首页> 外文学位 >Experimental investigation of the active flow control on a two-dimensional wind turbine airfoil.
【24h】

Experimental investigation of the active flow control on a two-dimensional wind turbine airfoil.

机译:二维风轮机翼型主动流控制的实验研究。

获取原文
获取原文并翻译 | 示例

摘要

Wind turbine blades experience unsteady aerodynamic loading under various off-design conditions. The fatigue loading reduces the operational time of the wind turbine hence leads to an increase in the Cost of Energy (CoE) of the wind power. In this study, active flow control with unsteady blowing actuators was applied to a two-dimensional wind turbine airfoil to alleviate the unsteady aerodynamic loading and improve the aerodynamic performance, particularly under large scale freestream disturbances. A low speed, open jet aeroacoustic wind tunnel was designed and constructed based on an existing anechoic chamber for this investigation. A theoretical analysis based on a Blade Element Momentum (BEM) algorithm was performed to evaluate the effect of flow control on the power output of the wind turbines. The result from the assessment indicates a 60% increase in operational range could be achieved with flow control. In addition, experimental investigations were carried out utilizing surface dynamic pressure sensors, a force balance and Particle Image Velocimetry (PIV) flow field measurement techniques. The results show that the fluctuating loading generated by an upstream cylinder wake was reduced by up to 12% using a proportional closed loop control algorithm at 27 degree angle of incidence. Under the same unsteady freestream conditions, the averaged lift coefficient at 19 degree angle of incidence was enhanced by up to 20% while the pressure drag coefficient was reduced by up to 10%.
机译:在各种非设计条件下,风力涡轮机叶片会承受不稳定的空气动力负荷。疲劳载荷减少了风力涡轮机的运行时间,因此导致风力发电的能源成本(CoE)增加。在这项研究中,将带有非稳定吹气执行器的主动流控制应用于二维风力涡轮机翼型,以减轻非稳定的空气动力负荷并改善空气动力性能,特别是在大规模自由流扰动下。在此研究的基础上,基于现有消声室设计并建造了低速,开放式喷气声波风洞。进行了基于叶片单元动量(BEM)算法的理论分析,以评估流量控制对风力发电机功率输出的影响。评估结果表明,使用流量控制可以将操作范围增加60%。此外,利用表面动压力传感器,力平衡和粒子图像测速(PIV)流场测量技术进行了实验研究。结果表明,使用成比例的闭环控制算法在入射角为27度时,上游汽缸尾流产生的波动载荷降低了12%。在相同的非恒定自由流条件下,入射角为19度时的平均升力系数提高了20%,而压力阻力系数降低了10%。

著录项

  • 作者

    Wang, Guannan.;

  • 作者单位

    Syracuse University.;

  • 授予单位 Syracuse University.;
  • 学科 Engineering Aerospace.;Engineering Mechanical.;Energy.
  • 学位 Ph.D.
  • 年度 2013
  • 页码 194 p.
  • 总页数 194
  • 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