Hostname: page-component-586b7cd67f-2plfb Total loading time: 0 Render date: 2024-11-25T02:11:34.723Z Has data issue: false hasContentIssue false
  • English
  • Français

Wake Curvature and the Kutta Condition in Laminar Flow

Published online by Cambridge University Press:  07 June 2016

S N Brown  and
K Stewartson
S N Brown
Affiliation:
Department of Mathematics, University College, London
K Stewartson
Affiliation:
Department of Mathematics, University College, London
Get access

Summary

The velocity defect in the wake and its curvature lead to a pressure jump across it. As a result the pressure distribution on the aerofoil and the lift are modified.

Type
Research Article
Information
Aeronautical Quarterly , Volume 26 , Issue 4 , November 1975 , pp. 275 - 280
Copyright
Copyright © Royal Aeronautical Society. 1975

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

1 Brown, S N Stewartson, K Trailing-edge stall. Journal of Fluid Mechanics, Vol 42, p 561, 1970.Google Scholar
2 Melnik, R E Chow, R Asymptotic theory of two-dimensional trailing-edge flows. NASA Conference on Aerodynamic Analysis Requiring Advanced Computation, Hampton, Va, 1975.Google Scholar
3 Spence, D A Wake curvature and the Kutta condition. Journal of Fluid Mechanics, Vol 44, p 625, 1970.Google Scholar
4 Goldstein, S Concerning some solutions of boundary-layer equations in hydrodynamics. Proceedings, Cambridge Philosophical Society, Vol 26, p l, 1930.Google Scholar
5 Stewartson, K Multi-structured boundary layers on flat plates and related bodies. Advances in Applied Mechanics XIV, Academic Press, p 145, 1974.Google Scholar