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英文: The -D numerical simulation was employed to study the dynamic stall of the NREL S809 airfoil using the CFD software. The sinuous periodic flow field around the airfoil was presented when the angle of attack changing from 9°— °.
中文: 本文应用CFD软件Fluent 0对NRELS809翼型的二维动态流场进行了数值模拟,得到了翼型攻角在9°~ °范围内按正弦周期变化时的绕流流场。
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