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ausm-euler0012
- this fortran code can be used for analyse Inviscid flow over naca0012 airfoil with C_type grid. this code is developed by AUSM+ method.
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.
EulerCode
- ROUTINES FOR GENERATION OF A C-TYPE GRID SYSTEM USE FOR FLOWS PAST AN AIRFOIL
airfoil
- 三维翼型表面网格生程序,适合复杂外形计算。-this program can compute a wing s surface grid
1
- 采用偏微分方程数值解法生成翼型O型网格并采用速度势方程求低速不可压无粘流场 -Numerical solution of partial differential equations using Airfoil O-grid generation and use low-speed velocity potential Equation incompressible inviscid flow field
airfoil
- 生成翼面网格，为流体计算做准备，Fortran编写简练合理-Wing surface grid is generated, in order to prepare for the calculation of fluid, Fortran to prepare concise and reasonable
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_grid
- This Fortran Program develop for NACA0200 Airfoil Axi-symmetric grid generation. The grid is clustered in x. Program is basic level for under graduate students.
source
- 偏微分方程法生成翼型C网格程序 fortran-PDE grid generation method program fortran airfoil C
C-type-gridgeneration-for-naca0012
- this code can be used to develop C-type grid generaton for naca 0012 airfoil. by import the airfoil dots with manner of the code, you can develop c_type grid for any airfoil.
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
aerofoilgrid
- 绕翼型网格生成程序，采用O型网格，拉普拉斯方程。-Around the airfoil mesh generation process, the use of O-type grid, Laplace s equation.
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
airfoil
- 三维翼型表面网格生程序,适合复杂外形计算。-this program can compute a wing s surface grid
naca0012
- 采用椭圆型偏微分方程生成的O网格，简单实用 适合初步学习网格生成的代码， 仔细看看代码的机构 会学到实用的技巧-naca0012 airfoil with o-grid based on the elliptical partial differential equations
c_grid
- 机翼、翼型 C 网格生成程序 fortran code-fotran code ，C grid fortran fur airfoil and win
VKT.airfoil
- 通过Karman-Trefftz 翼型的网格和计算方法，使用Fortran编写，粘性计算。-Through the grid and calculation methods Karman-Trefftz airfoil, written in Fortran, viscous calculations.
structered-airfoil
- structured grid generation around airfoil NACA 4 digits
unstructered-airfoil
- unstructured grid generation around airfoil
Type o grid around the airfoil
- 实现在一个经典翼形周围画出高质量的O型网格，用fortran编写，程序简单易读。(Type o grid around the airfoil)