Three-dimensional Navier-Stokes equations were solved by finite volume method.

采用有限容积法，求解全三维N-S方程。

The method can organically unite the Navier solution and the Levy solution and has the advantages of rapid convergence and high precision.

本方法可以将经典的纳维叶解和李维解法有机地统一起来，且收敛速度快，计算精度高。

The basic differential equations of orthotropic sandwich with initial deflection was established, and solved by Navier dual- trigonometric series.

方程组的求解采用改进的纳维叶双三角级数法，得到了临界屈曲载荷的计算公式。

The unstructured viscous grids of M6 wing and the simple flow results of corresponding Navier-Stokes solution based on the present grid are also provided.

同时给出了利用该方法生成的M6机翼非结构粘性网格来求解机翼粘性绕流的简单算例。

The generation and evolution of turbulent spots using the wall impulse model in the plane Couette flow are studied by direct numerical simulation of Navier-Stokes equations.

湍流斑是近壁剪切流动中的重要现象，它们的生成和发展与流动转捩和湍流的形成密切相关。

In a perturbation analysis, a two-dimensional theoretical solution based on Navier- Stokes equations is constructed for gaseous slip flows in a micro-channel with different slip conditions.

以微直通道内气体滑移流动为例，采用扰动分析方法，结合不同阶滑移条件，得出N-S方程的理论解。