搜索资源列表
NACA
- 计算NACA4位翼型的程序,在E盘naca文件夹下生成翼型数据,保存为.txt格式-calculated NACA4 - airfoil procedures, the E-folder NACA airfoil data generation, preservation of. Txt format
wing-airfoil-Matlab
- 机翼翼型的matlab编程，简单易学，注重基础-Wing airfoil Matlab programming, easy to learn, and focus on basic
airfoil-insert
- catia二次开发-导入翼型，文件中包含几种常见翼型用于测试 -catia secondary development- import airfoil, the file contains several common airfoil is used to test
The-NACA-airfoil-series
- NACA Airfoil 4 Series, 5 Series, 6 Series,-NACA Airfoil 4 Series, 5 Series, 6 Series,...
read-airfoil
- Airfoil design soft distance, use is very good, very high accuracy
naca-airfoil
- 生成NACA翼型的vb程序，输入4位数naca翼型，得到翼型剖面。-NACA airfoil generates vb program, enter the 4-digit naca airfoil, get airfoil sections.
2d-airfoil-release2.0
- 2d-airfoil-release2.0，解2维机翼的面元法，运行时放在英文目录下-2d-airfoil-release2.0, solutions of two-dimensional wing panel method, the runtime directory in English
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.
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
make-2601points-from-one-airfoil
- 翼型数据插值到2601个点，使用matlab语言-Airfoil data interpolated to 2601 points, using matlab language
airfoil
- Plot a 2D airfoil and calculation of lift,pressure and drag coefficients
structered-airfoil
- structured grid generation around airfoil NACA 4 digits
unstructered-airfoil
- unstructured grid generation around airfoil
airfoil
- FORTRAN FILE AIRFOIL
AirFoil
- NASA翼型仿真器的汉化版，JAVA APPLET(NASA AIRFOIL SIMULATOR)
airfoil_generator
- Generates NACA 4 or 5 Digit Airfoil
sourse
- Airfoil CP Using Source Panel Method
vortex
- Airfoil CP Plot Using Vortex Method
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)
xfoil m files
- matlab和xfoil之间的接口，直接通过运行matlab运行xfoil，输入翼型坐标数据得到翼型的气动参数。(The interface between MATLAB and xfoil can directly run xfoil by running matlab, and the aerodynamic parameters of airfoil can be obtained by inputting airfoil coordinate data.)