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Longitudinal stability and control of a tilt-wing vtol aircraft with rigid and flapping propeller blades
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TLDR
Longitudinal stability and control of a tilt-wing vtol aircraft model with rigid and flapping propeller blades was studied in this article, where the model was equipped with a single propeller.Abstract:
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Citations
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NASA Langley Distributed Propulsion VTOL Tilt-Wing Aircraft Testing, Modeling, Simulation, Control, and Flight Test Development
Paul M. Rothhaar,Patrick C. Murphy,Barton J. Bacon,Irene M. Gregory,Jared A. Grauer,Ronald C. Busan,Mark A. Croom +6 more
TL;DR: An overview of the techniques and advances required to develop the GL-10 tilt-wing, tilt-tail, long endurance, VTOL aircraft control system is provided.
Proceedings ArticleDOI
NASA Langley Distributed Propulsion VTOL TiltWing Aircraft Testing, Modeling, Simulation, Control, and Flight Test Development
Journal ArticleDOI
Dynamic stability of V/STOL aircraft at low speeds
TL;DR: Fry, B. L. and Zabinsky, J. M., "Feasibility of V/STOL Concepts for Short-Haul Transport Aircraft" CR-743, 1967, NASA as discussed by the authors.
References
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Force-Test Investigation of the Stability and Control Characteristics of a 1/4-Scale Model of a Tilt-Wing Vertical-Take-Off-and-Landing Aircraft
William A. Newsom,Louis P. Tosti +1 more
TL;DR: In this paper, a wind-tunnel investigation has been made to determine the aerodynamic characteristics of a 1/4-scale model of a tilt-wing vertical-take-off-and-landing aircraft.
Rapid-Transition Tests of a 1/4-Scale Model of the VZ-2 Tilt-Wing Aircraft
TL;DR: In this article, the longitudinal stability and control characteristics of a 1/4-scale model of the VZ-2 tilt-wing vertical-take-off-and-landing aircraft during rapid transitions has been made on the Langley control-line facility.