Abstract
Unsteady turbulent flow characteristics over a two-blade horizontal wind turbine rotor is analyzed using a large-eddy simulation technique. The wind turbine rotor corresponds to the configuration of the U.S. National Renewable Energy Laboratory (NREL) phase VI campaign. The filtered incompressible Navier-Stokes equations in a non-inertial reference frame fixed at the centroid of the rotor, are solved with centrifugal and Coriolis forces using an unstructured-grid finite-volume method. A systematic analysis of effects of grid resolution, computational domain size, and time-step size on simulation results, is carried out. Simulation results such as the surface pressure coefficient, thrust coefficient, torque coefficient, and normal and tangential force coefficients are found to agree favorably with experimental data. The simulation showed that pressure fluctuations, which produce broadband flow-induced noise and vibration of the blades, are especially significant in the mid-chord area of the suction side at around 70 to 95 percent spanwise locations. Large-scale vortices are found to be generated at the blade tip and the location connecting the blade with an airfoil cross section and the circular hub rod. These vortices propagate downstream with helical motions and are found to persist far downstream from the rotor.
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Recommended by Associate Editor Jungil Lee
Taeyoung Kim received his M.S. in Mechanical Engineering from Carnegie Mellon University in 2011. He is now a doctoral candidate in the School of Mechanical Engineering at Georgia Institute of Technology.
Donghyun You received his Ph.D. in Mechanical Engineering from Stanford University in 2004. He is currently an Associate Professor in the Department of Mechanical Engineering at Pohang University of Science and Technology (POSTECH).
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Kim, T., You, D. Large-eddy simulation analysis of turbulent flow over a two-blade horizontal wind turbine rotor. J Mech Sci Technol 30, 4989–4996 (2016). https://doi.org/10.1007/s12206-016-1018-4
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DOI: https://doi.org/10.1007/s12206-016-1018-4