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 |
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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6 脉冲工作模式下DBD等离子体诱导涡结构$Q=0.3$等值面(运动参数: $\alpha_{0}=10^\circ$, $\alpha_{1}=7^\circ$, $f=0.5$ Hz, 激励电参数: $DR=0.5$, $f_{p}=100$ Hz) |
| Fig. 6 $Q=0.3$ iso-surface of vortices structure induced by pulsed mode DBD plasma (motion parameters: $\alpha_{0}=10^\circ$, $\alpha_{1}=7^\circ$, $f=0.5$ Hz, actuation electric parameters: $DR=0.5$, $f_{p}=100$ Hz) |
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