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Calculation of two-dimensional and three-dimensional regular shock intersections

Published online by Cambridge University Press:  04 July 2016

B. L. Hunt
B. L. Hunt*
Affiliation:
Department of Aeronautical Engineering, University of Bristol
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Extract

The intersection of two oblique shock waves of opposite families is a common occurrence in supersonic flows. It can result either in a regular intersection, where the downstream waves are weak shocks and a single slip line emanates from the intersection, or in a form of Mach reflection where a strong shock bridges the gap between two three-shock confluences each of which generates a slip line. The transition between regular and Mach reflection has been discussed for the symmetrical case by Henderson and Lozzi and by Horning et al. The conditions at a three-shock confluence point have been analysed for two-dimensional flow by Henderson and for three-dimensional flow by Hunt and Lamont and by Rudman.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 84 , Issue 836 , September 1980 , pp. 285 - 289
Copyright
Copyright © Royal Aeronautical Society 1980 

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Footnotes

*

Now Manager, Propulsion Research, Northrop Corporation, Hawthorne, California.

References

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