A small aircraft has a wing area of 35 m 2 , a lift coefficient of 0.45
Question:
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,
(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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Related Book For
Fundamentals of Thermal-Fluid Sciences
ISBN: 978-0078027680
5th edition
Authors: Yunus A. Cengel, Robert H. Turner, John M. Cimbala
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