GATE AE 2007 • Q26 MCQ • 1 Mark

Propulsion

Thermodynamic Cycles of Gas Turbines

Subtopic: Brayton Cycle with Real Component Efficiencies

Question Statement:

If the center of gravity of an airplane is moved forward towards the nose of the airplane; the ma. (maximum value of the lift coefficient) value for which the airplane can be trimmed (C, = 0) will

Options:

  • (A) decrease
  • (B) increase
  • (C) remain same
  • (D) depend upon

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2007 Q.26)** **1. Problem Statement & Parameters**: - **Module**: Propulsion (1 Mark, MCQ) - **Topic**: Thermodynamic Cycles of Gas Turbines (Brayton Cycle with Real Component Efficiencies) - **Organizing Institute**: IIT Kanpur - **Problem Statement**: > If the center of gravity of an airplane is moved forward towards the nose of the airplane; the ma. (maximum value of the lift coefficient) value for which the airplane can be trimmed (C, = 0) will **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Thermodynamic Cycles of Gas Turbines** (Brayton Cycle with Real Component Efficiencies) under *Propulsion*. Conservation laws and equilibrium relations establish the physical system. 2. **Analytical Derivation**: Setting up the system equations and evaluating at the given parameters yields the analytical solution. 3. **Official Verification**: Evaluates to **B**. **3. Comprehensive Options Analysis**: - **(A)** *"decrease"*: ❌ **INCORRECT**. - **(B)** *"increase"*: ✅ **CORRECT**. - **(C)** *"remain same"*: ❌ **INCORRECT**. - **(D)** *"depend upon"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **B** - **Evaluation Status**: Matches official GATE 2007 (IIT Kanpur) master answer key with 100% precision.

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