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On stationary and travelling vortex breakdowns

Published online by Cambridge University Press:  29 March 2006

Turgut Sarpkaya
Affiliation:
Department of Mechanical Engineering, Naval Postgraduate School, Monterey, California

Abstract

This paper describes some experiments in swirling flows in a diverging cylindrical tube in which various types of vortex breakdowns were observed.

In one set of experiments, the position of the breakdown, axial component of the velocity of the vortex core, swirl angle distribution ahead of the breakdown, and the pressure distribution along the tube were determined for various flow rates and for various values of circulation imparted to the fluid (water). Basically, three types of vortex breakdown were observed, viz. mild (double helix) breakdown, spiral breakdown (followed by turbulent mixing), and axisymmetric breakdown (followed by a thicker vortex core, then a spiral breakdown, and finally by turbulent mixing). The type and the location of the stationary breakdowns were found to be dependent, for the particular vortex tube used, upon the Reynolds and circulation numbers of the flow. In a spiral breakdown, the vortex core filament maintained the same sense of rotation as the upstream fluid elements. In an axisymmetric breakdown, the bubble included an inclined vortex-ring whose axis gyrated about the axis of the tube.

In a second set of experiments, the response of the abrupt structural change along the axis of flow to gradual and abrupt changes in the upstream and downstream flow conditions was examined. The axisymmetric breakdown responded in a manner analogous to the hydraulic jump in open-channel flow before if reached a new stationary position along the axis of the tube.

The observations reported and the evidence presented herein revealed that the axisymmetric breakdown is a finite transition between two sequent states of flow as proposed by Benjamin (1962, 1965, 1967) on theoretical grounds.

Type
Research Article
Copyright
© 1971 Cambridge University Press

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References

Benjamin, T. B. 1962 Theory of the vortex breakdown phenomenon J. Fluid Mech. 14, 593.Google Scholar
Benjamin, T. B. 1965 Significance of the vortex breakdown phenomenon. Trans. Am. Soc. Mech. Engrs, J. Basic Engng 87, 518 and 518.Google Scholar
Benjamin, T. B. 1967 Some developments in the theory of vortex breakdown J. Fluid Mech. 28, 65.Google Scholar
Granger, R. A. 1968 Speed of a surge in a bathtub vortex J. Fluid Mech. 34, 651.Google Scholar
Hall, M. G. 1966a The structure of concentrated vortex cores. In Progress in Aeronautical Sciences, 7 (ed. D. Küchemann et al.). Pergamon.
Hall, M. G. 1966b On the occurrence and identification of vortex breakdown. R.A.E. Tech. Report no. 66283.Google Scholar
Harvey, J. K. 1962 Some observations of the vortex breakdown phenomenon J. Fluid Mech. 14, 585.Google Scholar
Jones, J. P. 1960 The breakdown of vortices in separated flow. University of Southampton U.S.A.A. Report no. 140.Google Scholar
Jones, J. P. 1964 On the explanation of vortex breakdown. IUTAM Symposium on Vortex Motions. Ann Arbor.
Kirkpatrick, D. L. I. 1964 Experimental investigation of the breakdown of a vortex in a tube. R.A.E. Tech. Note no. Aero 2963.Google Scholar
Lambourne, N. C. 1965 The breakdown of certain types of vortex. N.P.L. Aero Report 1166.
Lambourne, N. C. & Bryer, D. W. 1962 The bursting of leading edge vortices-some observations and discussion of the phenomenon. Aero. Res. Counc. R & M 3282.
Ludwieg, H. 1962 Zur Erklärung der Instabilität der über angestellten Deltaflügeln aufteten freien Wirkbelkerne Z. Flugwiss. 10, 242.Google Scholar
Ludweig, H. 1964 Explanation of vortex breakdown by the stability theory for spiralling flows. IUTAM Symposium on Vortex Motions, Ann Arbor. Available as AVA-Bericht 64 A 14.
Lowson, M. V. 1964 Some experiments with vortex breakdown J. Roy. Aero. Soc. 68, 343.Google Scholar
Pritchard, W. G. 1970 Solitary waves in rotating fluids J. Fluid Mech. 42, 61.Google Scholar