搜索资源列表
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
Euler
- 基于James格式的CFD程序,计算NACA0012翼型流场和升力阻力系数.网格由Fluent提供的Gmbit生成,计算结果可以通过Tecplot观看-James formats based on the CFD program to calculate the flow field and the NACA0012 airfoil lift drag coefficient. Fluent grid provided by the G
pablo
- 一个可以生成标准翼型坐标，并对翼型在不同攻角下进行升力系数及阻力系数计算的软件。-Can generate a standard airfoil coordinates, and the airfoil at different angle of attack carried out under the lift coefficient and drag coefficient calculation software.
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 e
Airfoil
- 实现B样条曲线画机翼，可输入自选参数得到不同展弦比，后掠角，上反角的机翼-B-spline curve to achieve painting wing, enter the optional parameters of different aspect ratio,后掠角, on the wing angle
EulerCode
- ROUTINES FOR GENERATION OF A C-TYPE GRID SYSTEM USE FOR FLOWS PAST AN AIRFOIL
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
javafoilinstaller
- Multi-Element Airfoil Sections program design
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
Potential_Flow_Simulator
- 翼型在势流中的模拟，以求得其压力系数分布，升力系数等-Airfoil in potential flow in the simulation, with a view to obtaining the pressure coefficient distribution, the lift coefficient
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
aiefoilconclution
- 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
airfoil
- 生成翼面网格，为流体计算做准备，Fortran编写简练合理-Wing surface grid is generated, in order to prepare for the calculation of fluid, Fortran to prepare concise and reasonable
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)
AirFoil_grid
- This Fortran Program develop for NACA0200 Airfoil Axi-symmetric grid generation. The grid is clustered in x. Program is basic level for under graduate students.
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
ausm-euler0012
- this fortran code can be used for analyse Inviscid flow over naca0012 airfoil with C_type grid. this code is developed by AUSM+ method.
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.
Airfoil-Design-and-Data
- Airfoil-Design-and-Data.pdf