搜索资源列表
pyxfoil
- 二维翼型坐标生成与气动力计算
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
- 有Fortran语言编写的计算二维翼型的程序，适用于航空航天行业-Fortran language with the calculation of two-dimensional airfoil procedures for aerospace industry
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
src
- 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.
src
- 计算二维翼型升阻力系数及翼型设计，广泛的用于风机翼型以及风力机等翼型设计-Calculation of two-dimensional airfoil lift and drag coefficients and airfoil design
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
Airfoil-2D-Panelmethod
- 使用Matlab语言编写的二维翼型Hess-smith面元法气动力计算程序-Using Matlab language Hess-smith airfoil aerodynamic surface element method calculation program
Caculation-for-NACA24012
- 程序包二维翼型，计算涡面元系数，画出翼型，压力系数，升力系数，并在来流速度为1的时候画出翼型上下表面的速度-Caculation for airfoil including
zuobiaobianhuan
- 这个程序主要是把二维翼型坐标变换成三维翼型坐标，通过翼型位置-弦长-扭角等参数得到三维翼型坐标，完成后面的三维建模-This program is mainly two-dimensional airfoil coordinate into the three-dimensional coordinates of the airfoil, the airfoil by position- to give the three-dimens
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
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)
opt_foil
- 二维翼型优化程序，需要调用fluent和tecplot(2D foil optimization technique, need to use fluent and tecplot)
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)