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Engineering, 07.04.2020 20:32 samirahscott

Compute the Reynolds number of the Cessna 172S wing based on the mean geometric chord (S/b) at a cruise condition of 124 knots at 8,000 ft altitude. Show your work. Would you expect the flow over the wing to be mostly laminar or mostly turbulent

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Compute the Reynolds number of the Cessna 172S wing based on the mean geometric chord (S/b) at a cru...
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