A small aircraft has a wing area of 35 m2, a lift coefficient of 0.45 at takeoff settings, and a total mass of 4000 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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A small aircraft has a wing area of 35 m2, a lift
coefficient of 0.45 at takeoff settings, and a total mass of
4000 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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