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Streamline pattern of flow past a cylinder is shown 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


Question ID - 156030 :-

Streamline pattern of flow past a cylinder is shown 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

1 Answer
5876 Votes
3537

Answer Key : (C) -

(C) 3 and 4



Next Question :

Consider a supersonic stream at a Mach number $M=2$, undergoing a gradual expansion. The stream is turned by an angle of 3 degrees due to the expansion. The following data is given.

The Mach number downstream of the expansion is
(A) 1.88
(B) 2.00
(C) 2.11
(D) 2.33


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