搜索资源列表
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
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.
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
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
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
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
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
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.
Airfoil-Design-and-Data
- Airfoil-Design-and-Data.pdf