Show that for unpowered flight (for which the lift, drag, and weight forces are in equilibrium) the

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Show that for unpowered flight (for which the lift, drag, and weight forces are in equilibrium) the glide slope angle, \(\theta\), is given by \(\tan \theta=C_{D} / C_{L}\).

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Munson Young And Okiishi's Fundamentals Of Fluid Mechanics

ISBN: 9781119080701

8th Edition

Authors: Philip M. Gerhart, Andrew L. Gerhart, John I. Hochstein

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