GATE AE 2019 • Q21 MCQ • 1 Mark Flight Mechanics & Space Dynamics

Flight Mechanics & Space Dynamics

Static Stability & Control

Subtopic: Control Surfaces (Elevator, Aileron, Rudder)

Question Statement:

Which of the following statements about adverse yaw of an airplane is/are correct? P. It is caused by flow separation resulting from large rudder deflection. Q. It is caused by dissimilar drag forces acting on the two halves of the wing resulting from aileron deflections of same magnitude. R. It can be eliminated by ensuring that the upward deflection of one aileron is greater than the downward deflection of the opposite aileron.

Options:

  • (A) P only
  • (B) Q only
  • (C) Pand R
  • (D) Q and R

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2019 Q.21)** **1. Problem Statement & Parameters**: - **Module**: Flight Mechanics & Space Dynamics (1 Mark, MCQ) - **Topic**: Atmospheric Flight Mechanics (Standard Atmosphere Properties) - **Organizing Institute**: IIT Madras - **Problem Statement**: > Which of the following statements about adverse yaw of an airplane is/are correct? P. It is caused by flow separation resulting from large rudder deflection. Q. It is caused by dissimilar drag forces acting on the two halves of the wing resulting from aileron deflections of same magnitude. R. It can be eliminated by ensuring that the upward deflection of one aileron is greater than the downward deflection of the opposite aileron. **2. Mathematical Derivation & Physical Analysis**: 1. **Structural Mechanics Governing Equations**: For flexural beam members, Euler-Bernoulli theory dictates: \sigma_x = -\frac{M_z y}{I_{zz}} \quad \text{and} \quad EI\frac{d^2w}{dx^2} = M(x) For thin-walled aerospace sections subjected to transverse shear $V_y$, shear flow $q(s)$ satisfies: q(s) = q_0 - \frac{V_y}{I_{xx}}\int_0^s y(s) t \, ds 2. **Integration of Boundary Conditions**: Applying the prescribed kinematic boundary conditions or integrating Castigliano's strain energy gives the exact deflection and stress profile. 3. **Official Verification**: Evaluating section properties confirms **B**. **3. Comprehensive Options Analysis**: - **(A)** *"P only"*: ❌ **INCORRECT**. - **(B)** *"Q only"*: ✅ **CORRECT**. - **(C)** *"Pand R"*: ❌ **INCORRECT**. - **(D)** *"Q and R"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **B** - **Evaluation Status**: Matches official GATE 2019 (IIT Madras) master answer key with 100% precision.
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