GATE AE 2023 • Q26 MSQ • 1 Mark

Propulsion

Thermodynamic Cycles of Gas Turbines

Subtopic: Brayton Cycle with Real Component Efficiencies

Question Statement:

Which of the following statement(s) is/are true about the state of stress in a plane?

Options:

  • (A) Maximum or major principal stress is algebraically the largest direct stress at a point.
  • (B) The magnitude of minor principal stress cannot be greater than the magnitude of major principal stress.
  • (C) The planes of maximum shear stress are inclined at 90 degrees to the principal axes.
  • (D) The normal stresses along the planes of maximum shear stress are equal.

Official Answer Key:

A, D

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2023 Q.26)** **1. Governing Concept & Theory**: Governed by principles of **Thermodynamic Cycles of Gas Turbines** (Aerospace Propulsion, 1 Mark, MSQ). **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, D**. **3. Official Answer Verification**: - **Official Result**: **A, D** - **Evaluation Status**: Matches official GATE 2023 master key with 100% accuracy.

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