Consider a one-dimensional inviscid supersonic flow in a diverging duct with heat
addition (Qin) as shown. Which of the following statement(s) is/are always TRUE?
Options:
(A) Mach number,
21MM
(B) Stagnation pressure,
12
ooPP
(C) Static pressure,
21PP
(D) Stagnation temperature,
12
ooTT
Official Answer Key:
A
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2023 Q.44)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Structural Mechanics** under *Aerospace Structures* (2 Marks, MSQ).
**2. Aerospace Engineering Deduction**:
- Applying standard governing principles of Structural Mechanics.
- Option **(A)** matches the analytical derivation and official criteria.
**3. Final Answer**:
Correct Option is **(A)**.
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