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Scaling of incipient separation in highspeed laminar flows

Published online by Cambridge University Press:  04 July 2016

G. R. Inger
G. R. Inger*
Affiliation:
College of Aeronautics*Cranfield Institute of Technology, UK
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Abstract

This study provides the theoretical foundation for awell-established, but.heretofore empirical,criterion for incipient separation in moderatelyhypersonic shock/boundary layer interactions. It isbased on an examination of the leading high Reynoldsnumber approximation to triple deck theory, combinedwith its reformulation in terms of the referencetemperature concept. The analysis further providesextensions giving the effects of both low supersonicMach numbers and non-adiabatic wall temperatures onincipient separation.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 98 , Issue 976 , July 1994 , pp. 227 - 231
Copyright
Copyright © Royal Aeronautical Society 1994 

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Footnotes

*

Visiting Professor; permanent address, Departmentof Aerospace Engineering and EngineeringMechanics, Iowa State University, Ames, Iowa,USA.

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