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Plate-injection into a separated supersonic boundary layer. Part 2. The transition regions

Published online by Cambridge University Press:  29 March 2006

K. Stewartson
K. Stewartson
Affiliation:
Department of Aeronautical and Astronautical Engineering, The Ohio State University, Columbus
Permanent address: Department of Mathematics, University College, London.
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Abstract

The model proposed by Smith & Stewartson (1973), to describe the separated boundary layer induced by strong injection over a finite length of a flat plate in a supersonic mainstream, is shown to provide the basis for a fully consistent solution of the Navier–Stokes equations for this problem, valid in the limit of infinite Reynolds number. The solution takes the form of asymptotic expansions in each of a large number of overlapping regions of the flow field, which are consistently matched across areas of common validity.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 62 , Issue 2 , 23 January 1974 , pp. 289 - 304
Copyright
© 1974 Cambridge University Press

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References

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