Streamline pattern of flow past a cylinder is s hown in the figure below. The oncoming flow is
steady, irrotational and incompressible. The flow is from left to right. Bernoulli's equation
CANNOT
be applied between the points
(A) 1 and 2 (B) 1 and 5 (C ) 3 and 4 (D) 5 and 6
Official Answer Key:
0.0
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2013 Q.36)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Incompressible & Compressible Aerodynamics** under *Aerodynamics & Fluid Mechanics* (2 Marks, NAT).
**2. Analytical Calculation**:
- Substituting aerodynamic parameters into governing Incompressible & Compressible Aerodynamics equation.
**3. Final Answer**:
Acceptable official numerical value is **0.0**.
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