Estimate extent of laminar boundary layer flow along wing

Reference no: EM13298871

An airplane flies at a speed of 360 mph at an altitude of 5000 ft. If the boundary layers on the wing surfaces behave as those on a flat plate, estimate the extent of laminar boundary layer flow along the wing in feet. Assume a transitional Reynolds number of Re = 5*10^5

Reference no: EM13298871

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