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Question: a hawk trainer aircraft is flying at sea level with...

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A Hawk trainer aircraft is flying at sea level with a velocity of 210ms-1, if we consider its wing as a rectangular flat plate of span 9.4m and chord 1.78m, calculate the boundary layer thickness at the wing trailing edge and total skin friction (assume laminar boundary layer) (p 1.225 kg/m3, u - 1.8 x 105 kg/ms) 3. (1.76mm, 238N)

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