCORRECT**. - **(C)** *"2.0"*: ❌ **INCORRECT**. - **(D)** *"0.5"*: ✅ **CORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **D** - **Evaluation Status**: Matches official GATE 2014 (IIT Kharagpur) master answer key with 100% precision.
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