搜索资源列表
NACA
- 计算NACA4位翼型的程序,在E盘naca文件夹下生成翼型数据,保存为.txt格式-calculated NACA4 - airfoil procedures, the E-folder NACA airfoil data generation, preservation of. Txt format
aerofoil
- 一个能将一般图纸（CAD或其他）的弯曲或者其他变形之后的翼型复原成原始翼型-one can generally drawings (CAD or other) or other of bending deformation of the airfoil recovery after the original wing into Type
aiefoilconclution.rar
- 已知实验测得的翼型的压力分布和翼型数据，计算其升力系数和阻力阻力,Known experimental measured airfoil pressure distribution and airfoil data to calculate the lift coefficient and drag resistance
EULERAUSM
- 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，便于阅读-Ausm format based on the Euler equation procedures, comes with naca0012 the airfoil data, computational fluid dynamics is a good learning routines, the effort to prepare, notes a lot
EulerCode
- ROUTINES FOR GENERATION OF A C-TYPE GRID SYSTEM USE FOR FLOWS PAST AN AIRFOIL
YcYf
- 计算翼型的最大厚度弦向位置以及对翼型的点坐标进行均匀差值-Calculate the maximum thickness of airfoil chord and the airfoil to the location coordinates of the point difference between uniform
airfoil
- 利用FORTRAN 开发的机翼数值模拟的源代码。其中包括了网格划分。-The development of the use of FORTRAN source code for the numerical simulation of the wing. Including mesh.
airfoilgrd
- 双曲生成二维翼型C型网格（后缘可以有台阶）-Generate two-dimensional airfoil C-hyperbolic grid (there are steps you can back edge)
C-type-gridgeneration-for-naca0012
- this code can be used to develop C-type grid generaton for naca 0012 airfoil. by import the airfoil dots with manner of the code, you can develop c_type grid for any airfoil.
NACA-series-airfoil-program
- 基于拉普拉斯法的翼型生成程序,是生成NACA系列翼型的方便工具-Airfoil generation program to generate NACA series airfoil, based on Laplace s law ,which is a convenient tool.
Airfoil
- 采用excel编写了翼型升力系数、阻力系数及力矩系数的360°扩展程序-Using excel to prepare the airfoil lift coefficient, drag coefficient and torque coefficient 360 extension
VKT.airfoil
- 通过Karman-Trefftz 翼型的网格和计算方法，使用Fortran编写，粘性计算。-Through the grid and calculation methods Karman-Trefftz airfoil, written in Fortran, viscous calculations.
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
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
airfoil
- FORTRAN FILE AIRFOIL
AirFoil
- NASA翼型仿真器的汉化版，JAVA APPLET(NASA AIRFOIL SIMULATOR)
airfoil_generator
- Generates NACA 4 or 5 Digit Airfoil
sourse
- Airfoil CP Using Source Panel Method
vortex
- Airfoil CP Plot Using Vortex Method
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)