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Fundamentals of Airplane Flight Mechanics 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. Full description
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Revue de presse :
"There are two basic problems in airplane mechanics: (1) given an airplane, what are its performance, stability and control characteristics? and (2) given performance, stability and control characteristics, what is the airplane? The book is concerned with the first problem, but its organization is motivated by the structure of the second problem. ... The book is not only a very good educational tool, but also a competent research exposition monograph, and it is recommended to students and researchers in flight mechanics." --Adrian Carabineanu, Zentralblatt MATH, Vol. 1126 (3), 2008
"The text under review addresses performance, stability, and control (static and dynamic) characteristics of aircraft from the viewpoint, according to the author, of a one semester, junior-level course on these topics. ... It is readable, at an appropriate level for undergraduates ... . It is also a good choice to help a more experienced person to come up to speed on basic flight mechanics. I certainly recommend it for these situations." --Keith Koenig, SIAM Review, Vol. 49 (4), 2007
Présentation de l'éditeur :
"The text under review addresses performance, stability, and control (static and dynamic) characteristics of aircraft from the viewpoint, according to the author, of a one semester, junior-level course on these topics. ... It is readable, at an appropriate level for undergraduates ... . It is also a good choice to help a more experienced person to come up to speed on basic flight mechanics. I certainly recommend it for these situations." --Keith Koenig, SIAM Review, Vol. 49 (4), 2007
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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- ÉditeurSpringer
- Date d'édition2010
- ISBN 10 3642079873
- ISBN 13 9783642079870
- ReliureBroché
- Nombre de pages312
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Fundamentals of Airplane Flight Mechanics by Hull, David G. G. [Paperback ]
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Description du livre Etat : New. PRINT ON DEMAND Book; New; Fast Shipping from the UK. No. book. N° de réf. du vendeur ria9783642079870_lsuk
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Fundamentals of Airplane Flight Mechanics
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Description du livre Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -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. 312 pp. Englisch. N° de réf. du vendeur 9783642079870
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Fundamentals of Airplane Flight Mechanics
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Description du livre Etat : New. pp. 314. N° de réf. du vendeur 263075266
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Fundamentals of Airplane Flight Mechanics
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Description du livre Etat : New. N° de réf. du vendeur I-9783642079870
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Fundamentals of Airplane Flight Mechanics
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Description du livre Taschenbuch. Etat : Neu. Druck auf Anfrage Neuware - Printed after ordering - 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. N° de réf. du vendeur 9783642079870
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Fundamentals of Airplane Flight Mechanics
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Description du livre Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. A new avenue to flight dynamics through equations of motionFocus put on the important issues: trajectory analysis and stability and controlComplete algorithms are presented for computing aerodynamicsFlight mechanics is the applic. N° de réf. du vendeur 5047041
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Description du livre Etat : New. Print on Demand pp. 314 125 Illus. N° de réf. du vendeur 5853981
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