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A note on the description of an attached supersonic boundary layer near a point of injection cut-off

Published online by Cambridge University Press:  29 March 2006

A. Amr  and
D. R. Kassoy
A. Amr
Affiliation:
Mechanical Engineering Department, University of Colorado, Boulder
D. R. Kassoy
Affiliation:
Mechanical Engineering Department, University of Colorado, Boulder
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Abstract

Supersonic boundary-layer flow on a flat plate near a point of injection cut-off is considered. The goal is to develop a non-singular solution in the limit of large Reynolds number in the vicinity of the boundary-condition change. An application of Goldstein-type singular solutions shows that an interaction-type theory is required even for transverse velocity jumps on the boundary O(R− ½). The interaction analysis is developed in terms of the linearized triple-deck theory described by Smith & Stewartson (1973a). The analytically derived solution provides a continuous pressure and wall-shear distribution.

Information

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 71 , Issue 3 , 14 October 1975 , pp. 455 - 463
Copyright
© 1975 Cambridge University Press

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References

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