风力机翼型动态失速等离子体流动控制数值研究1)
NUMERICAL STUDY ON DYNAMIC STALL FLOW CONTROL FOR WIND TURBINE AIRFOIL USING PLASMA ACTUATOR 1)
风力机翼型动态失速等离子体流动控制数值研究1) |
| 张卫国, 史喆羽, 李国强, 杨永东, 黄明其, 白云卯 |
|
NUMERICAL STUDY ON DYNAMIC STALL FLOW CONTROL FOR WIND TURBINE AIRFOIL USING PLASMA ACTUATOR 1) |
| Zhang Weiguo, Shi Zheyu, Li Guoqiang, Yang Yongdong, Huang Minqi, Bai Yunmao |
| 图8 一个振荡周期内翼型表面压力系数分布图(运动参数: $\alpha_{0}=10^\circ$, $\alpha_{1}=7^\circ$, $f=0.5$ Hz, $V=10$ m/s) |
| Fig. 8 Distribution of pressure coefficient on airfoil surface during an oscillating period (motion parameters: $\alpha_{0}=10^\circ$, $\alpha_{1}=7^\circ$, $f=0.5$ Hz, $V=10$ m/s) |
|
|