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A model airplane has a wing span of 3.1 ft and a chord (leading edge–trailing edge distance) of 5 in. The model flies in air at 60F^{\circ}F and atmospheric pressure. The wing can be regarded as a flat plate so far as drag is concerned. (a) At what speed will a turbulent boundary layer start to develop on the wing? (b) What will be the total drag force on the wing just before turbulence appears?

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Given:
Air at 60°F60\degree\mathrm{F} and atmospheric pressure\text{atmospheric pressure}
Wing Span, L=3.1 ftL = 3.1 ~ \mathrm{ft}
Leading Edge Distance, x=5 inx = 5 ~ \mathrm{in}

Required:
Velocity at which Turbulence starts to occur, UU
Drag Force on Wing, FsF_s

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