Fundamentals of Airplane Flight Mechanics
David G. Hull, «Fundamentals of Airplane Flight Mechanics»
Springer | ISBN 3540465715 | 1 edition (March 2007) | PDF |2.3 Mb | 298 pages
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Fundamentals of Airplane Flight Mechanics
Synopsis:
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This text is concerned with the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. Algorithms are presented for calculating lift, drag, pitching moment, and stability derivatives. Flight mechanics is a discipline. As such, it has equations of motion, acceptable approximations, and solution techniques for the approximate equations of motion. Once an analytical solution has been obtained, numbers are calculated in order to compare the answer with the assumptions used to derive it and to acquaint students with the sizes of the numbers. A subsonic business jet is used for these calculations.
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related link:
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Stability Derivatives Flight Mechanics Plane Algorithms Airplane Flight Mechanics Problems Aerodynamic Control Solution Techniques Analytical Solution Vertical Plane Business Jet Analytical Solutions Derivation Approximations Assumptions Newton S Laws New
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