The steady plane flow in the figure has the polar velocity components vθ = Ωr and vr

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The steady plane flow in the figure has the polar velocity components vθ = Ωr and vr = 0. Determine the circulation Γ around the path shown.

R2 R1
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Fundamentals Of Momentum Heat And Mass Transfer

ISBN: 9781118947463

6th Edition

Authors: James Welty, Gregory L. Rorrer, David G. Foster

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