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Oblique slot blowing into a supersonic laminar boundary layer

Published online by Cambridge University Press:  24 October 2008

N. Riley
N. Riley
Affiliation:
School of Mathematics and Physics, University of East Anglia, Norwich
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Extract

The response of a supersonic laminar boundary layer is considered when fluid is blown obliquely into it from a slot in the boundary. The velocity and length scales associated with the slot blowing are chosen in such a way that the triple-deck theory of Stewartson (9) may be exploited. It is shown that, depending upon the blowing angle, there can be either a compressive or expansive interaction between the boundary layer and free stream upstream from the slot.

Type
Research Article
Information
Mathematical Proceedings of the Cambridge Philosophical Society , Volume 80 , Issue 3 , November 1976 , pp. 541 - 554
Copyright
Copyright © Cambridge Philosophical Society 1976

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References

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