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Engineering, 26.11.2019 05:31 kaizodude

The induced drag generated on the wing of a cirrus jet is 210 n. the wing has a wing area of 17 m2, an aspect ration of 8.5 and a span efficiency factor of 0.8. the plane is cruising at 220 km/hr at sea level. determine the weight of the aircraft.

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The induced drag generated on the wing of a cirrus jet is 210 n. the wing has a wing area of 17 m2,...

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