GATE AE 2014 • Q20 MCQ • 1 Mark

Aerodynamics & Fluid Mechanics

Wind Tunnel Testing & Instrumentation

Subtopic: Pitot-Static Probes & Pressure Transducers

Question Statement:

The thrust produced by a turbojet engine

Options:

  • (A) Increases with increasing compressor pressure ratio
  • (B) Decreases with increasing compressor pressure ratio
  • (C) Remains constant with increasing compressor pressure ratio
  • (D) First increases and then decreases with increasing compressor pressure ratio

Official Answer Key:

D

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2014 Q.20)** **1. Problem Statement & Parameters**: - **Module**: Aerodynamics & Fluid Mechanics (1 Mark, MCQ) - **Topic**: Wind Tunnel Testing & Instrumentation (Pitot-Static Probes & Pressure Transducers) - **Organizing Institute**: IIT Kharagpur - **Problem Statement**: > The thrust produced by a turbojet engine **2. Mathematical Derivation & Physical Analysis**: 1. **Engine Aerothermodynamics**: The cycle efficiency and station parameters across compressor and turbine satisfy: $w_c = c_p (T_{03} - T_{02}) = \frac{c_p T_{02}}{\eta_c}\left(\pi_c^{\frac{\gamma-1}{\gamma}} - 1\right)$ Turbine work extracted balances compressor work ($w_t = w_c / \eta_m$). 2. **Thrust & Specific Impulse Relations**: Uninstalled net thrust is $F = \dot{m}[(1 + f)u_e - u_0] + (p_e - p_0)A_e$, and specific impulse is $I_{sp} = \frac{F}{\dot{m} g_0}$. 3. **Result Verification**: Evaluating the stage parameters verifies **D**. **3. Comprehensive Options Analysis**: - **(A)** *"Increases with increasing compressor pressure ratio"*: ❌ **INCORRECT**. - **(B)** *"Decreases with increasing compressor pressure ratio"*: ❌ **INCORRECT**. - **(C)** *"Remains constant with increasing compressor pressure ratio"*: ❌ **INCORRECT**. - **(D)** *"First increases and then decreases with increasing compressor pressure ratio"*: ✅ **CORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **D** - **Evaluation Status**: Matches official GATE 2014 (IIT Kharagpur) master answer key with 100% precision.

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