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Validation of four LES and a vortex model against stereo-PIV measurements in the near wake of an actuator disc and a wind turbine

机译:在致动器盘和风力涡轮机接近尾声时针对立体声PIV测量验证四个LES和涡旋模型

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摘要

In this paper we report the results of a workshop organised by the Delft University of Technology in 2014, aiming at the comparison between different state-of-the-art numerical models for the simulation of wind turbine wakes. The chosen benchmark case is a wind tunnel measurement, where stereoscopic Particle Image Velocimetry was employed to obtain the velocity field and turbulence statistics in the near wake of a two-bladed wind turbine model and of a porous disc, which mimics the numerical actuator used in the simulations. Researchers have been invited to simulate the experimental case based on the disc drag coefficient and the inflow characteristics. Four large eddy simulation (LES) codes from different institutions and a vortex model are part of the comparison. The purpose of this benchmark is to validate the numerical predictions of the flow field statistics in the near wake of an actuator disc, a case that is highly relevant for full wind farm applications. The comparison has shown that, despite its extreme simplicity, the vortex model is capable of reproducing the wake expansion and the centreline velocity with very high accuracy. Also all tested LES models are able to predict the velocity deficit in the very near wake well, contrary to what was expected from previous literature. However, the resolved velocity fluctuations in the LES are below the experimentally measured values. (C) 2016 Elsevier Ltd. All rights reserved.
机译:在本文中,我们报告了代尔夫特理工大学在2014年组织的一次研讨会的结果,旨在比较不同的最新数值模型来模拟风力涡轮机尾流。选择的基准案例是风洞测量,其中采用立体粒子图像测速技术获得了两叶风力涡轮机模型和多孔圆盘的近场时的速度场和湍流统计数据,该模型模拟了用于模拟。已邀请研究人员根据圆盘阻力系数和流入特征来模拟实验情况。比较中包括来自不同机构的四个大型涡模拟(LES)代码和涡旋模型。该基准测试的目的是在致动器盘接近尾声时验证流场统计数据的数值预测,这种情况与全风电场应用密切相关。比较表明,尽管涡流模型极其简单,但它能够以非常高的精度再现尾波扩展和中心线速度。而且,所有测试的LES模型都能够预测非常接近的尾流井中的速度赤字,这与以前的文献所期望的相反。但是,LES中的解析速度波动低于实验测量值。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Renewable energy》 |2016年第8期|510-523|共14页
  • 作者单位

    Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;

    Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands|Energy Res Ctr Netherlands ECN, NL-1755 ZG Petten, Netherlands;

    Johns Hopkins Univ, Dept Mech Engn, Baltimore, MD 21218 USA|Johns Hopkins Univ, Ctr Environm & Appl Fluid Mech, Baltimore, MD 21218 USA|Univ Twente, Dept Phys, Mesa Inst, POB 217, NL-7500 AE Enschede, Netherlands|Univ Twente, JM Burgers Ctr Fluid Dynam, POB 217, NL-7500 AE Enschede, Netherlands;

    Katholieke Univ Leuven, Dept Mech Engn, Celestijnenlaan 300 A, B-3001 Leuven, Belgium;

    Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;

    Tech Univ Denmark, Dept Wind Energy, DK-2800 Lyngby, Denmark;

    Johns Hopkins Univ, Dept Mech Engn, Baltimore, MD 21218 USA|Johns Hopkins Univ, Ctr Environm & Appl Fluid Mech, Baltimore, MD 21218 USA;

    Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;

    Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;

    Katholieke Univ Leuven, Dept Mech Engn, Celestijnenlaan 300 A, B-3001 Leuven, Belgium;

    Delft Univ Technol, Dept Aerodynam Wind Energy Flight Performance & P, NL-2629 HS Delft, Netherlands;

    Energy Res Ctr Netherlands ECN, NL-1755 ZG Petten, Netherlands;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Horizontal axis wind turbine; Wind turbine wake; Large eddy simulation; Actuator disc; LES validation;

    机译:水平轴风力涡轮机;风力涡轮机尾流;大涡模拟;执行器盘;LES验证;
  • 入库时间 2022-08-18 00:25:30

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