Large eddy simulations of the flow past wind turbines: actuator line and disk modeling
Article first published online: 10 APR 2014
Copyright © 2014 John Wiley & Sons, Ltd.
How to Cite
Martínez-Tossas, L. A., Churchfield, M. J. and Leonardi, S. (2014), Large eddy simulations of the flow past wind turbines: actuator line and disk modeling. Wind Energ.. doi: 10.1002/we.1747
- Article first published online: 10 APR 2014
- Manuscript Accepted: 18 FEB 2014
- Manuscript Revised: 5 DEC 2013
- Manuscript Received: 8 APR 2013
- computational fluid dynamics;
- actuator line model;
- actuator disk model;
- large eddy simulations
Large eddy simulations of the flow through wind turbines have been carried out using actuator disk and actuator line models for the turbine rotor aerodynamics. In this study, we compare the performance of these two models in producing wind turbine wakes. We also examine parameters that strongly affect the performance of these models, namely, grid resolution and the way in which the actuator force is projected onto the flow field. The proper choice of these two parameters has not been adequately addressed in previous works. We see that as the grid is coarsened, the predicted power decreases. As the width of the body force projection function is increased, the predicted power increases. The actuator disk and actuator line models produce similar wake profiles and predict power within 1% of one another when subject to the same uniform inflow. The actuator line model is able to generate flow structures near the blades such as root and tip vortices which the actuator disk model does not, but in the far wake, the predicted mean wakes are very similar. In order to perform validation against experimental data, the actuator line model output was compared with data from the wind tunnel experiment conducted at the Norwegian University of Science and Technology, Trondheim. Agreement between measured and predicted power, wake profiles, and turbulent kinetic energy has been observed for most tip speed ratios; larger discrepancies in power and thrust coefficient, though, have been found for tip speed ratios of 9 and 12. Copyright © 2014 John Wiley & Sons, Ltd.