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Low speed aerodynamics of canard configurations
Published online by Cambridge University Press: 04 July 2016
Summary
Numerical methods have been developed for the prediction of aerodynamic characteristics of canard wing configurations by considering both attached and separated flow over the canard surface; the flow over the main wing surface is always assumed to be attached. Experimental tests have been conducted in a low speed wind tunnel to compare the theoretical results predicted by the numerical methods. The comparison shows good agreement up to approximately 16° incidence.
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- Copyright © Royal Aeronautical Society 1989
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