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Trailing edge flows

Published online by Cambridge University Press:  29 March 2006

N. Riley
Affiliation:
University of East Anglia, Norwich
K. Stewartson
Affiliation:
University College, London

Abstract

The flow is examined in the neighbourhood of the trailing edge of slender aerodynamic shapes which terminate in either a cusp or a wedge. The manner in which the boundary layer reacts to the rapidly varying pressure field in such regions is analyzed using the method of matched asymptotic expansions. The case of a wedge is examined in greater detail and a criterion for separation to occur is established.

Type
Research Article
Copyright
© 1969 Cambridge University Press

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References

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