A jet-STOL powered-lift aircraft has the ability to perform a relatively steep (7.5 deg) final approach at high power setting and a low speed. The DHC-5 Buffalo/Spey Augmentor-Wing research aircraft is the first machine of its kind to accomplish this performance. The aircraft uses an approach in which the cold bypass thrust is vectored by the augmentor flap. Aspects of aircraft reliability are discussed together with taxi trials, stalling characteristics, lateral directional control, single-engine operations, roll acceleration, and flight in turbulent conditions.
The augmentor wing - Powered-lift STOL a proven concept
Interavia ; 29
01.02.1974
Sonstige
Keine Angabe
Englisch
The Augmentor Wing - A new approach to jet STOL.
NTRS | 1967
|The external augmentor concept for V/STOL aircraft
NTRS | 1979
|Thrust augmentor application for STOL and V/STOL
NTRS | 1977
|