89 research outputs found
Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model
Flight Tests of a Model of a High-wing Transport Vertical-take-off Airplane with Tilting Wing and Propellers and with Jet Controls at the Rear of the Fuselage for Pitch and Yaw Control
An investigation of the stability and control of a high-wing transport vertical-take-off airplane with four engines during constant-altitude transitions from hovering to normal forward flight was conducted with a remotely controlled free-flight model. The model had four propellers distributed along the wing with the thrust axes in the wing chord plane. The wing could be rotated to 90 degrees incidence so that the propeller thrust axes were vertical for hovering flight. An air jet at the rear of the fuselage provided pitch and yaw control for hovering and low-speed flight
Transition-flight Tests of a Model of a Low-wing Transport Vertical-take-off Airplane with Tilting Wing and Propellers
An investigation of the stability and control of a low-wing four-engine transport vertical-take-off airplane during the transition from hovering to normal forward flight has been conducted with a remotely controlled free-flight model. The model had four propellers distributed along the wing with the thrust axes in the wing-chord plane. The wing could be rotated to 90 degrees incidence so that the propeller thrust axes were vertical for hovering flight
Hovering-flight Tests of a Model of a Transport Vertical-take-off Airplane with Tilting Wing and Propellers
A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model
Additional Studies of the Stability and Controllability of an Unswept-wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques
Dynamic Stability and Control Characteristics of a Delta-wing Vertically Rising Airplane Model in Take-offs, Landings and Hovering Flight
Dynamic Stability and Control Characteristics of a Vertically Rising Airplane Model in Hovering Flight
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