Flight Test Data On The Static Fore And Aft Stability Of Various German Airplanes
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| Author | : Walter Hübner |
| Publisher | : |
| Total Pages | : 668 |
| Release | : 1933 |
| Genre | : Airplanes |
| ISBN | : |
The static longitudinal stability of an airplane with locked elevator is usually determined by analysis and model tests. The present report proposes to supply the results of such measurements. The method consisted of recording the dynamic pressure versus elevator displacement at different center-of-gravity positions in unaccelerated flight.
| Author | : |
| Publisher | : |
| Total Pages | : 664 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1370 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 660 |
| Release | : 1933 |
| Genre | : Aeronautics |
| ISBN | : |
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
| Author | : |
| Publisher | : |
| Total Pages | : 736 |
| Release | : 1932 |
| Genre | : Aeronautics |
| ISBN | : |
Chiefly translations from foreign aeronautical journals.
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 456 |
| Release | : 1933 |
| Genre | : Aeronautics |
| ISBN | : |
Chiefly translations from foreign aeronautical journals.
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 2608 |
| Release | : |
| Genre | : Government publications |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 2606 |
| Release | : 1896 |
| Genre | : Government publications |
| ISBN | : |
| 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.
| Author | : Gotthold Mathias |
| Publisher | : |
| Total Pages | : 584 |
| Release | : 1934 |
| Genre | : Airplanes |
| ISBN | : |
The discussion of the structural methods for obtaining lateral stability discloses the remarkable influence of the constant fuselage and wing proportions to the yawing moments. For the effectiveness of modifications in vertical tail surfaces and tail length, these quotas - little observed heretofore, in this connection - are decisive. This also applies to the amount of dihedral of the wing with regard to the roll stability of the complete wing already existing without angle of the dihedral.
