首页> 外文期刊>Energy >Steady wind performance of a 5 kW three-bladed H-rotor Darrieus Vertical Axis Wind Turbine (VAWT) with cambered tubercle leading edge (TLE) blades
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Steady wind performance of a 5 kW three-bladed H-rotor Darrieus Vertical Axis Wind Turbine (VAWT) with cambered tubercle leading edge (TLE) blades

机译:具有弧形结节前缘(TLE)叶片的5 kW三叶片H型转子Darrieus垂直轴风力涡轮机(VAWT)的稳定风能

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摘要

The performance of a 5 kW three-bladed H-rotor Darrieus Vertical Axis Wind Turbine with cambered Tubercle Leading Edge NACA 0025 blades was established using computational fluid dynamics. 3D models and simulations of the VAWT were realized using CAD and CAE software, after which post-processing analyses provided understanding of the VAWT and blade flow physics. Results showed the TLE to be detrimental to flow and performance of a cambered VAWT. Using torque, lift and drag data, the cambered TLE VAWT was shown to deviate significantly against the cambered VAWT over one complete converged rotation. Cambered TLE VAWT blades encounter reduced lift forces and increased drag forces leading to lowered and eventual reversal of torque values. The z-vorticity and Q-criterion visualizations further supported the numerical results with the post-processed images showing vortices the size of the blade chord generated at blade wakes of the cambered TLE. The vortices emanate from the flow separation at the blade crests creeping in at the blade trailing edge at 75 degrees azimuth and reaching halfway through the blade chord length at 106 degrees azimuth. Spanwise separation was observed to be restricted at blade crests. The resulting flow degradation translated to the poor performance of the wind turbine. (C) 2019 Elsevier Ltd. All rights reserved.
机译:使用计算流体力学来确定具有弧形块状前缘NACA 0025叶片的5 kW三叶片H型转子Darrieus垂直轴风力涡轮机的性能。使用CAD和CAE软件实现了VAWT的3D模型和仿真,之后的后处理分析提供了对VAWT和叶片流物理学的理解。结果表明,TLE不利于弧形VAWT的流量和性能。使用扭矩,升力和阻力数据,表明拱形TLE VAWT在一个完整的收敛旋转中相对于拱形VAWT明显偏离。弧形的TLE VAWT叶片遇到的升力减小,阻力增大,导致扭矩值降低并最终逆转。 z涡度和Q准则可视化进一步支持了数值结果,后处理的图像显示了涡旋,该涡旋在弧形TLE的叶片尾流产生时产生了叶片弦的大小。涡流是由叶片波峰处的流动分离产生的,该波峰在75度方位角处在叶片后缘处蠕动,并在106度方位角处到达叶片弦长的一半。观察到翼展方向的分离限制在叶片顶部。导致的流量下降导致风力涡轮机性能下降。 (C)2019 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Energy》 |2019年第15期|278-291|共14页
  • 作者单位

    Univ Philippines Diliman, Energy Engn Grad Program, Quezon City 1101, Philippines;

    Univ Philippines Diliman, Energy Engn Grad Program, Quezon City 1101, Philippines|Univ Philippines Diliman, Dept Mech Engn, Quezon City 1101, Philippines;

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

    TLE; Camber; VAWT; CFD;

    机译:标题;Camber;VAWT;CFD;
  • 入库时间 2022-08-18 04:13:47

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