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Question: 2 an airplane wing planform area 50 m2 aircraft lift...

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2. An airplane (wing planform area 50 m2, aircraft lift coefficient C0.6, zero-lift drag coefficient C0.01, Oswald factor 0.90, aspect ratio 6) is flying straight and level at 10,000 m. Its true air speed in body-fixed coordinates is given as: 192.45 ms-1 51.764 ms-1 16.837 ms-1 lu v ) Calculate the body-fixed force vector Y resulting from lift and drag. (20 points).

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