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Supersonic flow over an inclined wing of zero aspect ratio
Published online by Cambridge University Press: 24 October 2008
Abstract
An asymptotic expression is found for the lift distribution on a long, narrow, laminar wing, at incidence in a supersonic stream. The approximations of the linearized potential theory are used.
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- Research Article
- Information
- Mathematical Proceedings of the Cambridge Philosophical Society , Volume 46 , Issue 2 , April 1950 , pp. 307 - 315
- Copyright
- Copyright © Cambridge Philosophical Society 1950
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