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Cavities at atmospheric pressure behind two-dimensional bodies at an angle of attack

Published online by Cambridge University Press:  17 February 2009

P. M. Haese
P. M. Haese
Affiliation:
School of Applied Mathematics, The University of Adelaide, Adelaide SA 5005, Australia; e-mail: phaese@maths.adelaide.edu.au.
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Abstract

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This paper presents an interior source method for the calculation of semi-infinite cavities behind two-dimensional bluff bodies placed at an angle of attack in a uniform stream. Aspects under consideration include the pressure distribution along the body, especially just ahead of the separation point, lift and drag forces, and how these quantities vary with the angle of attack. We include discussion of the physical conditions of separation, and identify critical angles of attack for which the cavitating flow past an airfoil may (a) become unstable, or (b) yield the greatest lift to drag ratio.

Type
Research Article
Information
The ANZIAM Journal , Volume 47 , Issue 1 , July 2005 , pp. 103 - 119
Copyright
Copyright © Australian Mathematical Society 2005

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