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5 CFD和OSU风洞试验结果对比($Re_{c}=1.0\times 10^{6}$, $\alpha_{0}=14^\circ$, $\alpha_{1}=10^\circ$, $f=1.83$ Hz) |
| Fig. 5 Comparison between the results of CFD calculation and OSU wind tunnel test ($Re_{c}=1.0\times 10^{6}$, $\alpha_{0}=14^\circ$, $\alpha_{1}=10^\circ$, $f=1.83$ Hz) |
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