A small aircraft has a wing area of 28 m2, a lift coefficient of 0.45 at takeoff settings, and a total mass of 2500 kg. Determine (a) the takeoff speed of this aircraft at sea level at standard atmospheric conditions, (b) the wing loading, and (c) the required power to maintain a constant cruising speed of 300 km/h for a cruising drag coefficient of 0.035.
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