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The Pressure Distribution Due to Incidence on a Slender Elliptic Half–Cone

Published online by Cambridge University Press:  28 July 2016

C. R. Taylor
C. R. Taylor*
Affiliation:
Imperial College
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Extract

The slender–body solution for the flow about low aspect–ratio wings of non–zero thickness yields a pressure distribution which is valid in the vicinity of the leading edge and therefore suitable for comparison with measured distributions. In this note an expression is derived for the theoretical pressure distribution, due to small incidence, on a slender elliptic half–cone in uniform motion. It is shown that this distribution is additive to the zero incidence pressure distribution. A comparison with some low speed measurements shows qualitative agreement.

The method can be simply extended to other bodies of elliptic cross section.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 59 , Issue 538 , October 1955 , pp. 694 - 695
Copyright
Copyright © Royal Aeronautical Society 1955

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References

1. Ward, G. N. Linearized Theory of Steady High Speed Flow, Part III. Cambridge University Press.Google Scholar
2. Milne–Thompson, L. M. Theoretical Hydrodynamics, 2nd Edition, pp. 157–161. Macmillan.Google Scholar
3. Fraenkel, L. E. (1952). Supersonic Flow past Slender Bodies of Elliptic Cross Section. To be published as R. & M. 2954.Google Scholar