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Laser Doppler anemometry measurements in the near-wake of an isolated Formula One wheel

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Abstract

An experimental investigation was conducted to identify the main structures in the near wake of an isolated Formula One wheel rotating in ground contact. A 50 percent-scale isolated wheel assembly, geometrically similar to the configuration mounted on a Formula One racing car, was tested in a closed-return three-quarter open-jet wind tunnel. The test Reynolds number, based on wheel diameter was 6.8 × 105. Using laser doppler anemometry, three velocity components were measured with a total of 1966 data points across four planes and within one diameter downstream of the wheel axis. Based on analysis of these data, the main characteristics of the near-wake of an isolated wheel rotating in ground contact are presented. A revised model of the trailing vortex system induced in the wake of such a wheel is proposed, which clarifies the contradictory ones published in the literature to date.

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Abbreviations

D :

wheel diameter

f :

focal length (of laser doppler anemometer probe)

t :

transit time (of seeding particle)

u :

velocity component in the x-direction

u :

freestream velocity

v :

velocity component in the y-direction

w :

velocity component in the z-direction

x :

streamwise Cartesian coordinate (see Fig. 3)

y :

crosswise Cartesian coordinate (see Fig. 3)

z :

vertical Cartesian coordinate (see Fig. 3)

τ i :

integral timescale

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Acknowledgments

Financial support from an Engineering and Physical Sciences Research Council CASE award and the loan of wind tunnel model components from Jaguar Racing is gratefully acknowledged.

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Correspondence to A. J. Saddington.

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Saddington, A.J., Knowles, R.D. & Knowles, K. Laser Doppler anemometry measurements in the near-wake of an isolated Formula One wheel. Exp Fluids 42, 671–681 (2007). https://doi.org/10.1007/s00348-007-0273-7

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  • DOI: https://doi.org/10.1007/s00348-007-0273-7

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