Experimental effects of fuselage camber on longitudinal aerodynamic characteristics of a series of wing-fuselage configurations at a Mach number of 1.41
1976
25 S.
graph. Darst.
Report
Englisch
Transonic flow over wing/fuselage configurations
NTRS | 1981
|Aerodynamic Centre of Wing-Fuselage Combinations
NTIS | 1976