Effect of streamline contouring in the wing-fuselage juncture in combination with the supersonic area rule on a sweptback-wing-fuselage configuration of high fineness ratio
1960
19 S
Ill., graph. Darst
Book
English
Turbulent flow around a wing-fuselage type juncture
AIAA | 1985
|Turbulent flow around a wing/fuselage-type juncture
NTRS | 1986
|Flow control in a wing/fuselage-type juncture
AIAA | 1988
|