The program to design and build a Buffalo/Spey Augmentor-Wing research aircraft is presented. The development of an internally blown flap system for the generation of powered lift is discussed. Modification, development, and testing of the Rolls-Royce Spey engine are reported. The ground tests and first flights of the aircraft are described and the application of the internally blown flap concept for short takeoff military transport aircraft is proposed.
The Buffalo/Spey jet-STOL research aircraft
01.04.1973
Aufsatz (Konferenz)
Keine Angabe
Englisch
Tema Archiv | 1975
Kraftfahrwesen | 1982
|Tema Archiv | 1974