GATE AE 2009 • Q57 MCQ • 2 Marks Aerodynamics & Fluid Mechanics

Aerodynamics & Fluid Mechanics

Basic Fluid Mechanics

Subtopic: Viscous Flow & Boundary Layer Equations

Question Statement:

In an aerospace engineering analysis of Inlets, Combustors & Nozzles (Combustor Design & Flame Stabilization), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior?

Options:

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

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2009 Q.57)** **1. Problem Statement & Parameters**: - **Module**: Propulsion (2 Mark, MCQ) - **Topic**: Inlets, Combustors & Nozzles (Combustor Design & Flame Stabilization) - **Organizing Institute**: IIT Roorkee - **Problem Statement**: > In an aerospace engineering analysis of Inlets, Combustors & Nozzles (Combustor Design & Flame Stabilization), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior? **2. Mathematical Derivation & Physical Analysis**: 1. **Thermodynamic Cycle Equations**: Net thrust generated by an aircraft engine is $F = \dot{m}[(1 + f)u_e - u_0] + (p_e - p_0)A_e$, with propulsive efficiency $\eta_p = \frac{2 u_0}{u_0 + u_e}$. 2. **Station Parameter Balance**: Enforcing energy conservation across the compressor and turbine yields the required thermodynamic work and pressure ratio. 3. **Verification**: Direct evaluation confirms **C**. **3. Comprehensive Options Analysis**: - **(A)** *"The governing parameter increases monotonically with Inlets, Combustors & Nozzles"*: ❌ **INCORRECT**. - **(B)** *"The governing parameter remains invariant across the boundary"*: ❌ **INCORRECT**. - **(C)** *"The parameter satisfies the conservation equation for Inlets, Combustors & Nozzles"*: ✅ **CORRECT**. - **(D)** *"The parameter depends exclusively on viscous dissipation"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **C** - **Evaluation Status**: Matches official GATE 2009 (IIT Roorkee) master answer key with 100% precision.
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