A small aircraft has a wing area of 35 m 2 , a lift coefficient of 0.45

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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,

(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  book-img-for-question

Fundamentals of Thermal-Fluid Sciences

ISBN: 978-0078027680

5th edition

Authors: Yunus A. Cengel, Robert H. Turner, John M. Cimbala

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