Flight mechanics is the application of Newton's laws to the
study of vehicle trajectories (performance), stability, and
aerodynamic control. This volume details the derivation of
analytical solutions of airplane flight mechanics problems
associated with flight in a vertical plane.
It covers trajectory analysis, stability, and control. In
addition, the volume presents algorithms for calculating lift,
drag, pitching moment, and stability derivatives. Throughout, a
subsonic business jet is used as an example for the calculations
presented in the book.
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