Effects of Wing Incidence on the Longitudinal Trim Characteristics of a Cambered 70 Deg delta-Wing Configuration at Mach Numbers 3.0 to 5.0
1960
53 pages
Report
No indication
English
Delta wing , Incidence , Trim , Wing camber , Aerodynamics , Afterbody , Body , Camber , Configuration , Control , Delta , Longitudinal , Moment , Negative , Stability , Supersonic , Test , Wing