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A hybrid method for transonic flow past multi-element aerofoils

Published online by Cambridge University Press:  21 April 2006

M. G. Hill  and
N. Riley
M. G. Hill
Affiliation:
School of Mathematics and Physics, University of East Anglia, Norwich NR4 7TJ, UK Present address: Department of Civil Engineering, University College, Swansea, SA2 8PP, UK.
N. Riley
Affiliation:
School of Mathematics and Physics, University of East Anglia, Norwich NR4 7TJ, UK
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Abstract

A method for calculating transonic potential flow past a multi-element aerofoil configuration is presented. The method is a hybrid method that is based upon a compressible-flow panel method, valid for subcritical flow, and a finite-difference method that is suitable for supercritical flow calculations. The effectiveness of the proposed method is demonstrated, first by application to a single aerofoil and then to a three-element aerofoil.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 170 , September 1986 , pp. 253 - 264
Copyright
© 1986 Cambridge University Press

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References

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