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- 计算二维翼型升阻力系数及翼型设计，广泛的用于风机翼型以及风力机等翼型设计-Calculation of two-dimensional airfoil lift and drag coefficients and airfoil design
k_pohlhausen
- 已知翼型坐标及其各点的马赫数分布用波豪森近似方法求解层流附面层厚度-The known airfoil coordinates of its point of Mach number distribution wave the Stockhausen approximation method for solving laminar flow boundary layer thickness
flapping
- 使用非定常涡格法(UVLM)计算一种简单扑翼机的升力。对应文献Time Domain Modeling of Unsteady Aerodynamic Forces on a Flapping Airfoil -Eric Durand（MIT Master thesis）-Unsteady vortex lattice method (UVLM) a simple flapping wing machine lift. Corresponding literature Time Domain M
WING-MATLAB-CODE
- 详细介绍了飞机翼型的分析过程，具有很好的实际应用效果-Aircraft airfoil analysis process, and has a very good application effect
wogewoge0
- 涡格法求解翼型的气动力，包括阻力 升力 法向力-Vortex lattice method for solving the the aerodynamic airfoil, including resistance lift normal force
center
- jamson中心格式求解naca0012翼型的绕流，计算精度较高-format solve naca0012 airfoil of jamson center around the flow calculation accuracy
pablo_4kth
- Potential flow around Airfoils with Boundary Layer coupled One-way (Pablo) is a pedagogical low-speed airfoil analysis program written in MATLAB. It uses a one way coupled inviscid + boundary layer model.
Matlab-Optimization-tools
- 基于Matlab软件中的优化算法和优化工具，针对风力机翼型通用型线集成表达式建立了优化数学模型。以风力机翼型的最大升阻比为优化设计目标函数，翼型形状控制方程的系数为设计变量，翼型的厚度和弯度为约束条件，设 计得到了相对厚度为18％的风力机翼型，并对其性能进行了计算分析。研究结果拓宽了风力机叶片翼型的设计思路和设计方法。-Based the Matlab software optimization algorithm and optimization tools for the integra
Wind-turbine-blades-design
- 本文利用MATLAB的遗传算法工具箱，对弦长和扭角沿风力机展向分布进行优化，得到设计工况下的最优叶片设计。目标函数是设计工况下基于动量叶素理论和Glauert等修正所得出的功率系数。在设计工况下得到的设计结果，其功率系数在一定的风速范围内都能保持一个较高的数值，同时其有效攻角分布大致都在所选翼型的升力与阻力系数的比值最大处，与理论相符合。其结果说明该优化实际的有效性。-In this paper, the use of MATLAB genetic algorithm toolbox, chor
Aerodynamic-performance
- 提高风力机将风能转化为机械能的效率，根据我国西北地区的风频风能曲线，用最优设计攻角沿叶片轴线的非线性分布修正传统Wilson算法，优化设计大型水平轴风力机叶片的气动性 能．该优化设计利用Madab优化工具箱，优化速度干涉因子的迭代计算，提高计算效率；考虑多翼型和变攻角等因素对叶片外形优化的影响，从结构及加工工艺角度修正翼型．通过对1．2MW风力发电机组叶片外形的气动性能计算和优化设计，结果表明该优化设计的有效性和可行性，可为风力机叶片外形设计提供参考．-Improve wind turbin
WindTurbineSpr
- OPTIMIZATION OF A WIND TURBINE ROTOR WITH VARIABLE AIRFOIL SHAPE VIA A GENETIC ALGORITHM
source-code
- 采用斜激波-膨胀波理论计算流场中对称菱形翼型各个表面的压力系数及翼型升阻力系数-Using oblique shock- expansion wave theory rhombus symmetrical airfoil flow field in each surface pressure coefficient and airfoil lift and drag coefficients
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
Xfoil-Interface
- 翼型气动计算软件XFOIL的Matlab界面-Airfoil interface with Matlab computing software XFOIL
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
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
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
c_grid
- 机翼、翼型 C 网格生成程序 fortran code-fotran code ，C grid fortran fur airfoil and win