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A Comparison of Two Integral Equation Methods for High Subsonic Lifting Flows

Published online by Cambridge University Press:  07 June 2016

D Nixon
D Nixon*
Affiliation:
Queen Mary College, University of London
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Summary

A comparison is made of two recently published integral equation methods for calculating the high subsonic flow around lifting and non-lifting aerofoils. It is shown that one method leads to a non-unique solution.

Type
Research Article
Information
Aeronautical Quarterly , Volume 26 , Issue 1 , February 1975 , pp. 56 - 58
Copyright
Copyright © Royal Aeronautical Society. 1975

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References

1 Nørstrud, H The transonic aerofoil problem with embedded shocks. Aeronautical Quarterly, Vol XXIV, pp 129–138, 1973.Google Scholar
2 Nixon, D Hancock, G J High subsonic flow past a steady two-dimensional aerofoil. ARC Current Paper 1280, 1974.Google Scholar