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12 浅失速, 翼型动态分离涡Q等值面发展图($\alpha_{0}=10^\circ$, $\alpha_{1}=7^\circ$, $f=0.5$ Hz, $V=10$ m/s) |
| Fig. 12 Development of Q iso-surface for dynamic separation vortex around airfoil, light stall ($\alpha_{0}=10^\circ$, $\alpha_{1}=7^\circ$, $f=0.5$ Hz, $V=10$ m/s) |
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