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Introduction to flight testing and applied aerodynamics /
"This textbook presents a basic and concise analysis of airplane performance, stability, and control. Basic algebra, trigonometry, and some calculus are used. Topics discussed include engine and propeller performance, estimation of drag, airplane dynamics, wing spanwise lift distributions, flig...
| Clasificación: | Libro Electrónico |
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| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
©2011.
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| Colección: | AIAA education series.
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| Temas: | |
| Acceso en línea: | Texto completo |
| Sumario: | "This textbook presents a basic and concise analysis of airplane performance, stability, and control. Basic algebra, trigonometry, and some calculus are used. Topics discussed include engine and propeller performance, estimation of drag, airplane dynamics, wing spanwise lift distributions, flight experimentation, airspeed calibration, takeoff performance, climb performance, and dynamic and static stability. Special features examples containing student-obtained data about specific airplanes and engines; simple experiments that determine an airplane's performance and handling qualities;and end-of-chapter problems (with answers supplied in an appendix)."--Publisher description |
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| Descripción Física: | 1 online resource (ix, 133 pages) : illustrations |
| Bibliografía: | Includes bibliographical references (page 127) and index. |
| ISBN: | 1600868290 9781600868290 9781600868283 1600868282 |