For which one of the nozzle exit Mach numbers given below is the thrust highest?
Options:
(A) 1
(B) 1.5
(C) 2
(D) 2.5
Linked Answer Questions
Statement for Linked Answer Questions 52 and 53: Circulation theory of lift is assumed for a thin
symmetric airfoil at an angle of attack α. Free stream velocity is U.
Official Answer Key:
A
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2013 Q.51)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Incompressible & Compressible Aerodynamics** under *Aerodynamics & Fluid Mechanics* (2 Marks, MCQ).
**2. Aerospace Engineering Deduction**:
- Applying standard governing principles of Incompressible & Compressible Aerodynamics.
- Option **(A)** matches the analytical derivation and official criteria.
**3. Final Answer**:
Correct Option is **(A)**.
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