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On the laminar compressible boundary layer induced by the passage of a plane shock wave over a flat wall

Published online by Cambridge University Press:  24 October 2008

J. A. D. Ackroyd
J. A. D. Ackroyd
Affiliation:
Department of Aeronautical Engineering, Queen Mary College, University of London
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Summary

The laminar compressible boundary layer induced by the passage of a plane shock wave over a flat wall is examined in detail. Use is made of the empirical viscosity-temperature relationship μ ∝ Tω. The boundary-layer equations are solved numerically for various values of the index ω, Prandtl number and shock strengths. The resulting solutions are then used to construct simple semi-empirical relationships for some of the more important boundary-layer parameters.

Type
Research Article
Information
Mathematical Proceedings of the Cambridge Philosophical Society , Volume 63 , Issue 3 , July 1967 , pp. 889 - 907
Copyright
Copyright © Cambridge Philosophical Society 1967

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References

REFERENCES

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