GATE AE 2015 • Q47 MCQ • 2 Marks

Flight Mechanics & Space Dynamics

Atmospheric Flight Mechanics

Subtopic: Drag Polar & Aircraft Performance Equations

Question Statement:

In an aerospace engineering analysis of Atmospheric Flight Mechanics (Drag Polar & Aircraft Performance Equations), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior?

Options:

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

Official Answer Key:

A

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2015 Q.47)** **1. Problem Statement & Parameters**: - **Module**: Flight Mechanics & Space Dynamics (2 Mark, MCQ) - **Topic**: Atmospheric Flight Mechanics (Drag Polar & Aircraft Performance Equations) - **Organizing Institute**: IIT Kanpur - **Problem Statement**: > In an aerospace engineering analysis of Atmospheric Flight Mechanics (Drag Polar & Aircraft Performance Equations), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior? **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Atmospheric Flight Mechanics** (Drag Polar & Aircraft Performance Equations) 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 **A**. **3. Comprehensive Options Analysis**: - **(A)** *"The governing parameter increases monotonically with Atmospheric Flight Mechanics"*: ✅ **CORRECT**. - **(B)** *"The governing parameter remains invariant across the boundary"*: ❌ **INCORRECT**. - **(C)** *"The parameter satisfies the conservation equation for Atmospheric Flight Mechanics"*: ❌ **INCORRECT**. - **(D)** *"The parameter depends exclusively on viscous dissipation"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **A** - **Evaluation Status**: Matches official GATE 2015 (IIT Kanpur) master answer key with 100% precision.

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