Flight tests were conducted of a twin engine airplane modified to a STOL configuration with rotating cylinder flaps and interconnected propellers. The flight tests included verification of the functional operation of the rotating cylinder flap system and the determination of the low speed flying qualities and performance characteristics with emphasis on approach and landing.
Flight tests of a rotating cylinder flap on a North American Rockwell YOV-10 aircraft
1972-11-01
Report
No indication
English
Monograph: North American Rockwell X-15
Online Contents | 1997
North American Rockwell RA-5C Vigilante
Tema Archive | 1973
|Die North American Space Division von Rockwell International
Tema Archive | 1973