搜索资源列表
chaoyinsuyixing
- 该程序研究了攻角为2度的条件下超音速翼型的气动力特性。-This program studies the aerodynamic characteristics of of supersonic airfoils under an attack angle of 2 degrees .
external_compressible
- 问题考虑围绕翼型的流动在4°攻角和一个自由流马赫数0.8。流量是跨音速，并有近于上（吸气）侧中间弦m/c=0.45一个相当强烈的震撼。弦长为1米。-The problem considers the flow around an airfoil at an angle of attack and a free stream Mach number of ( ). The flow is transonic, and has a fairly stron
find-from-excel
- 查询EXCEL中翼型的空气动力系数值,如气动力矩，升力系数，阻力系数等-find date excel
Wilson_optimization
- 基于wilson算法的风力机叶片翼型的优化和三维坐标转换-Wind turbines airfoil optimization and three-dimensional transformation based on wilson algorithm
xfoilP4
- 进行航空，航天的翼型或者风力机叶片的空气动力学分析-Aerodynamic analysis of aviation, aerospace or wind turbine blade airfoil
Xfoil699src
- 对风力机或水轮机的不同叶片翼型进行分析和计算-Different wind turbine blade or turbine airfoil analysis and calculation
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
Matlab-Xfoil
- 使用Matlab语言生成Xfoil的计算文件，并调用Xfoil快速计算翼型的气动力-Using Matlab language generation Xfoil calculation file and call Xfoil quick calculation of aerodynamic airfoil
airfoilprep
- 一种用于风力机设计和性能校核的翼型气动数据预处理，包括panel插值，全周插值，3D修正等。使用python语言 -Airfoil data preprocessing for wind turbine design and performance verification using python language
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
gold
- 基于黄金分割法的一维搜索算法，被优化函数为翼型的阻力，变量为翼型的展弦比-Based on Golden Section one-dimensional search algorithm is optimized airfoil resistance function, variable aspect ratio airfoil
yixing
- 通过翼型表面温度以及流场分布的特征以及计算-Through the airfoil surface temperature and flow field distribution features
dflo-code-36
- deal.II有限元数值计算库的子程序。用于激波，翼型绕流等方面计算。-Subroutine of deal.II finite element numerical calculation library. Calculation of the flow around the airfoil for shock wave.
pablo
- 风力机翼型分析软件PABLO，内含多个翼型数据，可实现翼型气动性能分析与计算结果可视化。-A wind turbine airfoil design software developed with matlab
风力机动态特性研究
- 哥廷根188翼型水平轴风力发电机关于雷诺数的影响研究
TTM
- 运用CFD所学知识进行编程计算，用TTM方法生成翼型网格-The use of CFD computing programming knowledge to generate airfoil grid method with TTM
Caculation-for-NACA24012
- 程序包二维翼型，计算涡面元系数，画出翼型，压力系数，升力系数，并在来流速度为1的时候画出翼型上下表面的速度-Caculation for airfoil including
fortran-naca0012
- foutran语言，孤立翼型绕流程序,程序很长，需要耐心看，这是北航的作业程序-fortran language, isolated on the Flow around a program, the program is very long, you need to be patient, this is Northern operational procedures
par
- 基于Bezier曲线的翼型参数化，相比基于样条曲线的翼型参数化方法，该方法具有较好的鲁棒性-airfoil parameterization method base on Bezier Curve,it is more stable than the parameterization method base on Spline
zuobiaobianhuan
- 这个程序主要是把二维翼型坐标变换成三维翼型坐标，通过翼型位置-弦长-扭角等参数得到三维翼型坐标，完成后面的三维建模-This program is mainly two-dimensional airfoil coordinate into the three-dimensional coordinates of the airfoil, the airfoil by position- to give the three-dimensional coordinates of the airfo