搜索资源列表
pyxfoil
- 二维翼型坐标生成与气动力计算
siaodaoseng
- 这是一种画翼型的方法。西奥道森方法画翼型，该方法画的翼型准确。-a code used to plot airfoil!
Potential_Flow_Simulator
- 翼型在势流中的模拟，以求得其压力系数分布，升力系数等-Airfoil in potential flow in the simulation, with a view to obtaining the pressure coefficient distribution, the lift coefficient
aiefoilconclution
- 已知实验测得的翼型的压力分布和翼型数据，计算其升力系数和阻力阻力-Known experimental measured airfoil pressure distribution and airfoil data to calculate the lift coefficient and drag resistance
Airfoil_Analyzer
- Matlab编写的一个翼型分析软件，且包含了大量常见的翼型数据-An airfoil analysis software written in Matlab, and contains a large number of common airfoil data
FourSeriesairfoil
- naca翼型坐标生成程序（Ｍａｔｌａｂ）-naca airfoil coordinates generating program (Matlab)
TheNURBSBook
- 工程界几何模型参数化用到的NURBS曲线生成的理论和相关源代码。可用以翼型参数化、船舶外形参数化等-the theory of NURBS curve generation and the related source code for Engineering of geometric model parameterization . Airfoil parameterization and ship shape parameteri
wingtheory
- 机翼及其翼型理论，推导过程比较完善，相关资料中文的比较少见，较为珍贵！-Wing and airfoil theory, the derivation process is complete, relevant information in Chinese is relatively rare, more precious!
AirFoil
- NASA翼型仿真器的汉化版，JAVA APPLET(NASA AIRFOIL SIMULATOR)
TTM方法生成翼型网格MATLAB程序
- 计算流体力学小程序：使用TTM方法生成机翼翼型网格(generate the wing grid with TTM method)
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
- 用来生成翼型NACA0012的计算网格，此网格可用于后续计算。程序数据在附件里。(A computational mesh used to generate airfoil NACA0012)
翼型失速延迟修正
- 基于三种失速延迟模型对CL、CD进行修正的程序(Program for modifying CL and CD based on stall delay model)
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)
NACA0012
- 此文件为naca0012翼型的msh格式(msh format of NACA0012 airfoil)
O网格椭圆型生成法及求解势流方程
- 自动生成NACA0012翼型的网格，并在网格的基础上求解势流方程，fortran编译，可自改(O grid that mainly generates NACA0012 airfoil)
NACA0012
- NACA0012翼型的网格生成以及零攻角绕流流场计算(Mesh generation of NACA0012 airfoil and calculation of flow field around zero angle of attack)
raetaf05.tar
- nasa一款翼型的所有数据 通用于各个软件(RAE 2822 AIRFOIL (rae2822-il))
Vortex2D
- 输入naca四位数翼型，和环境参数，可以计算得到压力分布和升力系数(Pressure distribution and lift coefficient can be calculated by inputting NACA four-digit airfoil and environmental parameters.)
DIY-Wind-Turbine-Analyzer-master
- 用叶素动量理论来求解维尔森方法中，翼型气动性能，轴向与切向诱导因子的计算程序(Calculation of airfoil induction factor)