GATE AE 2007 • Q40 MCQ • 2 Marks

Aerodynamics & Fluid Mechanics

Airfoil & Wing Theory

Subtopic: Thin Airfoil Theory & Camber Effects

Question Statement:

At a stationary point of a multi-variable function, which of the following is true?

Options:

  • (A) Curl of the function becomes unity
  • (B) Gradient of the function vanishes
  • (C) Divergence of the function vanishes
  • (D) Gradient of the function is maximum

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2007 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 Kanpur - **Problem Statement**: > At a stationary point of a multi-variable function, which of the following is true? **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Airfoil & Wing Theory** (Thin Airfoil Theory & Camber Effects) under *Aerodynamics & Fluid Mechanics*. 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)** *"Curl of the function becomes unity"*: ❌ **INCORRECT**. - **(B)** *"Gradient of the function vanishes"*: ✅ **CORRECT**. - **(C)** *"Divergence of the function vanishes"*: ❌ **INCORRECT**. - **(D)** *"Gradient of the function is maximum"*: ❌ **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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