期刊文献+

垂直轴风力机尾缘开裂襟翼气动性能及其偏转角调节规律 被引量:5

Aerodynamic performance on the trailing edge split flap and regulation law of deflection angle of VAWT
下载PDF
导出
摘要 为提高垂直轴风力机的气动性能,提出在小型3叶片垂直轴风力机叶片尾缘加装开裂襟翼的设计方案。首先,根据CFD数值模拟和正交设计得到偏转角对风力机气动性能影响最大;然后,进一步分析了叶尖速比分别为1.5和2.5时襟翼偏转角对风力机气动性能的影响和增升机理;最后,提出了襟翼偏转角调节规律。研究结果表明:襟翼的较优参数组合为长度l=20%c、偏转角β=10°和布置位置t=90%c。当叶尖速比TSR分别为1.5和2.5时,较小的襟翼偏转角(0°<β<10°)能提升叶片平均切向力系数CTavg,其中,襟翼偏转角β=10°时,风力机的风能利用率CP分别提升了7.7%和4.6%;与原型风力机相比,应用襟翼偏转角调节规律后,风能利用率CP分别提升12.4%和10.4%。 In order to improve the aerodynamic performance of vertical-axis wind turbine(VAWT),a design scheme for adding a split flap on the trailing edge of the small 3-blade VAWT was proposed.Firstly,by using CFD numerical simulation and orthogonal design method,it was found that the deflection angle had the greatest influence on the aerodynamic performance of wind turbine.Secondly,the influences of the flap deflection angle on the aerodynamic performance of the wind turbine and the increasing mechanism of lift were analyzed when the tip speed ratio was 1.5 and 2.5 respectively.Finally,the regulation law of the flap deflection angle was proposed.The results show that the optimal length(l)is 20%c,optimal deflection angle(β)is 10°and optimal arrangement position(t)is 90%c.When tip speed ratio(TSR)is 1.5 and 2.5 respectively,the smaller fixed deflection angle(0°<β<10°)can increase the average tangential force coefficient of the blade.The output power coefficient(CP)increases by 7.7%and 4.6%respectively when deflection angle is 10°.By using the regulation law of flap deflection angle,the output power coefficient increases by 12.4%and 10.4%respectively compared with that of the prototype wind turbine.
作者 张立军 顾嘉伟 朱怀宝 胡阔亮 江奕佳 缪俊杰 王旱祥 刘静 ZHANG Lijun;GU Jiawei;ZHU Huaibao;HU Kuoliang;JIANG Yijia;MIAO Junjie;WANG Hanxiang;LIU Jing(College of Mechanical and Electronic Engineering,China University of Petroleum,Qingdao 266580,China)
出处 《中南大学学报(自然科学版)》 EI CAS CSCD 北大核心 2020年第4期931-943,共13页 Journal of Central South University:Science and Technology
基金 国家自然科学基金资助项目(51707204) 中央高校基本科研业务专项资助项目(17CX05021)。
关键词 垂直轴风力机 开裂襟翼 正交设计 气动性能 调节规律 vertical-axis wind turbine(VAWT) split flap orthogonal design aerodynamic performance regulation law
  • 相关文献

参考文献12

二级参考文献56

  • 1刘志华,熊鹰,叶金铭,谭廷寿.基于多块混合网格的RANS方法预报螺旋桨敞水性能的研究[J].水动力学研究与进展(A辑),2007,22(4):450-456. 被引量:44
  • 2李俊峰,时璟丽,施鹏飞.风力12在中国[M].化学工业出版社,2005:1-2,105.87. 被引量:8
  • 3U.S.Department of energy,Sandia National Laboratories and American Wind Energy Associotion.The History of the DOE program.Vertical Axis Wind Turbine. 被引量:1
  • 4张显双.风能的利用[M].物理世界.人民教育出版社,2004. 被引量:2
  • 5倪受元.风力机的类型与种类[D].风力发电讲座,7-8. 被引量:1
  • 6Li Y C, Wang J J, Hua J. Experimental investigations on the effects of divergent trailing edge and Gurney flaps on a supercritical airfoil[J]. Aerospace Science and Technology, 2007, 11(2): 91-99. 被引量:1
  • 7Wang J J, Li Y C, Choi K S. Gurney flap-Lift enhancement, mechanisms and applications[J]. Progress in Aerospace Sciences, 2008, 44(1): 22-47. 被引量:1
  • 8Chandrasekhara M S. Optimum Gurney flap height determination for "lost-lift" recovery in compressible dynamic stall control[J]. Aerospace Science and Technology, 2010, 14(8): 551-556. 被引量:1
  • 9Troldborg N. Computational study of the Ris?-B1-18 airfoil with a hinged flap providing variable trailing edge geometry[J]. Wind Engineering, 2005, 29(2): 89-114. 被引量:1
  • 10Van Dam C P, Nakafuji D Y, Bauer C, et al. Computational design and analysis of a microtab based aerodynamic loads control system for lifting surfaces[C]// Micromachining and Microfabrication. International Society for Optics and Photonics, 2003: 28-39. 被引量:1

共引文献111

同被引文献42

引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部