搜索资源列表
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
- ＰＳＩＣ算法进行编程计算ＰＳＩＣ算法进行编程计算-st
naca
- 一款用来生成nasa翼型外形的小软件，解压后可以方便应用-Nasa airfoil shape used to generate a small software application can be easily decompressed
airfoildesign
- 使用作业调度算法，是关于一个作业调度算法的东西-Horizontal axis wind turbine (HAWT) is presently the main device for wind power. With the development of large-scale wind turbine, the research of airfoil designing which take a critical role in wind energy efficiency becomes
Airfoil-Nondimention
- 简单的程序,希望能有用，希望能帮助想要得到帮助的人。-simple program
nasa0012
- 使用fortran程序对二维nasa0012标准翼型进行的网格划分。-Fortran program using the standard two-dimensional airfoil nasa0012 meshing.
source
- 偏微分方程法生成翼型C网格程序 fortran-PDE grid generation method program fortran airfoil C
airfoil
- 二维翼型绕流非结构化网格，用FORTRAN编写，可以作为参考-Two-dimensional unstructured grid flow around airfoils, written in FORTRAN, can be used as reference
boundarylayer
- 计算弦长为L=8m、相对厚度为0.12的对称儒科夫斯基翼型受到的摩擦阻力和摩擦阻力系数，附面层厚度分布（附报告）-Calculated chord length L = 8m, the relative thickness of 0.12 Ru Khodorkovsky symmetric airfoil subject to friction and friction coefficient, boundary layer thickness distribution (with report
aerofoilgrid
- 绕翼型网格生成程序，采用O型网格，拉普拉斯方程。-Around the airfoil mesh generation process, the use of O-type grid, Laplace s equation.
Fluent2D
- 飞机翼型的升力系数、阻力系数、压力中心等计算-Aircraft airfoil lift coefficient, drag coefficient, center of pressure computation
airfoil
- 这是一个很好的程序，好动一拿出来和大家一起分享-This is a very good program, active up to share with everyone
two.boundary
- Two boundary mesh generation around naaca airfoil
fortran-files
- 文件1.f90：生成翼型naca0012的椭圆网格，并计算流场，给出壁面压力分布 文件2.f90：maccormack方法解一维burger s方程 文件3.f90：解一维laval管流动，其进出口均为亚音速，喉道后部有激波-File 1.f90: generate the airfoil naca0012 elliptical rotary cell, and calculate the flow field, given the wall pressure distributio
P_Q
- 2MW风机的最大功率跟踪(根据叶片翼型计算)-The maximum power point tracking of the 2MW wind turbine according to the blade airfoil
arc-parameter-in-extraction
- 提取叶片截面叶型面的中弧线参数，通过该方法可以较精确的提取叶片截面的中弧线-Extraction parameters of the camber line of the airfoil surface of the blade section by this method can be more accurate extraction of the camber line of the blade section
naca4gen
- Matlab 原程序生成 NACA 机翼坐标，可以用作CAD 的输入源。-"naca4gen" Generates the NACA 4 digit airfoil coordinates with desired no. of panels (line elements) on it.
yixing_fuban_1
- 描述翼型生成腹板 其中生成的腹板用于有限元计算-Descr iption the airfoil generates web which generated web for finite element calculation
FoilSim
- FoilSim is interactive simulation software that determines the airflow around various shapes of airfoils.-The software calculates the lift of the airfoils, allowing students to learn the factors that influence lift. The software includes a stall mode
FULTTER-COM
- 计算二元机翼的颤振速度，包含一个经过处理的时间延迟环节-Calculated airfoil flutter speed, contains a treated time delay link