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- W2317375522 abstract "Abstract : Close-coupled wing-canard configurations are ideally suited to applications in which high aircraft maneuverability is required at moderate speeds. The SAAB Viggen has exploited the advantages of placing canard and wing close together, but no theory has been capable of predicting the aerodynamics of this aircraft. In this investigation Sacks' method of simulating vortex sheets with distributions of discrete vortices has been applied to the study of the interaction of a slender wing with a nearly canard surface. The canard is detrimental to both lift and static longitudinal stability. The extent of canard wake roll-up is important in the interaction, and the flatter the wake the more adverse is the interaction. Downward canard deflection may lead to increases in lift of the entire configuration, and it is observed that for small vertical separations between the surfaces the forward portion of the wing is ineffective in producing lift. It is demonstrated that the canard can directly affect the pressure distribution on the wing and application of this configuration to direct lift control and control configured aircraft are noted. (Author)" @default.
- W2317375522 created "2016-06-24" @default.
- W2317375522 creator A5030665090 @default.
- W2317375522 date "1971-01-25" @default.
- W2317375522 modified "2023-09-27" @default.
- W2317375522 title "Nonlinear vortex interactions on wing-canard configurations" @default.
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- W2317375522 doi "https://doi.org/10.2514/6.1971-95" @default.
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