Fundamentals of Airplane Flight Mechanics

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Beschreibung

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.

Zusammenfassung

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. It presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. 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 readers with the sizes of the numbers. A subsonic business jet is used for these calculations.

Inhaltsverzeichnis

to Airplane Flight Mechanics.- 3DOF Equations of Motion.- Atmosphere, Aerodynamics, and Propulsion.- Cruise and Climb of an Arbitrary Airplane.- Cruise and Climb of an Ideal Subsonic Airplane.- Take-off and Landing.- PS and Turns.- 6DOF Model: Wind Axes.- Static Stability and Control.- 6DOF Model: Body Axes.- Dynamic Stability and Control.

Details

Erscheinungsjahr:	2010
Fachbereich:	Raumfahrttechnik
Genre:	Technik
Rubrik:	Naturwissenschaften & Technik
Medium:	Taschenbuch
Inhalt:	xiii 298 S.
ISBN-13:	9783642079870
ISBN-10:	3642079873
Sprache:	Englisch
Ausstattung / Beilage:	Paperback
Einband:	Kartoniert / Broschiert
Autor:	Hull, David G.
Auflage:	Softcover reprint of hardcover 1st ed. 2007
Hersteller:	Springer-Verlag GmbH Springer Berlin Heidelberg
Maße:	235 x 155 x 17 mm
Von/Mit:	David G. Hull
Erscheinungsdatum:	14.10.2010
Gewicht:	0,476 kg

Artikel-ID: 107211480

Zusammenfassung

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. It presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. 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 readers with the sizes of the numbers. A subsonic business jet is used for these calculations.

Inhaltsverzeichnis

Details

Erscheinungsjahr:	2010
Fachbereich:	Raumfahrttechnik
Genre:	Technik
Rubrik:	Naturwissenschaften & Technik
Medium:	Taschenbuch
Inhalt:	xiii 298 S.
ISBN-13:	9783642079870
ISBN-10:	3642079873
Sprache:	Englisch
Ausstattung / Beilage:	Paperback
Einband:	Kartoniert / Broschiert
Autor:	Hull, David G.
Auflage:	Softcover reprint of hardcover 1st ed. 2007
Hersteller:	Springer-Verlag GmbH Springer Berlin Heidelberg
Maße:	235 x 155 x 17 mm
Von/Mit:	David G. Hull
Erscheinungsdatum:	14.10.2010
Gewicht:	0,476 kg