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
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
References
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