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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
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.
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- Research Article
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- Copyright
- Copyright © Royal Aeronautical Society. 1975
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
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