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Delta Wings of Shapes Amenable to Exact Shock-wave Theory

Part of: 75 year anniversary of Aeronautical Engineering at Glasgow University

Published online by Cambridge University Press:  04 July 2016

T. Nonweiler
T. Nonweiler*
Affiliation:
Department of Aeronautics and Fluid Mechanics, University of Glasgow
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Summary

A class of delta wings is considered, whose under-surface has an inverted-V, or inverted-W, cross section of such a form that, at the “design” Mach number and incidence, the shock waves formed are plane. The geometry of the shock-wave system and surface is described briefly, and comments made about the utility of the concept in relation to hypersonic flow studies.

Type
Research Article
Information
The Aeronautical Journal , Volume 67 , Issue 625 , January 1963 , pp. 39 - 40
Copyright
Copyright © Royal Aeronautical Society 1963

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References

1.Nonweiler, T. (1959). Aerodynamic Problems of Manned Space Vehicles. Journal of the Royal Aeronautical Society, Vol. 63, No. 585, pp. 521–528. September 1959.CrossRefGoogle Scholar
2.Maikapar, G. I. (1959). On the Wave Drag of Non-Axisymmetric Bodies at Supersonic Speeds (In Russian). PMM Vol. 23, No. 2, pp. 376–378. 1959.Google Scholar