搜索资源列表
xfoil6.97
- MIT教授编写的大名鼎鼎的翼型性能计算软件-Airfoil performance computing software
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
Shock-Wave-Calculation
- 用CFD方法计算超声速下小攻角翼型产生的激波-CFD method with a small angle of attack under supersonic shock wave generated airfoil
panel
- 本程序是面元法，主要为了求解绕翼型速度分布。-panel method calculate velocity distribution
NACA0012-Ogrid
- NACA0012翼型O网格生成；速度势方程解流场-NACA0012 airfoil O mesh generation flow field velocity potential equation
diverge
- 细长体，薄翼型的气弹发散特性研究，包括发散动压，发散模态等-Aeroelastic divergence characteristics of unguided, slender body, multi-stage launch vehicles
naca0012-24-15
- 用于分析高雷诺数naca0012翼型和圆柱绕流，基本可用，但数值误差大，可通过修该某些参数缩小误差-For the analysis of high Reynolds number flow around a cylinder naca0012 airfoils and basic available, but the numerical error, the error can be reduced by modifying cert
c_grid
- 机翼、翼型 C 网格生成程序 fortran code-fotran code ，C grid fortran fur airfoil and win
CFD
- 这是一个求解NACA0012翼型在不同马赫数与攻角下的流场的Fortran源代码。计算格式采用了原始AUSM、AUSMDV以及AUSM+格式。为了提高计算精度，使用了不同限制器的MUSCL插值。-This is a Fortran source code for solving the flow field around the NACA0012 airfoil at different Mach numbers and angles
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
OCFD2d_dxyz_3rd
- 三阶高精度软件，用处很多，在很多公司都用使用。适合翼型分析-Three order high precision software, has many uses, are used in many companies. Suitable for airfoil analysis
pablo
- 国外使用面元法计算翼型升力的matlab程序包-matlab program using panel method to solve the lift of the foil
matlab-xfoil
- 通过matlab调用xfoil程序，对翼型升阻力力矩进行计算，并将计算结果生成结果文件，程序中对三种翼型进行了计算，用户可根据需要删减或复制程序的相同部分即可-Xfoil by calling the same part of matlab procedures, the airfoil lift and drag torque is calculated, and the calculated results file is gene
OpenCFD-EC2D-1.5.4
- 程序、算例及更新版的理论手册可在本贴的主贴中下载 (OpenCFD-EC2D-1.1.rar) 包含了一个RAE2822翼型绕流的完整算例。-Open CFD code for Engineering Computing
AirfoilNoise--data
- 某型飞机机翼在风洞中测得的翼型自噪声数据，可用于多输入单输出的神经网络建模。-A certain type of aircraft wings in the wind tunnel measured airfoil self-noise data, can be used for multi-input single-output neural network modeling.
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.
griddeform
- 用于翼型结构化网格的网格变形程序，采用径向基函数方法，容易拓展到三维。-grid deforming program for airfoil structured grid, based on radial basis function method, easily extended to three-dimensional.
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.
ga_v1
- 用于翼型优化的遗传算法，比较简单，适用于一维情况，优化升力等- Genetic algorithms for optimization airfoil is relatively simple for the one-dimensional case, the optimization of the lift, etc.
CST_airfoil_fitting
- 一个拟合CST曲线的程序，用来做翼型优化使用（也可以用到其它曲线拟合上）。 首先读入一个翼型数据，反求这个翼型的6*2个控制参数。通过这修改这个12个控制参数（其中的任意几个），来达到生成新的翼型的目的。(使用了NASA0714翼型作为例子 )-it is a code for airfoil curves fitting, which based on CST formula.Firstly, the program read a