An Investigation of Supersonic Store Interference in the Vicinity of a 22 Deg Swept Wing Fuselage Configuration at Mach Numbers of 1.61 and 2.01
1958
106 pages
Report
No indication
English
Aerodynamics , Fluid Mechanics , Aircraft configuration , Swept wing , Wind tunnel , Wing-fuselage-store , Aircraft , Bomber , Configuration , Detachment , Drag , Force , Fuselage , Graph , Heavy , Interference , Lift , Moment , Pitch , Pressure , Store , Supersonic , Tunnel , Wind , Wing , Yaw