Effects of nonuniform incident velocity on a dynamic wind turbine airfoil

被引:23
|
作者
Gharali, Kobra [1 ]
Johnson, David A. [1 ]
机构
[1] Univ Waterloo, Dept Mech & Mechatron Engn, Wind Energy Grp, Waterloo, ON N2L 3G1, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
wind turbine; dynamic stall; S809; airfoil; numerical simulation; unsteady incident velocity; unsteady freestream; UNSTEADY FREESTREAM; OSCILLATING AIRFOIL; FREE-STREAM; STALL; SIMULATION;
D O I
10.1002/we.1694
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
For further insight into the performance of a horizontal axis wind turbine blade section under yaw loads, a 2D numerical simulation of a pitching S809 airfoil under dynamic stall with an unsteady incident velocity is presented. The streamwise incident velocity and pitch angle of incidence oscillated with the same frequency but with a range of phase differences,-phi. Changing phi caused variation of the results, which can be highlighted as significantly augmented and dramatically damped dynamic stall loads, both increasing and decreasing trends for vortex growth time during phi increase, a shifted location of the maximum loads and a change in the order of the vortex pair circulation in each cycle. The results showed strong dependency on the velocity and acceleration of the freestream during dynamic stall, which categorized the results in four individual subdomains with different behaviors. Copyright (c) 2014 John Wiley & Sons, Ltd.
引用
收藏
页码:237 / 251
页数:15
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