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.
1990-01-01
Conference paper
Electronic Resource
English
Estimation of the Wing Lift Distribution of the STOL Experimental Aircraft, “ASKA”
SAE Technical Papers | 1994
|NASA propulsive lift STOL technology program
NTRS | 1973
|