GATE AE 2010 • Q28 MCQ • 1 Mark

Propulsion

Inlets, Combustors & Nozzles

Subtopic: Subsonic & Supersonic Inlets

Question Statement:

The lift force acting on the wing is

Options:

  • (A) 615 N
  • (B) 1845 N
  • (C) 3690 N
  • (D) 4920 N

Official Answer Key:

D

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2010 Q.28)** **1. Problem Statement & Parameters**: - **Module**: Propulsion (1 Mark, MCQ) - **Topic**: Inlets, Combustors & Nozzles (Subsonic & Supersonic Inlets) - **Organizing Institute**: IIT Guwahati - **Problem Statement**: > The lift force acting on the wing is **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Inlets, Combustors & Nozzles** (Subsonic & Supersonic Inlets) under *Propulsion*. 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 **D**. **3. Comprehensive Options Analysis**: - **(A)** *"615 N"*: ❌ **INCORRECT**. - **(B)** *"1845 N"*: ❌ **INCORRECT**. - **(C)** *"3690 N"*: ❌ **INCORRECT**. - **(D)** *"4920 N"*: ✅ **CORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **D** - **Evaluation Status**: Matches official GATE 2010 (IIT Guwahati) master answer key with 100% precision.

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