N - s method for solving the flow around a wing with deflection of flap is presented 给出了带襟翼偏转的三维机翼绕流的一种求解n - s方程的计算方法。
2.
A n - s method for solving the flow around a wing with deflection of flap is presented 给出了带襟翼偏转的三维机翼绕流的一种求解n - s方程的计算方法。
3.
The potential flow theory is then applied to the overlap of the slipstream and the flow over the wing 用位流理论来处理螺旋桨滑流与机翼绕流的迭加。
4.
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。
5.
This deforming method coupled with ale euler solver is applied to simulate unsteady transonic flow about oscillating airfoil ( 2 - d ) and oscillating rigid rectangular wing ( 3 - d ) . computational results are in good agreement with experimental data 本文将网格变形方法与数值解算器耦合起来求解了二维振动翼型绕流和三维振动矩形机翼绕流，计算结果与实验结果一致，证明本文的数值方法具有较高的准确性。
