Effect of solidity on aerodynamic forces around straight-bladed vertical axis wind turbine by wind tunnel experiments (depending on number of blades)

被引:84
|
作者
Li, Qing'an [1 ]
Maeda, Takao [2 ]
Kamada, Yasunari [2 ]
Murata, Junsuke [2 ]
Shimizu, Kento [2 ]
Ogasawara, Tatsuhiko [2 ]
Nakai, Alisa [2 ]
Kasuya, Takuji [2 ]
机构
[1] Mie Univ, Div Syst Engn, 1577 Kurimamachiya Cho, Tsu, Mie 5148507, Japan
[2] Mie Univ, Div Mech Engn, 1577 Kurimamachiya Cho, Tsu, Mie 5148507, Japan
关键词
Wind turbine; Pressure distributions; Numbers of blades; Six-component balance; Wind tunnel experiments; REYNOLDS-NUMBER; PERFORMANCE; WAKE; PROFILE; ENERGY; FIELD;
D O I
10.1016/j.renene.2016.05.054
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
The prediction of aerodynamic forces around straight-bladed Vertical Axis Wind Turbines (VAWT) is important for wind turbine applications. This paper focused on evaluating the aerodynamic forces acting on a single blade, depending on the different numbers of blades in wind tunnel experiments. In this study, numbers of blades were from two to five and the cross-sectional shape of the tested airfoil was a NACA0021. Firstly, the power coefficient was measured by a torque meter and a six-component balance. Secondly, pressures acting on the surface of rotor blades were measured during rotation by multiport pressure devices. Then, the evolutions of normal coefficient, tangential coefficient and lift-to-drag ratio C-L/C-D, which were obtained from pressure distributions, were discussed. Finally, the power coefficients calculated by pressure distributions were compared with the experiment data of the torque meter and the six:component balance. The results showed that the pressure difference substantially decreased with the increase of solidity. In addition, the values of six-component balance and torque meter showed smaller values than those calculated by pressure distributions. In words, these results provided theoretical significance towards the development of a simple design for straight-bladed VAWT. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:928 / 939
页数:12
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