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)