Hostname: page-component-848d4c4894-x24gv Total loading time: 0 Render date: 2024-04-30T15:52:16.040Z Has data issue: false hasContentIssue false

The vortex-street structure of ‘turbulent’ jets. Part 1

Published online by Cambridge University Press:  29 March 2006

J. C. Lau
Affiliation:
University of Singapore
M. J. Fisher
Affiliation:
Institute of Sound and Vibration Research, University of Southampton, England

Abstract

It was suggested by Lau, Fisher & Puchs (1972) that the basic structure of a ‘turbulent’ round jet might consist, essentially, of an axial array of fairly evenly spaced vortices moving downstream in the mixing region of the jet. The present experimental study is an attempt to establish this hypothesis on a sound footing. The problem which was posed was first to find proof of the existence of a fairly regular pattern in the mixing region, and second to extract detailed information on the component parts of this pattern to identify the nature of the structure.

Hot-wire signals in the mixing layer are known to possess a predominance of spikes. In the region closer to the high velocity side of the layer, these spikes tend to be downward ones whilst in the opposite region, they are upward. These spikes have been attributed to the entrainment mechanism in the mixing layer and had been thought to be random. A closer study of time-history curves of these hotwire signals suggests that they might not be as random as would appear at first glance. A probability analysis was conducted of the time intervals between the successive downward spikes in the u′ signals, and it was found that indeed the highest probability occurred when the time interval corresponded to a frequency equal to the vortex passing frequency.

A time-domain averaging (or eduction) technique was used to try to identify the nature of the flow structure using the spikes to trigger the eduction process. On the basis of these results it would seem that the suggestion of a vortex street is well founded. Furthermore, it appears that, as the individual vortices in the street move downstream, they are continuously transporting fluid masses across the mixing layer, and it is this effect which is producing the Reynolds stresses in the mixing layer, and causing the spikes in the u’ signals in this region.

Type
Research Article
Copyright
© 1975 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

Anderson, A. B. C. 1956 J. Acoust. Soc. Am. 28, 914.
Bradshaw, P., Ferriss, D. H. & Johnson, R. E. 1964 J. Fluid Mech. 19, 591.
Davies, P. O. A. L., Fisher, M. J. & Barratt, M. J. 1963 J. Fluid Mech. 15, 337.
Davies, P. O. A. L., Ko, N. W. M. & Bose, B. 1968 Aero. Res. Counc. Current Paper, no. 989.
Franklin, R. E. & Foxwell, J. H. 1960 Aero. Res. Counc. R. & M. nos. 3161, 3162.
Fuchs, H. V. 1970 Dsch. Luft- & Raumfahrt Rep. DLR-FB 7022.
Ko, N. M. W. & Davies, P. O. A. L. 1971 J. Fluid Mech. 50, 49.
Lau, J. C. 1971 Ph.D. thesis, I.S.V.R., University of Southampton.
Lau, J. C., Fisher, M. J. & Fuchs, H. V. 1972 J. Sound & Vib. 22, 379.