Full-Scale Wind-Tunnel Investigation of a VTOL Aircraft with a Jet-Ejector System for Lift Augmentation
1966
51 pages
Report
No indication
English
Aircraft , Aerodynamics , Aerodynamic characteristics , Ejector , Lift augmentation , Vtol aircraft , Wind tunnel stability test , Aerodynamic , Augmentation , Full , Jet , Lateral , Lift , Longitudinal , Scale , Stability , Stall , Static , System , Test , Thrust , Tunnel , Vtol , Wind , Wing