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。

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

youdao

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。

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

youdao