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Some Aspects of the Design of Half-Ring Wing-Body Combinations with Prescribed Wing Loadings

Published online by Cambridge University Press:  07 June 2016

K. C. Moore  and
J. G. Jones
K. C. Moore
Affiliation:
Royal Aircraft Establishment, Bedford
J. G. Jones
Affiliation:
Royal Aircraft Establishment, Bedford
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Summary

This paper is concerned with half-ring wing-body combinations with prescribed wing loadings at supersonic speeds. Configuration shapes, their pressure distributions and their associated flow fields are discussed.

Type
Research Article
Information
Aeronautical Quarterly , Volume 16 , Issue 1 , February 1965 , pp. 55 - 82
Copyright
Copyright © Royal Aeronautical Society. 1965

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References

1. Beane, B. J. and Ryan, B. M. Supersonic Drag Calculations for a Cylindrical Shell Wing of Semi-Circular Cross-Section Combined with a Central Body of Revolution. Douglas Aircraft Company Report No. SM-22627, Santa Monica Division, October 1956.Google Scholar
2. Jones, J. G. Quasi-Cylindrical Surfaces with Prescribed Loadings in the Linearised Theory of Supersonic Flow. Quarterly Journal of Mechanics and Applied Mathematics, Vol. XV, Part 4 p. 471, November 1962.CrossRefGoogle Scholar
3. Hayes, W. D. Linearised Supersonic Flow. North American Aviation, Inc., Report No. AL-222, 1947.Google Scholar
4. Moore, K. C. and Jones, J. G. Quasi-Cylindrical Surfaces with Prescribed Thickness Distributions. Quarterly Journal of Mechanics and Applied Mathematics, Vol. XVI, Part 4 p. 521, November 1963.CrossRefGoogle Scholar
5. Jahnke, E., Emde, F. and Lösch, F. Tables of Higher Functions. McGraw-Hill, 1960.Google Scholar
6. Eminton, E. On the Minimisation and Numerical Calculation of Wave Drag. A.R.C. 19,212, November 1955.Google Scholar
7. Whitham, G. B. On the Propagation of Weak Shock Waves. Journal of Fluid Mechanics, Vol. 1, 1956.CrossRefGoogle Scholar
8. Browand, F. K., Beane, B. J. and Nowlan, D. T. The Design and Test at Mach Number 2-5 of Two Low-Wave-Drag Ring-Wing Configurations of Aspect Ratio 1-3 and 2-6. Rand Memorandum RM-2933-PR, June 1962.Google Scholar