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Physics, 28.11.2019 02:31 charlesiarenee0

Consider lifting potential flow around a spinning circular cylinder of radius r put in uniform flow with a velocity magnitude ofv[infinity]. if the circulation around the cylinder is γ = 2πv[infinity]r, (a)find the locations of the stagnation points, (b) determine and plot (with computer) the pressure coefficient distribution on the surface of the cylinder, and (c) calculate the lift and the drag coefficients.

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Consider lifting potential flow around a spinning circular cylinder of radius r put in uniform flow...

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