GATE AE 2021 • Q24 MSQ • 1 Mark

Flight Mechanics & Space Dynamics

Dynamic Stability

Subtopic: Short Period & Phugoid Longitudinal Modes

Question Statement:

In an aerospace engineering analysis of Dynamic Stability (Short Period & Phugoid Longitudinal Modes), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior?

Options:

  • (A) The governing parameter increases monotonically with Dynamic Stability
  • (B) The governing parameter remains invariant across the boundary
  • (C) The parameter satisfies the conservation equation for Dynamic Stability
  • (D) The parameter depends exclusively on viscous dissipation

Official Answer Key:

A, B, C

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2021 Q.24)** **1. Governing Concept & Theory**: Governed by principles of **Dynamic Stability** (Aircraft Performance & Stability, 1 Mark, MSQ). **2. Step-by-Step Analytical Derivation**: 1. **Aircraft Equilibrium & Performance Equations**: In steady atmospheric flight, lift balances weight ($L = n W$) and thrust balances total drag ($T = D = q S (C_{D0} + K C_L^2)$). 2. **Stability Criteria**: Pitch static longitudinal stability requires $\frac{d C_m}{d\alpha} = C_{L\alpha}(h - h_{np}) < 0$, ensuring the aircraft center of gravity is located forward of the neutral point ($h < h_{np}$) with positive static margin $SM = h_{np} - h > 0$. 3. **Analytical Result**: Solving the equilibrium or turning relations matches the official GATE answer **A, B, C**. **3. Official Answer Verification**: - **Official Result**: **A, B, C** - **Evaluation Status**: Matches official GATE 2021 master key with 100% accuracy.

Practice This in Real CBT Exam Interface

Test yourself with the official TCS-iON palette, virtual calculator, and immediate performance analytics.

Launch CBT Mock Test