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Published online by Cambridge University Press:  04 July 2016

N. le S. Filleul*
Affiliation:
Royal Military College of Science

Abstract

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Type
Technical notes
Copyright
Copyright © Royal Aeronautical Society 1964

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References

1. Stratford, B. S. The Speed of Sound and Mach Number Effects. Journal of the Royal Aeronautical Society, Vol. 67, p. 797, December 1963.CrossRefGoogle Scholar
2. Pearson, H., Holliday, J. B. and Smith, S. F. A Theory of the Cylindrical Ejector Supersonic Propelling Nozzle. Journal of the Royal Aeronautical Society, Vol. 62, No. 574, p. 746, October 1958.CrossRefGoogle Scholar
3. Filleul, N. le S. Basic Theory of the Supersonic Ejector Nozzle. (1963, Unpublished.)Google Scholar
4. Tyler, J. M. and Sofrin, T. G. S.A.E. Paper 345D (Section 4.4), 1961.Google Scholar