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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)
nasa0012
- 使用fortran程序对二维nasa0012标准翼型进行的网格划分。-Fortran program using the standard two-dimensional airfoil nasa0012 meshing.
2dairfoil
- 二维翼型网格生成 的 fortran程序 非常经典 易于学习 -fortram program
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
yixingraoliu
- 基于非结构网格的Jameson中心格式方法求解二维Euler方程计算翼型绕流-Jameson based unstructured grid method for solving two-dimensional central scheme Airfoil Euler equation
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
naca0012翼型网格生成
- C语言生成C型网格，求解拉普拉斯方程生成网格并计算压力系数(Solve the Laplace equation to generate the grid and calculate the pressure coefficient)
DFFD
- 直接FFD（DFFD）几何参数化方法，可以对二维翼型实现参数化，实现网格变形(DFFD parameterization technique, used to deform the 2D airfoil)
椭圆型偏微分方程生成O型网格
- 基于椭圆型偏微分方程生成二维NACA0012翼型的O型网格并求解流场(Generation of O-grid of two-dimensional NACA0012 airfoil and solution of flow field based on elliptic partial differential equation)
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。