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Axisymmetric hypersonic flow with strong viscous interaction

Published online by Cambridge University Press:  28 March 2006

John Webster Ellinwood  and
Harold Mirels
John Webster Ellinwood
Affiliation:
Aerospace Corporation, El Segundo, California
Harold Mirels
Affiliation:
Aerospace Corporation, El Segundo, California
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Abstract

Stewartson's theory for axisymmetric hypersonic flow of a model gas over slender bodies with strong viscous interaction and strong shock wave is extended to power-law viscosity variation and Prandtl numbers other than one. Flow properties at the body surface and shock are obtained without recourse to numerical integration. Numerical computations are presented for axisymmetric flow over a three-quarter power-law body with strong shock wave and viscous interactions that range from weak to strong.

Information

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 34 , Issue 4 , 23 December 1968 , pp. 687 - 703
Copyright
© 1968 Cambridge University Press

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