首页> 外文期刊>AIAA Journal >Numerical Investigation of the Performance of Pitching Airfoils at High Amplitudes
【24h】

Numerical Investigation of the Performance of Pitching Airfoils at High Amplitudes

机译:高振幅俯仰翼型性能的数值研究

获取原文
获取原文并翻译 | 示例
           

摘要

Recently, a renewed interest toward vertical-axis wind turbines has developed, due to the increasing need of a rational utilization of renewable energy resources. In vertical-axis wind turbines, each blade undergoes a wide variation of angle of attack during one rotation, with important dynamic stall phenomena. Neglecting wake-to-wake interactions and curvature effects, a pitching airfoil is a good representation of the flow experienced by the blades of a vertical-axis wind turbine. In the present work, the flow around an Eppler 387 airfoil in pure pitching is investigated, exploring a parametric space tailored to vertical-axis wind-turbine applications. In such a case, the angle of attack a varies in the range-40 deg < alpha < 40 deg, resulting in large-amplitude pitching oscillations. The Reynolds number, based on the freestream velocity and the chord length, is set to Re-c = 3 x 10(4). In this sense, the present work differs from earlier studies, where typically the combined heaving and pitching or pure pitching for propulsion purposes have been considered, which are characterized by higher frequencies and smaller amplitudes and mainly positive angles of attack. In this paper, a detailed analysis of the force coefficients and how their evolution is affected by the dynamics of the flow structures generated during pitch-up and pitch-down of the airfoil is presented. Furthermore, it is shown that a modified Strouhal number, which takes into account both frequency and amplitude, is an appropriate metric for the performance of an airfoil in these conditions.
机译:近来,由于对合理利用可再生能源的需求不断增加,人们对垂直轴风力涡轮机产生了新的兴趣。在垂直轴风力涡轮机中,每个叶片在旋转一圈时都会受到很大的迎角变化,并带有重要的动态失速现象。俯仰翼型忽略了尾对尾的相互作用和曲率效应,很好地表示了垂直轴风力涡轮机叶片所经历的流动。在当前的工作中,研究了纯俯仰时Eppler 387机翼周围的流动,探索了适合垂直轴风力涡轮机应用的参数空间。在这种情况下,迎角α在-40度<α<40度的范围内变化,导致大振幅的俯仰振荡。根据自由流速度和弦长,雷诺数设置为Re-c = 3 x 10(4)。从这个意义上讲,当前的工作与早期的研究不同,在早期的研究中,通常考虑了组合的起伏和俯仰或用于推进目的的纯俯仰,其特征在于频率更高,振幅更小且攻角主要为正。在本文中,详细分析了力系数及其在机翼俯仰和俯仰期间所产生的流动结构的动力学如何影响其演变。此外,还表明,考虑到频率和幅度的修正斯特劳哈尔数是在这些条件下机翼性能的合适度量。

著录项

  • 来源
    《AIAA Journal》 |2016年第8期|2221-2232|共12页
  • 作者单位

    George Washington Univ, Dept Mech & Aerosp Engn, 800 22nd St,NW, Washington, DC 20052 USA;

    George Washington Univ, Dept Mech & Aerosp Engn, 800 22nd St,NW, Washington, DC 20052 USA;

    George Washington Univ, Dept Mech & Aerosp Engn, 800 22nd St,NW, Washington, DC 20052 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

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号