Question Statement:
Bernoulli's equation is valid under steady state
Options:
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(A) only along a streamline in inviscid flow, and between any two points in potential flow.
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(B) between any two points in both inviscid flow and potential flow.
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(C) between any two points in inviscid flow, and only along a streamline in potential flow.
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(D) only along a streamline in both inviscid flow and potential flow.
2012 AEROSPACE ENGINEERING - AE
AE 4/12
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2012 Q.20)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Structural Mechanics** under *Aerospace Structures* (1 Mark, MCQ).
**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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