搜索资源列表
aerodynamics_Analyzer
- 这是一个小，但是非常有用的工具，用于分析飞行器的翼型。可以分析和比较飞机机翼几何特征，很快的绘制出机翼。包括：前缘半径、翼弦、厚度、中弧线、弯度和尾缘厚度等，这些参数直接影响翼型的气动性能。 - airfoil Analyzer Small but essential tool for all Aerospace Engineers and Scientists.
1
- 采用偏微分方程数值解法生成翼型O型网格并采用速度势方程求低速不可压无粘流场 -Numerical solution of partial differential equations using airfoil O-grid generation and use low-speed velocity potential Equation incompressible inviscid flow field
airfoil
- Fortran语言开发计算程序，用于有限元计算，是学习Fortran必备的文件
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
airfoil
- 有Fortran语言编写的计算二维翼型的程序，适用于航空航天行业-Fortran language with the calculation of two-dimensional airfoil procedures for aerospace industry
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.
karmen_treffitzz-airfoil
- karman airfoil is very important in study of aircraft in particular and aerodynamic systems in general. study of karman airfoil in innovative idea in the field of aerodynamics.
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
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
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
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
airfoil-of-wind-turbine
- 计算风力机叶片参数，自动绘制叶片的参数曲线-Calculate the parameters of wind turbine blades, vanes automatically draw parametric curves
matlab-xfoil
- 通过matlab调用xfoil程序，对翼型升阻力力矩进行计算，并将计算结果生成结果文件，程序中对三种翼型进行了计算，用户可根据需要删减或复制程序的相同部分即可-Xfoil by calling the same part of matlab procedures, the airfoil lift and drag torque is calculated, and the calculated results file is generated, the program for the thr
Qwin
- 组合翼面涡法Fortran核心程序，求解机翼的速度和压力分布-Combination of airfoil core eddy France Fortran program to solve the wing velocity and pressure distribution
naca-airfoil
- 生成NACA翼型的vb程序，输入4位数naca翼型，得到翼型剖面。-NACA airfoil generates vb program, enter the 4-digit naca airfoil, get airfoil sections.
2d-airfoil-release2.0
- 2d-airfoil-release2.0，解2维机翼的面元法，运行时放在英文目录下-2d-airfoil-release2.0, solutions of two-dimensional wing panel method, the runtime directory in English
Whirlwind_exe_9-30-2005
- 这是用C++语言编写的一个飞行器翼型估算软件-this is a software of airfoil caculation.
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