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On the viscous flow in the nose region of a symmetric blunt body in hypersonic flow

Published online by Cambridge University Press:  28 March 2006

B. S. H. Rarity
Affiliation:
Department of the Mechanics of Fluids, University of Manchester

Abstract

The flow field in the nose region of a blunt body in hypersonic flow is studied by considering the transport of vorticity and enthalpy. The entire region between body and shock is considered to be viscous, not necessarily thin in comparison with the nose radius of the body and to be of slowly varying density. The (given) post-shock vorticity need not be small and the density ratio ρs may either be small or near unity, the analysis being valid asymptotically at both limits.

It is found that the vorticity equation may be uncoupled from the total enthalpy equation if μ√ρ is constant. While the equations are not expected to be necessarily restricted to the immediate vicinity of the stagnation line, only there can the solution be written down explicitly; elsewhere, numerical integration is required.

Type
Research Article
Copyright
© 1966 Cambridge University Press

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References

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