Dynamic Stability Analysis of Ducted Fan Type Flying Platforms, Phase IV
Flight Study of the Conversion Maneuver of a Tilt-Duct VTOL Aircraft
Wind-Tunnel Investigation of a 4-Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing
Development of the U.S. Army VZ 2 (Boeing Vertol-76) Research Aircraft
Wind Tunnel Test Report Conventional Model. Volume I. Low Speed Force and Moment Data
Effects of Airframe Geometry on Downwash Problems of Tandem Ducted-Propeller VTOL Aircraft
Fuselage Structural Analysis. Volume IV. Engine Inlet, Thrust Spoiler, Pitch Fan Louvers