This study investigates the aerodynamic behavior of the flow around
a rotating and stationary 60% scale isolated wheel, with and without
the use of a moving ground plane. The aim of this research was to
improve the understanding of the fundamental aerodynamic flow
features around a wheel and to examine how rotation and moving
ground planes modify these and affect the production of drag. A
bespoke rotating wheel rig was designed and wind tunnel tests were
performed over a range of pre to post critical Reynolds numbers.
Force coefficients were obtained using balance measurements and
flow field data were obtained using Particle Image Velocimetry
(PIV). The unsteady flow field data generated was used to validate
unsteady CFD predictions. These were performed using STARCCM+ and a k- SST Improved Delayed Detached Eddy Simulation
(IDDES) turbulence model. This was seen to outperform other
models by capturing an increased amount of finer detailed, high
frequency vortical structures. The CFD showed good agreement with
the experimental results providing, for the first time, a validated
numerical methodology. Comparing stationary and rotating wheels
the CFD and experimental data both illustrated large scale structural
differences in the surrounding flow due to changes in separation and
wake structure. The rotating model also exhibited a lower drag at post
critical Reynolds numbers, which is corroborated by existing
literature. Importantly, the CFD showed minimal difference between
a stationary and moving ground plane simulation with a rotating
wheel. This is evidence that, provided the wheel is rotating, valid
experiments can be performed without the complexity of a moving
ground plane
History
School
Aeronautical, Automotive, Chemical and Materials Engineering
Department
Aeronautical and Automotive Engineering
Published in
WCX SAE World Congress Experience
SAE Technical Paper Series
Citation
RAJARATNAM, E. and WALKER, A.D., 2019. Experimental and computational study of the flow around a stationary and rotating isolated wheel and the influence of a moving ground plane. SAE Technical Paper 2019-01-0647, 2019, doi:10.4271/2019-01-0647
This paper was accepted for publication in the journal SAE Technical Paper and the definitive published version is available at https://doi.org/10.4271/2019-01-0647
Publication date
2019-04-02
Notes
This paper was presented at the WCX SAE World Congress Experience, Detroit, April 9-11th.