Question Statement:
The thrust produced by a turbojet engine
Options:
-
(A) Increases with increasing compressor pressure ratio
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(B) Decreases with increasing compressor pressure ratio
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(C) Remains constant with increasing compressor pressure ratio
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(D) First increases and then decreases with increasing compressor pressure ratio
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2014 Q.20)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Air-Breathing & Rocket Propulsion** under *Propulsion* (1 Mark, MCQ).
**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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