Flight 427, Gerry Byrne

Автор: E. Torenbeek; H. Wittenberg
Название: Flight Physics
ISBN: 9400790600 ISBN-13(EAN): 9789400790605
Издательство: Springer
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Цена: 9794.00 р.
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Описание: However, the very rst useful results of this research became ava- able a considerable length of time after the aviation pioneers had made their rst ights. Only after the rst motorized ights had been successfully made did researchers become more interested in the science of aviation, which from then on began to take shape.

Автор: N. Sundararajan; P. Saratchandran; Yan Li
Название: Fully Tuned Radial Basis Function Neural Networks for Flight Control
ISBN: 1441949151 ISBN-13(EAN): 9781441949158
Издательство: Springer
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Цена: 23508.00 р.
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Описание: Fully Tuned Radial Basis Function Neural Networks for Flight Control presents the use of the Radial Basis Function (RBF) neural networks for adaptive control of nonlinear systems with emphasis on flight control applications.

Автор: Ernst Heinrich Hirschel; Claus Weiland
Название: Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles
ISBN: 3642442951 ISBN-13(EAN): 9783642442957
Издательство: Springer
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Цена: 18284.00 р.
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Описание: In this book selected aerothermodynamic design problems in hypersonic vehicles are treated. Where applicable, it emphasizes the fact that outer surfaces of hypersonic vehicles primarily are radiation-cooled, an interdisciplinary topic with many implications.

Автор: David G. Hull
Название: Fundamentals of Airplane Flight Mechanics
ISBN: 3642079873 ISBN-13(EAN): 9783642079870
Издательство: Springer
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Цена: 10480.00 р.
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Описание:

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.