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The timing of vortex shedding in a cylinder wake imposed by periodic inflow perturbations

Published online by Cambridge University Press:  07 November 2005

E. KONSTANTINIDIS
Affiliation:
Experimental and Computational Laboratory for the Analysis of Turbulence, Department of Mechanical Engineering, King's College London, Strand, London WC2R 2LS, UK Present address: Department of Engineering and Management of Energy Resources, University of Western Macedonia, Kozani 50100, Greece
S. BALABANI
Affiliation:
Experimental and Computational Laboratory for the Analysis of Turbulence, Department of Mechanical Engineering, King's College London, Strand, London WC2R 2LS, UK
M. YIANNESKIS
Affiliation:
Experimental and Computational Laboratory for the Analysis of Turbulence, Department of Mechanical Engineering, King's College London, Strand, London WC2R 2LS, UK

Abstract

The interaction of vortex shedding from a circular cylinder with an inflow which has low-amplitude periodic velocity oscillations (perturbations) superimposed upon it, was investigated experimentally by means of particle image velocimetry. The experiments were made at three perturbation frequencies across the lock-on range in which the vortex shedding frequency is synchronized with the subharmonic of the imposed frequency. The basic wake pattern in this range is antisymmetric vortex shedding, i.e. the familiar 2S mode. The timing of vortex shedding is defined with respect to the cross-flow oscillation of the wake which is found to play a critical role. Quantitative analysis of the phase-referenced patterns of vorticity distribution in the wake shows that a vortex is actually shed from the cylinder when the cross-flow oscillation of the wake is strongest, marked by a sudden drop in the computed vortex strength. At the middle of the lock-on range, shedding occurs near the minimum inflow velocity in the cycle or, equivalently, during the forward stroke of a cylinder oscillating in-line with the flow. It is argued that the imposed timing of vortex shedding relative to the cylinder motion induces a negative excitation from the fluid, which might explain why the in-line response of a freely vibrating cylinder exhibits two positive excitation regions separated by the lock-on region found in forced oscillations.

Type
Papers
Copyright
© 2005 Cambridge University Press

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