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Applications of Linearised Characteristics to Sharp-Edged Conical Bodies

Published online by Cambridge University Press:  07 June 2016

L. C. Squire
L. C. Squire*
Affiliation:
Engineering Department, University of Cambridge
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Summary

A review of existing work in the field of linearised characteristics suggests that the hypersonic approximation introduced by Chapkis should be adequate in many cases of practical interest; furthermore, of the methods available, this approximation requires least computation for the calculation of pressure distributions on a given shape at given speed. The application of this method to sharp-edged conical shapes shows good agreement with measured zero-incidence pressure distributions for a variety of shapes and a wide range of hypersonic parameter. The agreement is less good at incidence, possibly due to flow separations in the real flow.

Type
Research Article
Information
Aeronautical Quarterly , Volume 16 , Issue 1 , February 1965 , pp. 1 - 14
Copyright
Copyright © Royal Aeronautical Society. 1965

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References

1. Chapkis, R. L. Hypersonic Flow over an Elliptic Cone; Theory and Experiment. Journal of the Aerospace Sciences, Vol. 28 p. 844, 1961.Google Scholar
2. Ferri, A. The Linearised Characteristics Method and its Application to Practical Non-Linear Supersonic Problems. N.A.C.A. Report 1102, 1952.Google Scholar
3. Vaglio-Laurin, R. and Van Dyke, M. D. A Discussion of Higher-Order Approximations for the Flow Field about a Slender Elliptic Cone. Journal of Fluid Mechanics, Vol. 3 p. 638, 1958.Google Scholar
4. Martellucci, A. An Extension of the Linearised Characteristics Method for Calculation of the Supersonic Flow about Elliptic Cones. Journal of the Aerospace Sciences, Vol. 27 p. 667, 1960.Google Scholar
5. Squire, L. C. Pressure Distributions and Flow Patterns on some Conical Shapes with Sharp Edges and Symmetrical Cross-Sections at M=4-0. R. & M. 3340, 1963.Google Scholar
6. Britton, J. W. Pressure Measurements at Supersonic Speeds on Three Uncambered Conical Wings of Unit Aspect Ratio. A.R.C. Current Paper 641, 1963.Google Scholar