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Prandtl-Batchelor flow on a circularcylinder and on aerofoil sections

Published online by Cambridge University Press:  04 July 2016

G. Giannakidis
G. Giannakidis*
Affiliation:
Department of AeronauticsImperial College of Science, Technology and MedicineLondon, UK
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Abstract

Steady, inviscid, incompressible, two dimensional flowscontaining vortex patches bounded by vortex sheetsare used to model finite separated regions oncertain closed bodies as an approach to modellingseparation bubbles. First of all the problem of avortex patch on a circle is considered. Calculationswere done for symmetric flows covering a wide rangeof values of the separation position, the strengthof the vortex sheet and the circulation at infinityand for non-symmetric flows at various angles ofincidence. Smooth separation was detected in somecases. This model is used as an intermediate stepfor the calculation of the flow around an ellipseand a Joukowski aerofoil with the use of theJoukowski transformation.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 100 , Issue 991 , January 1996 , pp. 15 - 26
Copyright
Copyright © Royal Aeronautical Society 1996 

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