Investigations on the Unsteady Aerodynamic Characteristics of a Horizontal-Axis Wind Turbine during Dynamic Yaw Processes

被引:30
作者
Wang, Xiaodong [1 ]
Ye, Zhaoliang [1 ,2 ]
Kang, Shun [1 ]
Hu, Hui [3 ]
机构
[1] North China Elect Power Univ, Minist Educ, Key Lab Condit Monitoring & Control Power Plant E, Beijing 102206, Peoples R China
[2] China Huaneng Clean Energy Res Inst, Beijing 102209, Peoples R China
[3] Iowa State Univ, Dept Aerosp Engn, Ames, IA 50011 USA
基金
中国国家自然科学基金;
关键词
HAWT; aerodynamic characteristics; dynamic yawing process; near wake; start-stop yaw velocity; POWER EXTRACTION; PERFORMANCE; INFLOW; OPTIMIZATION; BLADES; IMPACT; LOADS; WAKE; CFD;
D O I
10.3390/en12163124
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Wind turbines inevitably experience yawed flows, resulting in fluctuations of the angle of attack (AOA) of airfoils, which can considerably impact the aerodynamic characteristics of the turbine blades. In this paper, a horizontal-axis wind turbine (HAWT) was modeled using a structured grid with multiple blocks. Then, the aerodynamic characteristics of the wind turbine were investigated under static and dynamic yawed conditions using the Unsteady Reynolds Averaged Navier-Stokes (URANS) method. In addition, start-stop yawing rotations at two different velocities were studied. The results suggest that AOA fluctuation under yawing conditions is caused by two separate effects: blade advancing & retreating and upwind & downwind yawing. At a positive yaw angle, the blade advancing & retreating effect causes a maximum AOA at an azimuth angle of 0 degrees. Moreover, the effect is more dominant in inboard airfoils compared to outboard airfoils. The upwind & downwind yawing effect occurs when the wind turbine experiences dynamic yawing motion. The effect increases the AOA when the blade is yawing upwind and vice versa. The phenomena become more dominant with the increase of yawing rate. The torque of the blade in the forward yawing condition is much higher than in backward yawing, owing to the reversal of the yaw velocity.
引用
收藏
页数:23
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