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:
Correct : b
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