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Propulsion streamtubes in supersonic flow and supercritical intake cowl

Published online by Cambridge University Press:  04 July 2016

C. L. Bore*
Affiliation:
Formerly British Aerospace, Kingston

Summary

The proper treatment of the pre-entry and post-exit streamtubes of supersonic aircraft and their “corresponding” windtunnel models was considered in some depth for supersonic fighter designs, and investigated in wave drag research, but as a result of the cancellations of the major supersonic fighter programmes the results were not published. This note sets out the salient conclusions.

The development of the first supercritical air intake cowl is also outlined.

Type
Technical Note
Copyright
Copyright © Royal Aeronautical Society 1993 

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References

1. Bore, C.L. Some unpublished contributions to propulsion theory, Lecture to RAeS, 11 March 1992.Google Scholar
2. Bore, C.L. Area distribution optimisation for supersonic area rule, Hawker Aircraft POR 128, November 1961.Google Scholar
3. Bore, C.L. Area rule for aircraft having different area distributions either side of the wing plane, Hawker Aircraft POR 126, April 1961.Google Scholar
4. Eminton, E. On the Minimisation and Numerical Evaluation of Wave Drag, RAE Report 2564, November 1955.Google Scholar
5. Dove, P.H. A programme to compute the wave drag of a wing or wing-body combination using the R T Jones oblique plane method, Hawker Aircraft CPN 44, March 1960.Google Scholar
6. Bore, C.L. and Boyd, A.T. Correlation of predicted and experimental drag values: PI 150/1, Model K8, HSA Kingston PON 702, August 1963.Google Scholar
7. Strange, J.P. On the HSA wave-drag estimation program and the results obtained therefrom on TSR-2, HSA Kingston PON 1338, October 1968.Google Scholar
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10. Bore, C.L. Air intakes of the HS Harrier, Hawker Siddeley Technical Review, 5, (3).Google Scholar