A Flight Investigation of an Acceleration Restrictor
Author | : Arthur Assadourian |
Publisher | : |
Total Pages | : 34 |
Release | : 1960 |
Genre | : Acceleration (Mechanics) |
ISBN | : |
Download A Flight Investigation Of An Acceleration Restrictor full books in PDF, epub, and Kindle. Read online free A Flight Investigation Of An Acceleration Restrictor ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : Arthur Assadourian |
Publisher | : |
Total Pages | : 34 |
Release | : 1960 |
Genre | : Acceleration (Mechanics) |
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 | : 860 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1026 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1812 |
Release | : 1960 |
Genre | : Government publications |
ISBN | : |
Author | : Richard C. Dingeldein |
Publisher | : |
Total Pages | : 650 |
Release | : 1954 |
Genre | : Rotors (Helicopters) |
ISBN | : |
The power requirements measured in static thrust and in level forward flight are presented for two helicopter rotor configurations. One is a coaxial rotor arrangement having the rotors spaced approximately 19 percent of the rotor radius; the other is a tandem configuration in which the rotor-shaft spacing is 3 percent greater than the rotor daimater and in which the rotors lie in the same plane. The experimental meausrements are compared with the results of calculations based on existing NACA single-rotor theory.
Author | : Sandra K. Faull |
Publisher | : Arlington, Va. : United States Historical Documents Institute |
Total Pages | : 608 |
Release | : 1979 |
Genre | : Reference |
ISBN | : |