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Hypersonic flow over spiked cones

Published online by Cambridge University Press:  28 March 2006

C. J. Wood
C. J. Wood
Affiliation:
Department of Aeronautics, Imperial College, London University
Now at the Engineering Laboratory, University of Oxford.
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Abstract

An investigation has been made of the flow over spiked cone-cylinders mainly at a Mach number of 10. Five distinct types of flow were discovered. The occurrence of each is defined in terms of spike length and cone angle.

Following a discussion of the flow mechanism, a semi-empirical separation relation is derived. This can be used to predict the flow pattern for the most common type of separated flow.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 12 , Issue 4 , April 1962 , pp. 614 - 624
Copyright
© 1962 Cambridge University Press

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