Detached-Eddy Simulation of Flow Around the NREL Phase VI Blade

被引:0
|
作者
Johansen, J. [1 ]
Sørensen, N.N. [1 ]
Michelsen, J.A. [2 ]
Schreck, S. [3 ]
机构
[1] Risø National Laboratory, Wind Energy Department, PO Box 49, Roskilde,DK-4000, Denmark
[2] Department of Mechanical Engineering, Technical University of Denmark, Lyngby,DK-2800, Denmark
[3] National Renewable Energy Laboratory, 1617 Cole Boulevard, Golden,CO,80401, United States
关键词
Aerodynamic stalling - Angle of attack - Atmospheric thermodynamics - Boundary layers - Flow separation - Large eddy simulation - Shear flow - Turbine components - Turbomachine blades - Turbulence models - Turbulent flow - Wind turbine blades;
D O I
10.1002/we.63
中图分类号
学科分类号
摘要
The detached-eddy simulation model implemented in the computational fluid dynamics code EllipSys3D is used to calculate the flow around the non-rotating NREL Phase VI wind turbine blade. Results are presented for flow around a parked blade at fixed angle of attack and a blade pitching along the blade axis. Computed blade characteristics are compared with experimental data from the NREL/NASA Ames Phase VI unsteady experiment. The detached-eddy simulation model is a method for predicting turbulence in computational fluid dynamics computations, which combines a Reynolds-averaged Navier –Stokes method in the boundary layer with a large-eddy simulation in the free shear flow. The present study focuses on static and dynamic stall regions highly relevant for stall-regulated wind turbines. Computations do predict force coefficients and pressure distributions fairly well. Results using detached-eddy simulation show considerably more three-dimensional flow structures compared to conventional two-equation Reynolds-averaged Navier –Stokes turbulence models, but no particular improvements are seen in the global blade characteristics. © 2002 John Wiley & Sons, Ltd.
引用
收藏
页码:185 / 197
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