The results showed that different leading edge profiles could induce different forms of separation and that the induced shear layers are also different.
计算结果表明：三种不同剖面形状的前缘可以诱导产生不同的前缘分离，形成的各前缘剪切层的特点也不同。
In this paper, separation control on Joukowsky airfoil having leading edge rotational cylinder is investigated by numerical simulation method.
本文使用数值模拟方法研究了活动翼面对翼型背风面分离的控制作用。
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