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The motion of a thin oil sheet under the steady boundary layer on a body

Published online by Cambridge University Press:  28 March 2006

L. C. Squire
Affiliation:
Royal Aircraft Establishment, Bedford

Abstract

A solution is obtained for the motion of a thin oil sheet, of non-uniform thickness, under a boundary layer. The following points are deduced: (a) The oil flows in the direction of the boundary-layer skin-friction, except near separation, where the oil tends to indicate separation too early. These conclusions are independent of oil viscosity. (b) The effect of the oil flow on the boundary-layer motion is very small.

The application of the results to the interpretation of oil-flow patterns is briefly considered.

Type
Research Article
Copyright
© 1961 Cambridge University Press

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References

Black, J. 1952 J. Roy. Aero. Soc. 56, 279.
Eichelbrenner, E. A. & Oudart, A. 1955 La Recherche Aeronautique, 47, 11.
Goldstein, S. (Ed.) 1938 Modern Developments in Fluid Dynamics. Oxford University Press.
Goldstein, S. 1948 Quart. J. Mech. Appl. Math. 1, 43.
Howarth, L. 1938 Proc. Roy. Soc. A, 164, 547.
Pankhurst, R. C. & Squire, H. B. 1950 Aero. Res. Counc., Lond., Curr. Pap. 80.
Prandtl, L. 1952 Essentials of Fluid Dynamics. London: Blackie.
Squire, L. C. 1956 Ph.D. Thesis, University of Bristol.
Stalker, R. J. 1955 Australian A.R.L. Report A 96.
Stanbrook, A. 1957 Aero. Res. Counc., Lond., Rep. & Mem. 3114.
Winter, K. G., Scott-Wilson, J. B. & Davies, F. V. 1954 Aero. Res. Counc., Lond., Curr. Pap. 212.