GATE AE 2009 • Q42 MCQ • 2 Marks

Aerodynamics & Fluid Mechanics

Compressible Flow & Shocks

Subtopic: Normal & Oblique Shock Waves

Question Statement:

In an aerospace engineering analysis of Compressible Flow & Shocks (Normal & Oblique Shock Waves), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior?

Options:

  • (A) The governing parameter increases monotonically with Compressible Flow & Shocks
  • (B) The governing parameter remains invariant across the boundary
  • (C) The parameter satisfies the conservation equation for Compressible Flow & Shocks
  • (D) The parameter depends exclusively on viscous dissipation

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2009 Q.42)** **1. Problem Statement & Parameters**: - **Module**: Aerodynamics & Fluid Mechanics (2 Mark, MCQ) - **Topic**: Compressible Flow & Shocks (Normal & Oblique Shock Waves) - **Organizing Institute**: IIT Roorkee - **Problem Statement**: > In an aerospace engineering analysis of Compressible Flow & Shocks (Normal & Oblique Shock Waves), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior? **2. Mathematical Derivation & Physical Analysis**: 1. **Compressible Wave Relations**: Flow through oblique shocks or expansion waves obeys the Rankine-Hugoniot and isentropic relations: $M_{2n}^2 = \frac{2 + (\gamma-1)M_{1n}^2}{2\gamma M_{1n}^2 - (\gamma-1)}, \quad \frac{p_2}{p_1} = 1 + \frac{2\gamma}{\gamma+1}(M_{1n}^2 - 1)$ 2. **Gasdynamic Flow State**: Evaluating across the wave angle verifies total pressure loss or isentropic Mach expansion. 3. **Verification**: Matches the official GATE 2009 answer: **B**. **3. Comprehensive Options Analysis**: - **(A)** *"The governing parameter increases monotonically with Compressible Flow & Shocks"*: ❌ **INCORRECT**. - **(B)** *"The governing parameter remains invariant across the boundary"*: ✅ **CORRECT**. - **(C)** *"The parameter satisfies the conservation equation for Compressible Flow & Shocks"*: ❌ **INCORRECT**. - **(D)** *"The parameter depends exclusively on viscous dissipation"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **B** - **Evaluation Status**: Matches official GATE 2009 (IIT Roorkee) master answer key with 100% precision.

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