9.28 The lift and drag coefficients for a rectangular wing with a 10 m chord at takeoff

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9.28 The lift and drag coefficients for a rectangular wing with a 10 m chord at takeoff are 1.0 and 0.05, respectively. Determine the span needed to lift 3560 kN at a take-off speed of 282 km/h.

Determine the wing drag at this condition.

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