Technical Note - National Advisory Committee for Aeronautics
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1076 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
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Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1076 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Author | : James T. Matthews |
Publisher | : |
Total Pages | : 726 |
Release | : 1958 |
Genre | : Acceleration (Mechanics) |
ISBN | : |
A theoretical analysis was made to investigate the performance and acceleration-restriction capabilities of a normal-acceleration command control system in a fighter airplane. Several combinations of pitching velocity and pitching acceleration were investigated as feedback quantities in combination with normal acceleration.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 872 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 610 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Author | : Defense Documentation Center (U.S.) |
Publisher | : |
Total Pages | : 894 |
Release | : 1960 |
Genre | : Industrial arts |
ISBN | : |
Author | : Jonathan Craig Dutton |
Publisher | : |
Total Pages | : 232 |
Release | : 1993 |
Genre | : Science |
ISBN | : |