Variable sweep aircraft Patent
Development and characteristics of variable sweep wing control system for supersonic aircraft
Engineering topics
Publications and source records attributed to Hammond, A. D..
Development and characteristics of variable sweep wing control system for supersonic aircraft
Wind tunnel investigation of hot-gas ingestion and jet interference effects on jet powered V/STOL aircraft
Wind tunnel model tests of hot gas ingestion and jet interference on jet V/STOL aircraft
Longitudinal stability and control characteristics of powered model of twin-propeller deflected-slipstream STOL aircraft configuration
Thrust power losses during hovering for jet VTOL AIRCRAFT, due to jet induced base loss and ground effects
Explore the source record for details and available documents.
Subsonic longitudinal characteristics of variable sweep aircraft utilizing free floating wing apex for alleviation of longitudinal stability and supersonic performance problems
Control requirements for high lift, lateral and longitudinal control systems of STOL aircraft
Wind tunnel tests of static lateral and directional control of twin-propeller deflected slipstream STOL aircraft
Lateral control & hinge moment of spoiler-slot- deflector on sweptback wing at subsonic speed
Leading edge and trailing edge flap deflection effect on high left and lateral control characteristics of semispan variable sweep wing and tail surfaces