Aerospace Engineering > GATE 2012 > Fluid Dynamics
Bernoulli's equation is valid under steady state
A
only along a streamline in inviscid flow, and between any two points in potential flow.
B
between any two points in both inviscid flow and potential flow.
C
between any two points in inviscid flow, and only along a streamline in potential flow.
D
only along a streamline in both inviscid flow and potential flow.

Correct : c

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