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- W2335565554 abstract "Vortex panel and vortex lattice methods have been utilized in an analytic study to determine the two- and three-dimensional aerodynamic behavior of canard and wing configurations. The purpose was to generate data useful for the design of general aviation canard aircraft. Essentially no two-dimensional coupling was encountered and the vertical distance between the lifting surfaces was found to be the main contributor to interference effects of the three-dimensional analysis. All canard configurations were less efficient than a forward wing with an aft horizontal tail, but were less sensitive to off-optimum division of total lift between the two surfaces, such that trim drag could be less for canard configurations. For designing a general aviation canard aircraft, results point toward large horizontal and vertical distance between the canard and wing, a large wing-to-canard area ratio, and with the canard at a low incidence angle relative to the wing." @default.
- W2335565554 created "2016-06-24" @default.
- W2335565554 creator A5005544439 @default.
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- W2335565554 date "1984-01-09" @default.
- W2335565554 modified "2023-09-27" @default.
- W2335565554 title "Aerodynamic canard/wing parametric analysis for general aviation applications" @default.
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- W2335565554 doi "https://doi.org/10.2514/6.1984-560" @default.
- W2335565554 hasPublicationYear "1984" @default.
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