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A laminar boundary layer on a rotating three-dimensional blade

Published online by Cambridge University Press:  29 March 2006

Y. Miyake  and
S. Fujita
Y. Miyake
Affiliation:
Department of Mechanical Engineering, Osaka University, Osaka, Japan
S. Fujita
Affiliation:
Department of Mechanical Engineering, Osaka University, Osaka, Japan Present address: Mitsubishi Heavy Industry Co. Ltd, Kobe, Japan.
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Abstract

The laminar boundary layer on a rotating thin blade of an axial turbomachine is discussed. A method of deriving the basic equations of the flow for a generalized blade configuration is described, treating a typical blade in practical use as an example. A perturbation technique is applied to obtain a series solution composed of two groups of similar functions. The results give insight into the properties of the boundary layer on helical non-loaded blades in a uniform stream, indicating the influence purely of three-dimensionality of the blade configuration.

Information

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 65 , Issue 3 , 16 September 1974 , pp. 481 - 498
Copyright
© 1974 Cambridge University Press

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References

Bogdanova, V. V. 1971 Mekh. Zhid. i Gaza, no. 2, p. 84.
Fogarty, L. E. 1951 J. Aero. Sci. 18, 247.
Horlock, J. H. & Wordsworth, J. 1965 J. Fluid Mech. 23, 305.
McCrosky, W. J. & Yaggy, P. F. 1968 A.I.A.A.J. 6, 1919.
Takematsu, M. 1972 A.I.A.A.J. 10, 333.
Tan, H. S. 1953 J. Aero. Sci. 20, 780.
Toyokura, T. & Harada, K. 1969 J. Japan. Soc. Mech. Engrs, 72, 56 (in Japanese).