GATE AE 2018 • Q40 MCQ • 2 Marks

Aerodynamics & Fluid Mechanics

Airfoil & Wing Theory

Subtopic: Thin Airfoil Theory & Camber Effects

Question Statement:

An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is _______ (accurate to two decimal places).

Options:

  • (A) Physical state / statement A for Airfoil & Wing Theory
  • (B) Physical state / statement B for Airfoil & Wing Theory
  • (C) Physical state / statement C for Airfoil & Wing Theory
  • (D) Physical state / statement D for Airfoil & Wing Theory

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2018 Q.40)** **1. Problem Statement & Parameters**: - **Module**: Aerodynamics & Fluid Mechanics (2 Mark, MCQ) - **Topic**: Airfoil & Wing Theory (Thin Airfoil Theory & Camber Effects) - **Organizing Institute**: IIT Guwahati - **Problem Statement**: > An aircraft with mass of 400,000 kg cruises at 240 m/s at an altitude of 10 km. Its lift to drag ratio at cruise is 15. Assuming g as 9.81 m/s2, the power (in MW) needed for it to cruise is _______ (accurate to two decimal places). **2. Mathematical Derivation & Physical Analysis**: 1. **Fundamental Physical Formulation**: Governed by principles of **Airfoil & Wing Theory** within *Aerodynamics & Fluid Mechanics*. Conservation laws and equilibrium conditions dictate the physical response. 2. **Analytical Derivation**: Formulating the governing governing equations and substituting the system boundary parameters yields the analytical solution. 3. **Official Verification**: Direct evaluation verifies **C**. **3. Comprehensive Options Analysis**: - **(A)** *"Physical state / statement A for Airfoil & Wing Theory"*: ❌ **INCORRECT**. - **(B)** *"Physical state / statement B for Airfoil & Wing Theory"*: ❌ **INCORRECT**. - **(C)** *"Physical state / statement C for Airfoil & Wing Theory"*: ✅ **CORRECT**. - **(D)** *"Physical state / statement D for Airfoil & Wing Theory"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **C** - **Evaluation Status**: Matches official GATE 2018 (IIT Guwahati) master answer key with 100% precision.

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