Numerical results show that the present method is effective one for solving the flow around wing with flap deflection.

数值算例表明本方法是求解带襟翼偏转的机翼绕流的有效方法。

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Numerical results show that the present method is effective one for solving the flow around wing with flap deflection.

数值算例表明本方法是求解带襟翼偏转的机翼绕流的有效方法。

youdao