Fundamentals of Airplane Flight Mechanics
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Fundamentals of Airplane Flight Mechanics by David G Hull
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives.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)
| SKU | Unavailable |
| ISBN 13 | 9783642079870 |
| ISBN 10 | 3642079873 |
| Title | Fundamentals of Airplane Flight Mechanics |
| Author | David G Hull |
| Condition | Unavailable |
| Binding Type | Paperback |
| Publisher | Springer-Verlag Berlin and Heidelberg GmbH & Co. KG |
| Year published | 2010-10-14 |
| Number of pages | 298 |
| Cover note | Book picture is for illustrative purposes only, actual binding, cover or edition may vary. |
| Note | Unavailable |