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湍流工况涡流发生器对风力机翼型气动特性影响的试验研究

杨俊伟 沙成龙 王相军 杨华

空气动力学学报2025,Vol.43Issue(5):31-40,10.
空气动力学学报2025,Vol.43Issue(5):31-40,10.DOI:10.7638/kqdlxxb-2024.0227

湍流工况涡流发生器对风力机翼型气动特性影响的试验研究

Experimental investigation of vortex generator influence on wind turbine airfoil aerodynamic performance under turbulent inflow conditions

杨俊伟 1沙成龙 2王相军 3杨华3

作者信息

  • 1. 扬州大学广陵学院,扬州 225000||扬州大学电气与能源动力工程学院,扬州 225127
  • 2. 江苏省盐城技师学院,盐城 224000
  • 3. 扬州大学电气与能源动力工程学院,扬州 225127
  • 折叠

摘要

Abstract

This study investigates the effects of vortex generators(VGs)on the aerodynamic performance of a wind turbine airfoil under turbulent inflow conditions.A wind tunnel test setup was established to examine the flow control effects of VGs on the DU93-W-210 airfoil at various turbulence intensities with a Reynolds number of 1.5×105.The pressure coefficients,lift and drag coefficients,and flow separation were measured for static and dynamic conditions.Results showed that when the inflow turbulence intensity increased from 0.50%to 10.18%,VGs effectively delayed flow separation on the airfoil surface,expanding the range of angles of attack for enhanced static aerodynamic performance from 11°-17° to 11°-20°.The maximum lift coefficient increase initially rose and then decreased with higher turbulence intensity(the relative increments under the three conditions were 5.45%,7.79%,and 6.91%).During deep stall,VGs failed to suppress separation,resulting in increased pressure drag coefficients.Dynamic tests revealed that increased turbulence intensity allowed VGs to enhance lift at wider angles of attack during the downstroke phase.The aerodynamic improvement during downstroke was significantly greater than during the upstroke phase.Flow visualization using tuft methods further validated these findings.This research provides practical guidance for optimizing wind turbine airfoil design in turbulent conditions.

关键词

湍流/风洞试验/风力机翼型/涡流发生器/气动特性

Key words

turbulent/wind tunnel test/wind turbine airfoil/vortex generators/aerodynamic characteristics

引用本文复制引用

杨俊伟,沙成龙,王相军,杨华..湍流工况涡流发生器对风力机翼型气动特性影响的试验研究[J].空气动力学学报,2025,43(5):31-40,10.

基金项目

中国博士后科学基金面上项目(2023M742958) (2023M742958)

2024年江苏高校"青蓝工程"资助课题 ()

江苏省高等学校基础科学(自然科学)研究面上项目(23KJD130004) (自然科学)

扬州市自然科学基金(YZ2023169) (YZ2023169)

空气动力学学报

OA北大核心

0258-1825

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