Hostname: page-component-cd9895bd7-jn8rn Total loading time: 0 Render date: 2024-12-28T05:57:24.652Z Has data issue: false hasContentIssue false

On vortex shedding from a circular cylinder in the critical Reynolds number régime

Published online by Cambridge University Press:  29 March 2006

P. W. Bearman
Affiliation:
National Physical Laboratory, Teddington, Middlesex

Abstract

The flow around a circular cylinder has been examined over the Reynolds number range 105 to 7·5 × 105, Reynolds number being based on cylinder diameter. Narrow-band vortex shedding has been observed up to a Reynolds number of 5·5 × 105, i.e. well into the critical régime. At this Reynolds number the Strouhal number reached the unusually high value of 0·46. Spectra of the velocity fluctuations measured in the wake are presented for several values of Reynolds number.

Type
Research Article
Copyright
© 1969 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

Allen, H. J. & Vincenti, W. G. 1944 NACA Tech. Rep. no. 782.
Bearman, P. W. 1968 Nat. Phys. Lab. Aero. Rep. no. 1273.
Blackman, R. B. & Tukey, J. W. 1958 The Measurement of Power Spectra New York: Dover.
Delany, N. K. & Sorensen, N. E. 1953 NACA Tech. Note. no. 3038.
Humphreys, J. S. 1960 J. Fluid Mech. 9, 603.
Relf, E. F. & Simmons, L. F. G. 1924 Aero. Res. Counc. R. & M. no. 917.
Ribner, H. S. & Etkin, B. 1958 Proc. 1st Int. Congr. Aero. Sci. Madrid. London: Pergamon, 1959.
Roshko, A. 1961 J. Fluid Mech. 10, 345.
Tani, J. 1964 Progr. Aero. Sci. 5, 70.