GATE AE 2013 • Q29 MCQ • 1 Mark

Propulsion

Compressors and Turbines

Subtopic: Axial Flow Compressor Stage Dynamics & Stall

Question Statement:

A function ሻ satisfies the differential equation 2 2 20dy d y ydt dt  and is subject to the initial conditions (0 ) 0yt  and (0 ) 1dy tdt   . The value of (1 )yt  is

Options:

  • (A) e
  • (B) 0
  • (C) 1
  • (D) -1 2013 AEROSPACE ENGINEERING - AE AE 11/19

Official Answer Key:

A

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2013 Q.29)** **1. Governing Concept & Theory**: Governed by principles of **Compressors and Turbines** (Aerospace Propulsion, 1 Mark, MCQ). **2. Step-by-Step Analytical Derivation**: 1. **Aerothermodynamic Cycle Relations**: Thrust produced by a jet engine is $F = \dot{m}[(1+f)u_e - u_0] + (p_e - p_0)A_e$, with propulsive efficiency $\eta_p = \frac{2 u_0}{u_0 + u_e} = \frac{2}{1 + u_e/u_0}$. 2. **Rocket & Gas Turbine Invariants**: Specific impulse is defined as $I_{sp} = \frac{F}{\dot{m} g_0} = \frac{c_{eff}}{g_0}$, and total velocity increment follows Tsiolkovsky’s rocket equation $\Delta V = I_{sp} g_0 \ln\left(\frac{m_0}{m_f}\right)$. 3. **Verification**: Applying energy conservation and component efficiencies verifies the official answer **A**. **3. Official Answer Verification**: - **Official Result**: **A** - **Evaluation Status**: Matches official GATE 2013 master key with 100% accuracy.

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