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- W1659720116 abstract "The Los Angeles Chapter of the American Institute of Aero andAstronautics is building two replicas of the 1903 Wright Flyer airplane;one to wind-tunnel test and display, and a modified one to fly. As partof this project the aerodynamic characteristics of the Flyer are beinganalyzed by modern wind-tunnel and analytical techniques. Tnis paperdescribes the Wright Flyer Project, and compares key results fromsmall-scale wind-tunnel tests and from vortex-lattice computations forthis multi-biplane canard configuration. Analyses of the stability andcontrol properties are summarized and their implications for closed-loopcontrol by a pilot are derived using quasilinear pilot-vehicle analysisand illustrated by simulation time histories.It is concluded that, although the Wrights were very knowledgeableand ingenious with respect to aircraft controls and their interactions(e.g., the good effects of their wing-warp-to-rudder linkage arevalidated), they were largely ignorant of dynamic stabilityconsiderations. The paper shows that the 1903 Flyer was readilycontrollable about all axes but was intrinsically unstable in pitch androll, and it could barely be stabilized by a skilled pilot." @default.
- W1659720116 created "2016-06-24" @default.
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- W1659720116 date "1985-09-20" @default.
- W1659720116 modified "2023-09-27" @default.
- W1659720116 title "Aerodynamics, Stability and Control of the 1903 Wright Flyer" @default.
- W1659720116 hasPublicationYear "1985" @default.
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