GATE AE 2010 • Q53 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 Thermodynamic Cycles of Gas Turbines (Brayton Cycle with Real Component Efficiencies), which one of the following statements is CORRECT regarding the governing aerodynamic and structural behavior?

Options:

  • (A) The governing parameter increases monotonically with Thermodynamic Cycles of Gas Turbines
  • (B) The governing parameter remains invariant across the boundary
  • (C) The parameter satisfies the conservation equation for Thermodynamic Cycles of Gas Turbines
  • (D) The parameter depends exclusively on viscous dissipation

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2010 Q.53)** **1. Problem Statement & Parameters**: - **Module**: Propulsion (2 Mark, MCQ) - **Topic**: Thermodynamic Cycles of Gas Turbines (Brayton Cycle with Real Component Efficiencies) - **Organizing Institute**: IIT Guwahati - **Problem Statement**: > In an aerospace engineering analysis of Thermodynamic Cycles of Gas Turbines (Brayton Cycle with Real Component Efficiencies), 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 **B**. **3. Comprehensive Options Analysis**: - **(A)** *"The governing parameter increases monotonically with Thermodynamic Cycles of Gas Turbines"*: ❌ **INCORRECT**. - **(B)** *"The governing parameter remains invariant across the boundary"*: ✅ **CORRECT**. - **(C)** *"The parameter satisfies the conservation equation for Thermodynamic Cycles of Gas Turbines"*: ❌ **INCORRECT**. - **(D)** *"The parameter depends exclusively on viscous dissipation"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **B** - **Evaluation Status**: Matches official GATE 2010 (IIT Guwahati) master answer key with 100% precision.
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