| 書目名稱 | Fundamentals of Airplane Flight Mechanics | | 編輯 | David G. Hull | | 視頻video | http://file.papertrans.cn/351/350120/350120.mp4 | | 概述 | A new avenue to flight dynamics through equations of motion.Focus put on the important issues: trajectory analysis and stability and control.Complete algorithms are presented for computing aerodynamic | | 圖書封面 |  | | 描述 | .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. . | | 出版日期 | Textbook 2007 | | 關(guān)鍵詞 | 6DOF; Control; Stability; Trajectory Analysis; algorithm; algorithms; mechanics | | 版次 | 1 | | doi | https://doi.org/10.1007/978-3-540-46573-7 | | isbn_softcover | 978-3-642-07987-0 | | isbn_ebook | 978-3-540-46573-7 | | copyright | Springer-Verlag Berlin Heidelberg 2007 |
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