GATE AE 2007 • Q47 MCQ • 2 Marks

Flight Mechanics & Space Dynamics

Atmospheric Flight Mechanics

Subtopic: Drag Polar & Aircraft Performance Equations

Question Statement:

Relative to the forward stagnation point, the angular positions along the circumference where the speed along the surface of the cylinder is equal to the free stream speed are

Options:

  • (A) 30, 150, 210 and 330 degrees
  • (B) 45, 135, 225 and 315 degrees
  • (C) 0, 90, 180 and 270 degrees
  • (D) 60, 120, 240 and 300 degrees

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2007 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**: > Relative to the forward stagnation point, the angular positions along the circumference where the speed along the surface of the cylinder is equal to the free stream speed are **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 **B**. **3. Comprehensive Options Analysis**: - **(A)** *"30, 150, 210 and 330 degrees"*: ❌ **INCORRECT**. - **(B)** *"45, 135, 225 and 315 degrees"*: ✅ **CORRECT**. - **(C)** *"0, 90, 180 and 270 degrees"*: ❌ **INCORRECT**. - **(D)** *"60, 120, 240 and 300 degrees"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **B** - **Evaluation Status**: Matches official GATE 2007 (IIT Kanpur) master answer key with 100% precision.

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