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Asymptotic theory of high-aspect-ratio arched wings in steady incompressible flow

Published online by Cambridge University Press:  26 April 2006

G. Iosilevskii
G. Iosilevskii
Affiliation:
Faculty of Aerospace Engineering, Technion, Haifa 32000, Israel
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Abstract

Asymptotic theory of high-aspect-ratio wings in steady incompressible flow is extended to a case where the wing forms either an open or closed circular arc. The generalization is based on an integral formulation of the problem, which resembles the one used by Guermond (1990) for a plane curved wing. A second-order approximation is obtained for the load distribution on two model wings, one resembling that of a gliding parachute, and the other resembling a short duct.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 303 , 25 November 1995 , pp. 367 - 377
Copyright
© 1995 Cambridge University Press

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