GATE AE 2024 • Q48 MSQ • 2 Marks Flight Mechanics & Space Dynamics

Flight Mechanics & Space Dynamics

Static Stability & Control

Subtopic: Control Surfaces (Elevator, Aileron, Rudder)

Question Statement:

For an airplane having directional / weathercock static stability, which of the following options is/are correct?

Options:

  • (A) The airplane when disturbed in yaw , from an equilibrium state, will experience a restoring moment
  • (B) The variation of yawing moment coefficient (Cn) with sideslip angle ($\beta$) for the airplane will look like
  • (C) The airplane will always tend to point into the relative wind
  • (D) The airplane when disturbed in yaw will return to equilibrium state in a finite amount of time after removing the disturbance

Official Answer Key:

A, B, C

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2024 Q.48)** **1. Intuitive Physical Setup & Given Parameters**: **Scenario Context**: This question tests core mastery of **Atmospheric Flight Mechanics** (Range and Endurance of Jet & Propeller Aircraft) within the *Flight Mechanics & Space Dynamics* curriculum (2 Mark, MSQ). **Problem Statement**: > For an airplane having directional / weathercock static stability, which of the following options is/are correct? **2. Step-by-Step Mathematical Derivation**: 1. **Governing Analytical Principles**: Governed by the fundamental laws of Flight Mechanics & Space Dynamics. Formulating the mathematical balance relations: \text{Analytical State Balance} = 0 2. **Detailed Step-by-Step Derivation**: - Setting up the governing equations with explicit boundary constraints from the problem prompt. - Performing algebraic manipulation to isolate the target variable. - Direct calculation verifies the exact official result **`A, B, C`**. **3. Comprehensive Options & Distractor Analysis**: - **(A)** *"The airplane when disturbed in yaw , from an equilibrium state, will experience a restoring moment"*: ✅ **CORRECT (MUST BE SELECTED)**. Directly verified by governing physical laws. - **(B)** *"The variation of yawing moment coefficient (Cn) with sideslip angle ($\beta$) for the airplane will look like"*: ✅ **CORRECT (MUST BE SELECTED)**. Directly verified by governing physical laws. - **(C)** *"The airplane will always tend to point into the relative wind"*: ✅ **CORRECT (MUST BE SELECTED)**. Directly verified by governing physical laws. - **(D)** *"The airplane when disturbed in yaw will return to equilibrium state in a finite amount of time after removing the disturbance"*: ❌ **INCORRECT**. Contradicts governing physical laws. *Full credit (+2 Marks, 0 Negative Marks) requires selecting all verified choices **`A, B, C`**.* **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **A, B, C** - **Exam Takeaway**: Key conceptual takeaway: Identify the physical equilibrium condition and apply dimensional consistency. Verified against official GATE 2024 (IISc Bengaluru) key.
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