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Three-dimensional Improved Delayed Detached Eddy Simulation of a two-bladed vertical axis wind turbine

机译:两叶片垂直轴风力发电机的三维改进延迟分离涡模拟

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摘要

The aerodynamic performance of a two-bladed vertical axis wind turbine is investigated using the turbulence model of the Improved Delayed Detached Eddy Simulation and the polyhedral mesh. The sliding mesh technique is used to simulate the rotation of the rotor, Meanwhile, the results obtained by the shear stress transport k-omega model are presented as contrast. Then, the simulated power coefficients at different tip speed ratios and the wake velocity are validated by comparison with the experimental data from available literature. It is shown that the power coefficients and wake velocity predicted by the Improved Delayed Detached Eddy Simulation are closer to the experimental data than those by the shear stress transport k-omega model. The pressure distributions predicted by the two turbulence models show different degrees of discrepancies in different scales of flow separation. By comparing the vorticity magnitude graphs, the Improved Delayed Detached Eddy Simulation is found to be able to capture more exquisite vortices after the flow separations. Limited by its inherent ability, the shear stress transport k-omega model predicts vortices that are less realistic than those of Improved Delayed Detached Eddy Simulation. Hence, it may cause some errors in predicting the pressure distributions, especially when the blades suffer dynamic stall. It is demonstrated that the Improved Delayed Detached Eddy Simulation is regarded as a reliable model to analyze the aerodynamic performance of vertical axis wine turbines. (C) 2016 Elsevier Ltd. All rights reserved.
机译:使用改进的延迟分离涡模拟和多面体网格的湍流模型研究了两叶片垂直轴风力涡轮机的空气动力学性能。滑动网格技术被用来模拟转子的旋转,同时,剪切应力传递k-ω模型得到的结果作为对比。然后,通过与现有文献中的实验数据进行比较,验证了在不同的叶尖速度比和尾流速度下的模拟功率系数。结果表明,改进的延迟分离涡流模拟所预测的功率系数和尾流速度比剪切应力传输k-ω模型所预测的功率系数和尾流速度更接近实验数据。由两个湍流模型预测的压力分布在不同的分流规模中显示出不同程度的差异。通过比较涡度大小图,发现改进的延迟分离涡流模拟能够在流分离后捕获更多精致的涡流。受其固有能力的限制,剪切应力传输k-ω模型预测的涡旋不如改进的延迟分离涡流模拟的涡旋现实。因此,这可能在预测压力分布时引起一些误差,尤其是当叶片遭受动态失速时。结果表明,改进的延迟分离涡模拟被认为是分析垂直轴葡萄酒涡轮机气动性能的可靠模型。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Energy Conversion & Management》 |2017年第2期|235-248|共14页
  • 作者单位

    Shanghai Jiao Tong Univ, Sch Naval Architecture Ocean & Civil Engn, Shanghai, Peoples R China;

    Shanghai Jiao Tong Univ, Sch Naval Architecture Ocean & Civil Engn, Shanghai, Peoples R China|Collaborat Innovat Ctr Adv Ship & Deep Sea Explor, Shanghai, Peoples R China|Shanghai Jiao Tong Univ, State Key Lab Ocean Engn, Shanghai, Peoples R China;

    Shanghai Jiao Tong Univ, Sch Naval Architecture Ocean & Civil Engn, Shanghai, Peoples R China;

    Shanghai Jiao Tong Univ, Sch Naval Architecture Ocean & Civil Engn, Shanghai, Peoples R China;

    Shanghai Jiao Tong Univ, Sch Naval Architecture Ocean & Civil Engn, Shanghai, Peoples R China|Univ Houston, Cullen Coll Engn, Houston, TX USA;

  • 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

    Computational fluid dynamics; H-VAWTs; Polyhedral mesh; 3D IDDES; Aerodynamics;

    机译:计算流体力学;H-VAWT;多面体网格;3D IDDES;空气动力学;

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