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- 逆风格式欧拉方程求解naca0012二维翼型流场程序，内附网格文件和输入参数。-Wind Euler equations naca0012 format two-dimensional airfoil flow field procedures, containing the grid files and input parameters.
airfoilgrd
- 双曲生成二维翼型C型网格（后缘可以有台阶）-Generate two-dimensional airfoil C-hyperbolic grid (there are steps you can back edge)
airfoil
- 二维翼型绕流非结构化网格，用FORTRAN编写，可以作为参考-Two-dimensional unstructured grid flow around airfoils, written in FORTRAN, can be used as reference
2dairfoil
- 通过求解偏微分方程生成二维翼型的网格，适合初学者学习网格生成方面的知识。-Partial differential method airfoil mesh generation process
Laplace
- 求解椭圆型方程生成二维翼型网格，并采用逐线松弛迭代技术求解了二维翼型绕流，这是CFD计算中的典型例子，是cfd初学者的很好的学习例子。(Solving elliptic equations, generating two-dimensional airfoil mesh, and using line relaxation iterative technique to solve the two-dimensional airfoil flow, which is a typical examp
基于Laplace方程的翼型O-形网格生成器
- 源程序使用C++编写，通过求解椭圆型微分方程（拉普拉斯方程）生成绕翼型的O-形二维网格。网格坐标以.plt的格式输出，可使用tecplot进行查看。