4.6 Article

Large eddy simulations of the flow past wind turbines: actuator line and disk modeling

Journal

WIND ENERGY
Volume 18, Issue 6, Pages 1047-1060

Publisher

WILEY
DOI: 10.1002/we.1747

Keywords

computational fluid dynamics; actuator line model; actuator disk model; large eddy simulations

Funding

  1. National Renewable Energy Laboratory [AFC-1-11305-01]
  2. NSF PIRE [1243482]
  3. Office Of The Director
  4. Office Of Internatl Science &Engineering [1243482] Funding Source: National Science Foundation

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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 (c) 2014 John Wiley & Sons, Ltd.

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