Design of a boundary-layer suction system for turbulent trailing-edge noise reduction of wind turbines

被引:20
作者
Arnold, B. [1 ]
Lutz, Th. [1 ]
Kraemer, E. [1 ]
机构
[1] Univ Stuttgart, Inst Aerodynam & Gas Dynam, Pfaffenwaldring 21, D-70569 Stuttgart, Germany
关键词
Wind energy; Trailing-edge noise; Boundary-layer suction; VISCOUS COMPRESSIBLE FLOW; AIRFOILS; HOLE;
D O I
10.1016/j.renene.2018.02.050
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
The present work introduces a method for the design of a boundary-layer suction system for turbulent trailing-edge noise reduction of wind turbines. Since the latter hitherto has been primarily assessed in a two-dimensional framework, the paper is meant to point out whether the predicted improvements carry over to wind turbine flow. Since the processes of trailing-edge noise reduction and effective power alteration are intimately bound together, great emphasis is put on an accurate prediction of pump power requirement, the latter being based on a detailed suction hardware system implying pressure losses across each component. An exemplarily performed design reveals that, within a certain design regime, trailing-edge noise reduction is accompanied by an enhancement of rotor power. However, as of a distinct cross-over point at which the pump power requirement exactly compensates the amelioration of aerodynamic power, a trade-off between aeroacoustics and aerodynamics arises. The method bases on fully-resolved URANS computations and is applied to the generic NREL 5 MW turbine. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:249 / 262
页数:14
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