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11 深失速, 翼型动态分离涡Q等值面发展图($\alpha_{0}=10^\circ$, $\alpha_{1}=10^\circ$, $f=3$ Hz, $V=30$ m/s, 正行程迎角16.0$^\circ$) |
| Fig. 11 Development of Q iso-surface for dynamic separation vortex around airfoil, deep stall ($\alpha_{0}=10^\circ$, $\alpha_{1}=10^\circ$, $f=3$ Hz, $V=30$ m/s, Positive stroke 16.0$^\circ$ AOA) |
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