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Theory of an Accelerated Slender Supersonic Aerofoil

Published online by Cambridge University Press:  07 June 2016

Geoffrey L. Sewell
Geoffrey L. Sewell*
Affiliation:
University College, Hull
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Summary

The problem of a uniformly accelerated slender supersonic aerofoil is solved in this paper by a perturbation method for the cases when the acceleration is small. Full account is taken of the effect of the acceleration on the form of the shock line.

Type
Research Article
Information
Aeronautical Quarterly , Volume 5 , Issue 1 , May 1954 , pp. 52 - 54
Copyright
Copyright © Royal Aeronautical Society. 1954

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References

Sewell, G. L. (1950). Theory of an Oscillating Supersonic Aerofoil. Aeronautical Quarterly, May 1950.Google Scholar