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Engineering, 29.09.2019 01:10 tae8002001

Calculate the local reynolds number at a point 0.1 ft aft of the leading edge of a wing, which is being tested at sea level, standard day conditions, and at 800 ft/s (545 mph) true airspeed. what type of boundary layer exists at this point? assume recrit = 5 x 10^5

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Calculate the local reynolds number at a point 0.1 ft aft of the leading edge of a wing, which is be...

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