"Sinopsis" puede pertenecer a otra edición de este libro.
From the reviews:
"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)
"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)
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.
"Sobre este título" puede pertenecer a otra edición de este libro.
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Descripción Soft Cover. Condición: new. Nº de ref. del artículo: 9783642079870
Descripción Condición: New. PRINT ON DEMAND Book; New; Fast Shipping from the UK. No. book. Nº de ref. del artículo: ria9783642079870_lsuk
Descripción Condición: New. Nº de ref. del artículo: ABLIING23Mar3113020216723
Descripción PF. Condición: New. Nº de ref. del artículo: 6666-IUK-9783642079870
Descripción Taschenbuch. Condición: 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. Nº de ref. del artículo: 9783642079870
Descripción Condición: New. Nº de ref. del artículo: I-9783642079870
Descripción Taschenbuch. Condición: 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. Nº de ref. del artículo: 9783642079870
Descripción Condición: 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. Nº de ref. del artículo: 5047041