Hostname: page-component-8448b6f56d-qsmjn Total loading time: 0 Render date: 2024-04-19T00:10:19.301Z Has data issue: false hasContentIssue false

A disturbance-sensitive Reynolds number range of the flow past a circular cylinder

Published online by Cambridge University Press:  28 March 2006

J. H. Gerrard
Affiliation:
Mechanics of Fluids Department, Manchester University

Abstract

The change by an order of magnitude of the oscillating properties of the flow past a circular cylinder in the Reynolds number range 2*103 to 5*104 is demonstrated experimentally. It is shown that in this range these properties are highly susceptible to small disturbances of the frequency of the transition waves which precede turbulence in the shear layers just downstream of the cylinder. It is suggested that this susceptibility is responsible for the different lift coefficient values measured by various workers.

The effect of disturbances on the mean flow properties is also described.

The frequency-determining mechanism and the characteristic length of the oscillating flow are discussed.

Type
Research Article
Copyright
© 1965 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

Bishop, R. E. D. & Hassan, A. Y. 1963 The lift and drag forces on a circular cylinder in a flowing fluid. Proc. Roy. Soc. A, 277, 32.Google Scholar
Bloor, M. S. 1964 The transition to turbulence in the wake of a circular cylinder. J. Fluid Mech. 19, 290.Google Scholar
Collis, D. C. 1952 The dust problem in hot-wire anemometry. Aero. Quart. 4, 93.Google Scholar
Gerrard, J. H. 1961 An experimental investigation of the oscillating lift and drag of a circular cylinder shedding turbulent vortices. J. Fluid Mech. 11, 244.Google Scholar
Keefe, R. T. 1961 An investigation of the fluctuating forces acting on a stationary circular cylinder in a subsonic stream and of the associated sound field. Univ. Toronto Inst. Aerophys. Rep. no. 76.
Roshko, A. 1954 On the drag and shedding frequency of two-dimensional bluff bodies. N.A.C.A. Tech. Note, no. 3169.Google Scholar
Sato, H. 1956 Experimental investigation on the transition of laminar separated layer. J. Phys. Soc. Japan, 11, 702.Google Scholar
Schiller, L. & Linke, W. 1933 Z. Flugtech. Motorluft, 24, 193.
Somerville, M. J. & Turnbull, G. F. 1963 Self-generating high frequency carrier feed-back anemometer. Proc. I.E.E. 110, 1905.Google Scholar