Design an untwisted elliptical wing to fly at 200 km/hr in sea-level air with the fol lowing specifications: lift = 45,000 N planform area = 30 m 2 wing span 12 m The absolute angle of attack α" cannot exceed 120 to avoid stall. For the wing of min- imum induced drag, specify its aspect ratio, wing span, maximum chord, the design a, and the power required to compensate induced drag. If the wing span is limited to within 10 m, can a wing be designed to meet all other specifications? Explain.
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