Numerical investigation on aerodynamic performance of a novel vertical axis wind turbine with adaptive blades

被引:92
|
作者
Wang, Ying [1 ]
Sun, Xiaojing [1 ]
Dong, Xiaohua [2 ]
Zhu, Bing [1 ]
Huang, Diangui [1 ]
Zheng, Zhongquan [3 ]
机构
[1] Univ Shanghai Sci & Technol, Shanghai 200093, Peoples R China
[2] Shanghai Univ, Shanghai 200072, Peoples R China
[3] Univ Kansas, Aerosp Engn Dept, Lawrence, KS 66045 USA
基金
中国国家自然科学基金;
关键词
Adaptive blade; Darrieus vertical axis wind turbines; Computational Fluid Dynamics; Numerical simulation; Aerodynamic performance; TURBULENCE MODELS; SOLIDITY; AIRFOIL; FLOWS;
D O I
10.1016/j.enconman.2015.11.003
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this paper, a novel Darrieus vertical axis wind turbine was designed whose blade can be deformed automatically into a desired geometry and thus achieve a better aerodynamic performance. A series of numerical simulations were conducted by utilizing the United Computational Fluid Dynamics code. Firstly, analysis and comparison of the performance of undeformed and deformed blades for the rotors having different blades were conducted. Then, the power characteristics of each simulated turbine were summarized and a universal tendency was found. Secondly, investigation on the effect of blade number and solidity on the power performance of Darrieus vertical axis wind turbine with deformable and undeformable blades was carried out. The results indicated that compared to conventional turbines with same solidity, the maximum percentage increase in power coefficient that the low solidity turbine with three deformable blades can achieve is about 14.56%. When solidity is high and also turbine operates at low tip speed ratio of less than the optimum value, the maximum power coefficient increase for the turbines with two and four deformable blades are 7.51% and 8.07%, respectively. However, beyond the optimal tip speed ratio, the power improvement of the turbine using the deformable blades seems not significant and even slightly worse than the conventional turbines. The last section studied the transient behavior of vortex and turbulent flow structures around the deformable rotor blade to explore the physical mechanism of improving aerodynamic performance. The adaptive blades could obviously suppress the separation of flow from the blade surfaces. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:275 / 286
页数:12
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