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Effects of vortex generators on aerodynamic performance of thick wind turbine airfoils

机译:涡流发生器对厚型风力机翼型气动性能的影响

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摘要

The effects of vortex generators (VGs) on aerodynamic performance of thick wind turbine airfoils CAS-W2-350, CAS-W2-400, and CAS-W1-450 are presented. The measurements were carried out at a Reynolds number of 1 million with two experimental setups. Aerodynamic performance of testing models is obtained by measuring the surface pressure. The effects of height, chordwise position, and spanwise spacing between neighbor VGs are investigated, as well as the effect of a second row of VGs. The results show that the maximum lift coefficient increases with VGs installed towards the leading edge of airfoils but the lift at small angles of attack decreases when the chordwise position of VGs is smaller than 20% chord. The spanwise spacing between neighbor VGs has small effects on lift coefficient of CAS-W2-350, but strongly affects that of CAS-W2-400 before stall. The second row of VGs could further increase the lift coefficient at large angles of attack depending on the install positions and size of VGs. (C) 2016 Elsevier Ltd. All rights reserved.
机译:提出了涡流发生器(VGs)对厚风轮机翼CAS-W2-350,CAS-W2-400和CAS-W1-450的空气动力学性能的影响。用两个实验装置以一百万的雷诺数进行测量。测试模型的空气动力学性能是通过测量表面压力获得的。研究了相邻VG之间的高度,弦向位置和翼展方向间距的影响,以及第二排VG的影响。结果表明,当VG朝翼型前缘安装时,最大升力系数增加,但当VG的弦向位置小于20%弦时,小迎角的升力减小。相邻VG之间的翼展方向间距对CAS-W2-350的升力系数影响很小,但对失速前的CAS-W2-400升力系数影响很大。根据VG的安装位置和尺寸,第二排VG可以在较大迎角处进一步提高升力系数。 (C)2016 Elsevier Ltd.保留所有权利。

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