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Abstracts - KTH Mechanics

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Experiments on vortex pair dynamics in ground effect<br />

C. Cottin ∗ and T. Leweke ∗<br />

We investigate experimentally the 3D dynamics of a pair of counter-rotating vortices<br />

approaching a solid wall. In addition to its fundamental interest, this configuration<br />

has relevance for the problem of aircraft trailing vortices at take-off and landing.<br />

The vortices are generated in water at the edges of two impulsively rotated flat<br />

plates, and visualised using fluorescent dye. Measurements were performed using<br />

image analysis and Particle Image Velocimetry. The set-up and procedure are similar<br />

to the ones described in Ref. 1. Reynolds numbers, based on the circulation of one<br />

vortex, were in the range 1500-5500.<br />

In the major part of the experiments, the vortex pairs were generated close to<br />

3 vortex separation distances away from the wall. This is short enough for the flow<br />

not to develop long-wavelength displacement instabilities or elliptic core instabilities 1 ,<br />

before the wall effect becomes important. As the vortices approach the surface due<br />

to their mutually induced motion, secondary vorticity is generated at the wall (see<br />

figure 1), which is lifted off the surface and rolls up into a secondary vortex orbiting<br />

the primary one and causing its rebound. During this stage, short-wave perturbations<br />

grow at the periphery of the primary vortices (fig. 1a). At a later time, an instability<br />

with a larger axial wavelength develops on the secondary vortex (fig. 1b), leading to<br />

a rapid decay of the whole system into small-scale structures shortly afterwards. We<br />

will present evidence that these phenomena are caused by a centrifugal instability of<br />

the primary vortex and an elliptic instability of the secondary vortex, respectively.<br />

Some qualitative results on the interaction of a ground effect with the longwavelength<br />

Crow instability will also be presented.<br />

∗ IRPHE, CNRS/Universités Aix-Marseille, B.P. 146, F-13384 Marseille Cedex 13, France.<br />

1 Leweke and Williamson, J. Fluid Mech. 360, 85 (1998)<br />

(a)<br />

(b)<br />

Figure 1: Dye visualisation (side view) and vorticity levels (cross-cut of one vortex<br />

only) of a vortex pair in ground effect at Re = 3500. (a) t ∗ = 4.5, (b) t ∗ =6.4.<br />

199

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