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首页> 外文期刊>Energy >Flow control on the NREL S809 wind turbine airfoil using vortex generators
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Flow control on the NREL S809 wind turbine airfoil using vortex generators

机译：使用涡流发生器对NREL S809风力涡轮机翼型进行流量控制

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摘要

Vortex generators are widely used passive flow-control devices to improve the aerodynamic perfor-mance of large wind turbines. In this paper, the aerodynamic performance of the airfoil S809 without and with vortex generators was investigated using a computational fluid dynamic method of simulation. In this paper, the vortex generators in order to control the flow within the boundary layer of the S809 airfoil with the momentum transferring and the vortex trajectory was discussed. The results were obtained with three-dimensional incompressible Reynolds-averaged Navier-Stokes equations, and the turbulence was simulated with the shear stress transport k-omega turbulence model. It is shown that the vortex gen-erators can effectively improve the aerodynamic performance of the airfoil S809 and decrease the thickness of the boundary layer. The stall phenomenon is delayed. Double vortex generator arrangements show better performance in the control of flow separation and further improve the aerodynamic per-formance of the airfoil S809. According to the results of the vortex generators, the vortex generators can effectively enhance the lift coefficient of the airfoil and control the flow separation. It can provide some instructional meaning to the application of vortex generators on the wind turbine blade, which benefits to the utilization of wind power. (C) 2016 Elsevier Ltd. All rights reserved.
机译：涡流发生器是广泛使用的无源流量控制设备，可提高大型风力涡轮机的空气动力性能。在本文中，使用计算流体动力学模拟方法研究了不带涡流发生器和带涡流发生器的机翼S809的空气动力学性能。本文讨论了涡旋发生器，以控制动量传递和涡旋轨迹，从而控制S809机翼边界层内的流动。用三维不可压缩的雷诺平均Navier-Stokes方程获得了结果，并用剪切应力传递k-omega湍流模型模拟了湍流。结果表明，涡流发生器可以有效提高机翼S809的空气动力性能，减小边界层的厚度。失速现象被延迟。双涡流发生器装置在控制气流分离方面表现出更好的性能，并进一步提高了S809翼型的空气动力学性能。根据涡流发生器的结果，涡流发生器可以有效地提高翼型的升力系数并控制流分离。它可以为涡流发生器在风力发电机叶片上的应用提供一定的指导意义，有利于风力的利用。 （C）2016 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Energy》 |2017年第1期|1210-1221|共12页
  • 作者

    Wang Haipeng; Zhang Bo; Qiu Qinggang; Xu Xiang;

  • 作者单位

    Dalian Univ Technol, Sch Energy & Power Engn, Dalian 116024, Liaoning, Peoples R China;

    Dalian Univ Technol, Sch Energy & Power Engn, Dalian 116024, Liaoning, Peoples R China;

    Dalian Univ Technol, Sch Energy & Power Engn, Dalian 116024, Liaoning, Peoples R China;

    Dalian Univ Technol, Sch Energy & Power Engn, Dalian 116024, Liaoning, Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Vortex generator; Boundary layer; Flow control;

    机译：涡旋发生器边界层流量控制;

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