Aerospace Engineering > GATE 2022 > Incompressible Flow
Consider steady, two-dimensional, incompressible flow over a non-porous flat plate as shown in the figure. For the control volume PQRS, the speed, u∞, at section PQ is uniform and the speed at section RS is given by u(y) = A0(y/h)n, where n is a positive integer. The value of A0 for which the flow through section PS will vanish is:
A
u∞/(n+1)
B
u∞(n+1)
C
u∞/(n-1)
D
u∞(n-1)

Correct : b

Similar Questions

If → denotes increasing order of intensity, then the meaning of the words dry → arid → parched is analogous to diet → fast → ______. Which one of the given opt...
#10 MCQ
If two positive non-zero real variables x and y are such that (x+y) is proportional to x/y, then x+y:
#11 MCQ
Consider the following sample of numbers: 9, 18, 11, 14, 15, 17, 10, 69, 11, 13. The median of the sample is
#12 MCQ

Related Topics

steady incompressible flow flat plate boundary layer control volume analysis mass conservation equation GATE Aerospace Engineering 2022 GATE AE 2022 Q16 fluid mechanics flow velocity profile calculation

Unique Visitor Count

Total Unique Visitors

Loading......

Question Options

Contributed by: