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Experimental investigation on the wake interference among wind turbines sited in atmospheric boundary layer winds

机译:大气边界层风中风力涡轮机尾流干扰的实验研究

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摘要

We examined experimentally the effects of incom-ing surface wind on the turbine wake and the wake interfer-ence among upstream and downstream wind turbines sited in atmospheric boundary layer (ABL) winds. The experi-ment was conducted in a large-scale ABL wind tunnel with scaled wind turbine models mounted in different incom-ing surface winds simulating the ABL winds over typical offshore/onshore wind farms. Power outputs and dynamic loadings acting on the turbine models and the wake flow char-acteristics behind the turbine models were quantified. The results revealed that the incoming surface winds significantly affect the turbine wake characteristics and wake interference between the upstream and downstream turbines. The velocity deficits in the turbine wakes recover faster in the incoming surface winds with relatively high turbulence levels. Varia-tions of the power outputs and dynamic wind loadings acting on the downstream turbines sited in the wakes of upstream turbines are correlated well with the turbine wakes charac-teristics. At the same downstream locations, the downstream turbines have higher power outputs and experience greater static and fatigue loadings in the inflow with relatively high turbulence level, suggesting a smaller effect of wake inter-ference for the turbines sited in onshore wind farms.
机译:我们通过实验检查了传入的表面风对涡轮机尾流的影响以及位于大气边界层(ABL)风中的上游和下游风力涡轮机之间的尾流干扰。实验是在大型ABL风洞中进行的,比例风轮机模型安装在不同的传入地面风中,模拟典型海上/陆上风电场的ABL风。量化了作用在涡轮机模型上的功率输出和动态载荷以及涡轮机模型背后的尾流特性。结果表明,进入的表面风显着影响了涡轮机的尾流特性以及上游和下游涡轮机之间的尾流干扰。涡轮尾流中的速度赤字在湍流水平较高的情况下,在进入的表面风中恢复得更快。作用在上游涡轮机尾流中的下游涡轮机上的功率输出和动态风荷载的变化与涡轮机尾流特性密切相关。在相同的下游位置,下游涡轮机具有较高的功率输出,并且在入流中承受较大的静载荷和疲劳载荷,且湍流水平相对较高,这表明对位于陆上风电场的涡轮机而言,尾流干扰的影响较小。

著录项

  • 来源
    《力学学报:英文版》 |2017年第004期|742-753|共12页
  • 作者

    W. Tian; A. Ozbay; X. D. Wang; H.Hu;

  • 作者单位

    School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China;

    Department of Aerospace Engineering, Iowa State University, Ames, IA 50011, USA;

    Department of Aerospace Engineering, Iowa State University, Ames, IA 50011, USA;

    School of Energy, Power and Mechanical Engineering, North China Electric Power University, Beijing 102206, China;

    Department of Aerospace Engineering, Iowa State University, Ames, IA 50011, USA;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-19 03:49:46
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