138,97 €
163,49 €
Fundamentals of Airplane Flight Mechanics
138,97 € 
- Išsiųsime per 10–14 d.d.
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 t…
138.97
2025-07-06 23:59:00
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- Autorius: David G. Hull
- Leidėjas: Springer-Verlag GmbH
- Metai: 2007
- ISBN-10: 3540465715
- ISBN-13: 9783540465713
- Formatas: 16.4 x 24.3 x 2.5 cm, kieti viršeliai
- Kalba: Anglų
- Extra -15 % nuolaida šiai knygai su kodu: ENG15
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Aprašymas
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.EXTRA 15 % nuolaida
138,97 €
163,49 €
Išsiųsime per 10–14 d.d.
Kupono kodas: ENG15
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- Autorius: David G. Hull
- Leidėjas: Springer-Verlag GmbH
- Metai: 2007
- ISBN-10: 3540465715
- ISBN-13: 9783540465713
- Formatas: 16.4 x 24.3 x 2.5 cm, kieti viršeliai
- Kalba: Anglų
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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