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The turbulent boundary layer on a rotating cylinder in an axial stream

Published online by Cambridge University Press:  29 March 2006

T-S. Cham
Affiliation:
Cambridge University Engineering Department Present address: Faculty of Engineering, University of Singapore.
M. R. Head
Affiliation:
Cambridge University Engineering Department Present address: Indian Institute of Technology, Kanpur.

Abstract

Calculations are presented of the development of the turbulent boundary layer on a rotating cylinder with its axis along the stream, and the results are compared with measurements made by Parr. With the choice of a suitable co-ordinate system, the boundary layer downstream of the nose of the cylinder approximates closely to a condition of two-dimensionality, and a simple integral method of solution can be applied. The only evidence of three-dimensionality lies in the destabilizing effect of rotation on the turbulence structure of the layer and an analysis of this instability has been made which relates changes in mixing length and entrainment to an instability parameter in the form of a Richardson number.

In spite of the changes in shear stress distribution and entrainment brought about by rotation, mean velocity profiles and skin friction values are found to be related to H and Rθ in the same way as for the stationary flat plate.

Type
Research Article
Copyright
© 1970 Cambridge University Press

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References

Bradshaw, P. 1969 The analogy between streamline curvature and buoyancy in turbulent shear flow. J. Fluid Mech. 36, 177.Google Scholar
Fiedler, H. E. & Head, M. R. 1966 Intermittency measurements in the turbulent boundary layer. J. Fluid Mech. 25, 719.Google Scholar
Furuya, Y., Nakamura, I. & Kawachi, H. 1966 The experiment on the skewed boundary layer on a rotating body. Japan Soc. Mech. Engng Bull. 9, 36, 702.Google Scholar
Head, M. R. 1958 Entrainment in the turbulent boundary layer. Aero. Res. Counc. R & M 3152.Google Scholar
Horlock, J. H., Norbury, J. F. & Cooke, J. C. 1967 Three-dimensional boundary layers: a report on Euromech 2. J. Fluid Mech. 27, 369.Google Scholar
Howarth, L. 1951 The boundary layer in three-dimensional flow. Part I. Derivation of the equations for flow along a general curved surface. Phil. Mag. (7), 42, 239.Google Scholar
Parr, O. 1962 Untersuchungen der dreidimensionalen Grenzschicht an rotierenden Drehkörpern bei axialer Anströmung. Ph.D. Thesis, Institute of Fluid Mechanics, Braunschweig Technical University. See also 1963 Ing. Arch. 32, 39.
Sawyer, R. A. 1963 Two-dimensional reattaching jet flows including the effects of curvature on entrainment. J. Fluid Mech. 17, 481.Google Scholar
Thompson, B. G. J. 1965 A new two-parameter family of mean velocity profiles for incompressible turbulent boundary layers on smooth walls. Aero. Res. Counc. R & M 3463.Google Scholar