A Flight Investigation Of The Wake Turbulence Alleviation Resulting From A Flap Configuration Change On A B 747 Aircraft
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Aircraft Wake Vortices
| Author | : James N. Hallock |
| Publisher | : |
| Total Pages | : 396 |
| Release | : 1991 |
| Genre | : Aerodynamics |
| ISBN | : |
Aeronautical Engineering
| Author | : |
| Publisher | : |
| Total Pages | : 116 |
| Release | : 1978 |
| Genre | : Aeronautics |
| ISBN | : |
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Air Transportation Bibliography
| Author | : United States. Federal Aviation Administration. Office of Systems Engineering Management |
| Publisher | : |
| Total Pages | : 252 |
| Release | : 1978 |
| Genre | : Aeronautics |
| ISBN | : |
Government Reports Annual Index
| Author | : |
| Publisher | : |
| Total Pages | : 1204 |
| Release | : 1978 |
| Genre | : Research |
| ISBN | : |
Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.
Flight Stability and Automatic Control
| Author | : Robert C. Nelson |
| Publisher | : |
| Total Pages | : 464 |
| Release | : 1998 |
| Genre | : History |
| ISBN | : |
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Introduction to Aircraft Flight Mechanics
| Author | : Thomas R. Yechout |
| Publisher | : AIAA |
| Total Pages | : 666 |
| Release | : 2003 |
| Genre | : Aerodynamics |
| ISBN | : 9781600860782 |
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
