GATE AE 2025 โ€ข Q28 MCQ โ€ข 1 Mark

Propulsion

Inlets, Combustors & Nozzles

Subtopic: Subsonic & Supersonic Inlets

Question Statement:

A stress field is given by ๐œŽxx = ๐œŽzz = C1y; ๐œŽyy = C2y; ๐œxy = ๐œyz = ๐œzx = 0, where C1 and C2 are non-zero constants. If the stress field satisfies equilibrium, which one of the following options is correct?

Options:

  • (A) There is no body force per unit volume.
  • (B) There is a constant body force per unit volume in the y-direction.
  • (C) The body force per unit volume varies linearly in the y-direction.
  • (D) The direction of the body force per unit volume depends on the value of C1.

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2025 Q.28)** **1. Governing Concept & Theory**: Governed by principles of **Inlets, Combustors & Nozzles** (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 Tsiolkovskyโ€™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 **B**. **3. Official Answer Verification**: - **Official Result**: **B** - **Evaluation Status**: Matches official GATE 2025 master key with 100% accuracy. - **Selected Option**: **(B)** โ€” *"There is a constant body force per unit volume in the y-direction."*

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