Propulsive lift augmentation by side fences as applied to Japan's experimental STOL aircraft, ASKA
Flight Simulation Technologies Conference and Exhibit ; 1990 ; Dayton , OH , U.S.A.
01.01.1990
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Estimation of the Wing Lift Distribution of the STOL Experimental Aircraft, “ASKA”
SAE Technical Papers | 1994
|NASA propulsive lift STOL technology program
NTRS | 1973
|