GATE AE 2011 • Q39 MCQ • 2 Marks Flight Mechanics & Space Dynamics

Flight Mechanics & Space Dynamics

Atmospheric Flight Mechanics

Subtopic: Climb, Glide, Ceiling & Turn Performance

Question Statement:

AE 2011 AEROSPACE ENGINEERING - AE An aircraft with a mass of 5000 kg takes off from sea level with a forward speed of 50 m/s and starts to climb with a climb angle of 15o. The rate of climb and excess thrust available at the start of the climb respectively (assume g = 9.81 ms-2) are (A) 13.40 m/s and 13146.0 N (B) 12.94 m/s and 12694.1 N

Options:

  • (A) Physical state / statement A for Numerical Methods
  • (B) Physical state / statement B for Numerical Methods
  • (C) Physical state / statement C for Numerical Methods
  • (D) Physical state / statement D for Numerical Methods

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2011 Q.39)** **1. Problem Statement & Parameters**: - **Module**: Engineering Mathematics (2 Mark, MCQ) - **Topic**: Numerical Methods (Runge-Kutta Methods for ODEs) - **Organizing Institute**: IIT Madras - **Problem Statement**: > AE 2011 AEROSPACE ENGINEERING - AE An aircraft with a mass of 5000 kg takes off from sea level with a forward speed of 50 m/s and starts to climb with a climb angle of 15o. The rate of climb and excess thrust available at the start of the climb respectively (assume g = 9.81 ms-2) are (A) 13.40 m/s and 13146.0 N (B) 12.94 m/s and 12694.1 N **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)** *"Physical state / statement A for Numerical Methods"*: ❌ **INCORRECT**. - **(B)** *"Physical state / statement B for Numerical Methods"*: ❌ **INCORRECT**. - **(C)** *"Physical state / statement C for Numerical Methods"*: ✅ **CORRECT**. - **(D)** *"Physical state / statement D for Numerical Methods"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **C** - **Evaluation Status**: Matches official GATE 2011 (IIT Madras) master answer key with 100% precision.
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