Hostname: page-component-7bb8b95d7b-fmk2r Total loading time: 0 Render date: 2024-09-18T17:17:31.721Z Has data issue: false hasContentIssue false

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

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Gadd, G. E. 1957 J. Aero. Sci. 24, 759.
Goldburg, A. & Cheng, S. I. 1961 J. Math. Mech. 10, 529.
Lighthill, M. J. 1953 Proc. Roy. Soc. A, 217, 478.
Messiter, A. F. 1969 To be published in SIAM J. Appl. Math.
Stewartson, K. 1951 Proc. Camb. Phil. Soc. 47, 545.
Stewartson, K. 1968 Proc. Roy. Soc. A, 306, 275.
Stewartson, K. 1969 Mathematika, 16, 106.
Stewartson, K. & Williams, P. G. 1969 To be published in Proc. Soy. Soc. A.
Stratford, B. S. 1954 Aero. Res. Coun. (London) Rep. Mem. no. 3002.