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The effects of a sound wave on the compressible boundary layer on a flat plate

Published online by Cambridge University Press:  28 March 2006

C. R. Illingworth
Affiliation:
Department of Mathematics, University of Manchester

Abstract

The boundary layer on a hot flat plate which is fixed at zero incidence in a slow stream carrying a progressive sound wave is investigated. Formulae are obtained for the skin friction and the heat transfer in the extreme cases when the frequency is very low and very high. In addition, different methods of simplifying the boundary layer equations in unsteady compressible flow are briefly compared.

Type
Research Article
Copyright
© 1958 Cambridge University Press

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References

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