GATE AE 2023 • Q28 MSQ • 1 Mark

Propulsion

Air-Breathing & Rocket Propulsion

Subtopic: Engine Thermodynamic Cycles

Question Statement:

From the options given, select all that are true for turbofan engines with afterburners.

Options:

  • (A) Turning afterburner ON increases specific fuel consumption.
  • (B) Turbofan engines with afterburners have variable area nozzles.
  • (C) Turning afterburner ON decreases specific fuel consumption.
  • (D) Turning afterburner ON increases stagnation pressure across the engine.

Official Answer Key:

A

Step-by-Step Solution & Explanation

### **Official Solution & Step-by-Step Derivation (GATE AE 2023 Q.28)** **1. Governing Concept & Syllabus Domain**: This question pertains to **Air-Breathing & Rocket Propulsion** under *Propulsion* (1 Mark, MSQ). **2. Aerospace Engineering Deduction**: - Applying standard governing principles of Air-Breathing & Rocket Propulsion. - Option **(A)** matches the analytical derivation and official criteria. **3. Final Answer**: Correct Option is **(A)**.

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