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The Gossamer Condor was the first human-powered aircraft capable of controlled and sustained flight to prescribed figure-of-eight course around two turning points 1.6kmapart. It had a wing span of 29.26m\& wing chord of 2.29m. With a take of mass of 95.25kgthe aircraft flew at 4.57m/sin sea level conditions. Calculate the lift coefficient of the aircraft. Estimate the drag and power required to overcome the drag if the drag coefficient fthe aircraft is 0.046

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