搜索资源列表
BBB
- 风力机叶片翼型拟合，非均匀B样条拟合MATLAB程序(Wind turbine blade airfoil fitting, non-uniform B spline fitting MATLAB program)
1-C-grid
- 基于椭圆偏微分方程，针对NACA0012翼型生成C网格，生成最后的网格(C type mesh generation)
qhyx64
- 计算一般翼型的升力系数，速度和攻角可在程序中自行调整(Calculation of lift coefficient of general 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)
mvsjgg
- 基于ausm格式的欧拉方程求解程序,附带有naca0012的翼型数据,是学习计算流体力学的好例程,费尽心思编写的,注释多多()
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)
NACA_profile_generator_Matlab
- 计算 NACA 系列翼型坐标，已进行 CFD 仿真。(Calculate the coordinates of NACA wings.)
四轴 - 调试版V1.0.0 +型
- 一款关于四旋翼飞行器的源代码，经测试可用(A source code for the four rotor aircraft, tested available)
Construct2D_2.1.3
- 翼型计算的2D网格生成代码，学习和研究抛物和椭圆型网格生成算法(2D grid generation for computational fluid dynamics.Hyperbolic and elliptic grid generation available)
aaduqf1
- 基于ausm格式的欧拉方程求解程序,附带有naca0012的翼型数据,是学习计算流体力学的好例程,费尽心思编写的,注释多多()
ypjs
- 基于profile中翼型的风力机叶片设计程序，可由功率计算风机直径等参数(Based on the airfoil design program of profile, the parameters of fan diameter can be calculated by power.)
m文件
- 选定翼型的叶片设计。针对一种翼型用MATLAB绘制了翼型界面图，计算了其升力系数，最终生成长度归一的叶片模型。(blade design for the chosen airfoil)
T135_export
- Tornado，改进涡格法的MATLAB程序。自带NACA翼型库，是比较成熟的程序。简单好用。(This is the new webpage for Tornado Vortex Lattice method. Tornado is a Vortex Lattice Method for linear aerodynamic wing design applications in conceptual aircraft design or in aeronautical educati
二维Euler方程C++
- 该程序是用C++语言编写的，用来求解二维欧拉方程，采用的计算案例是二维翼型，采用中心差分格式进行离散和求解。
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.)
shape parameterization mothods
- 多学科优化参数化建模MATLAB程序，对翼型进行参数化建模(MATLAB Program for Parametric Modeling of Multidisciplinary Optimization)
MATLAB
- 离散点拟合贝塞尔曲线，可以改变阶数，求控制点并求出误差(Fitting Bezier curve with discrete points)
wangge
- 用MATLAB对NACA0012翼型进行了C型结构化网格划分(C-type structured meshing of NACA0012 airfoil is carried out with MATLAB)
NACA
- NACA翼型坐标生成文件，可根据输入NACA四位数字，生成NACA坐标(NACA airfoil coordinate generation file, which can generate NACA coordinates based on input NACA four digits)