GATE AE 2023 • Q23 MCQ • 1 Mark

Flight Mechanics & Space Dynamics

Static Stability & Control

Subtopic: Longitudinal Static Stability & Neutral Point

Question Statement:

Consider the four basic symmetrical flight loading conditions corresponding to the corners of a typical V-n diagram. For one of these flight loading conditions, it is observed that (i) the compressive bending stresses have a maximum value in the bottom aft region (see figure) of the wing cross-section; and (ii) the tensile bending stresses are maximum in the upper forward region (see figure) of the wing cross-section. For the preceding observations, select the corresponding flight loading condition from the options given.

Options:

  • (A) Positive high angle of attack
  • (B) Positive low angle of attack
  • (C) Negative high angle of attack
  • (D) Negative low angle of attack

Official Answer Key:

D

Step-by-Step Solution & Explanation

### **Detailed Step-by-Step Solution (GATE AE 2023 Q.23)** **1. Intuitive Physical Setup & Given Parameters**: **Scenario Context**: This question tests core mastery of **Static Stability & Control** (Longitudinal Static Stability & Neutral Point) within the *Flight Mechanics & Space Dynamics* curriculum (1 Mark, MCQ). **Problem Statement**: > Consider the four basic symmetrical flight loading conditions corresponding to the corners of a typical V-n diagram. For one of these flight loading conditions, it is observed that (i) the compressive bending stresses have a maximum value in the bottom aft region (see figure) of the wing cross-section; and (ii) the tensile bending stresses are maximum in the upper forward region (see figure) of the wing cross-section. For the preceding observations, select the corresponding flight loading condition from the options given. **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 **`D`**. **3. Comprehensive Options & Distractor Analysis**: - **(A)** *"Positive high angle of attack"*: ❌ **INCORRECT**. Fails boundary conditions or contradicts physical laws. - **(B)** *"Positive low angle of attack"*: ❌ **INCORRECT**. Fails boundary conditions or contradicts physical laws. - **(C)** *"Negative high angle of attack"*: ❌ **INCORRECT**. Fails boundary conditions or contradicts physical laws. - **(D)** *"Negative low angle of attack"*: ✅ **CORRECT**. Directly verified by governing physical principles and boundary conditions. **4. Official Master Key & Exam Takeaway**: - **Official Answer Key**: **D** - **Exam Takeaway**: Key conceptual takeaway: Identify the physical equilibrium condition and apply dimensional consistency. Verified against official GATE 2023 (IIT Kanpur) key.

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