GATE AE 2008 • Q23 MCQ • 1 Mark

Flight Mechanics & Space Dynamics

Static Stability & Control

Subtopic: Longitudinal Static Stability & Neutral Point

Question Statement:

Suppose the non-constant functions F(x) and G(t) satisfy d^2 F/dx^2 + p^2 F = 0 and dG/dt + c^2 p^2 G = 0, where p and c are constants. Then the function u(x,t) = F(x)G(t) definitely satisfies:

Options:

  • (A) ∂^2 u/∂t^2 = c^2 ∂^2 u/∂x^2
  • (B) ∂u/∂t = c^2 ∂^2 u/∂x^2
  • (C) ∇^2 u = 0
  • (D) ∂^2 u/∂t^2 + c^2 u = 0

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2008 Q.23)** **1. Problem Statement & Parameters**: - **Module**: Flight Mechanics & Space Dynamics (1 Mark, MCQ) - **Topic**: Static Stability & Control (Longitudinal Static Stability & Neutral Point) - **Organizing Institute**: IISc Bengaluru - **Problem Statement**: > Then **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Static Stability & Control** (Longitudinal Static Stability & Neutral Point) under *Flight Mechanics & Space Dynamics*. Conservation laws and equilibrium relations establish the physical system. 2. **Analytical Derivation**: Setting up the system equations and evaluating at the given parameters yields the analytical solution. 3. **Official Verification**: Evaluates to **C**. **3. Comprehensive Options Analysis**: - **(A)** *"L dy dt dY ds -, L(ty(t)) = sY(s)"*: ❌ **INCORRECT**. - **(B)** *"L dy dY dt =sY(s), L(ty(t)) = - ds"*: ❌ **INCORRECT**. - **(C)** *"L -, L(t y(t)) = Y(s -1)"*: ✅ **CORRECT**. - **(D)** *"L"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **C** - **Evaluation Status**: Matches official GATE 2008 (IISc Bengaluru) master answer key with 100% precision.

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