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task3
- 代码由FORTRAN开发，用于飞机设计中计算翼型绕流，求解椭圆方程-FORTRAN code from the development, design for aircraft airfoil flow calculation, solution of elliptic equations
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
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
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
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
FlutterBoundaryMapping
- 开发一个失败的边界映射算法和应用的翼型颤振模型，失败的边界测绘用MATLAB统计工具箱（集群）算法发展描述-Describes development of a failure boundary mapping algorithm and application to a Airfoil Flutter model
mesh-2d
- 生成三角形网格（对翼型）的程序，内附pdf说明手册-Generated triangle mesh (right wing) of the program, enclosing the pdf instruction manual
F15E
- F15E的3D图，能够直观反映该机型的外形特征及翼型布局，对研究该机型的气动外形及辐射特征有一定的参考价值-F15E, 3D map, be able to intuitively reflect the characteristics and airfoil shape model layout of the study of the aircraft' s aerodynamic shape and radiation characteristics of a certain refe
Aerodynamics
- 本课程是航空航天类院校本科飞行器设计与工程专业教学计划中的一门技术基础课。为飞行器设计与工程专业学生的必修课。本课程的目的和任务是使学生掌握流体力学基本知识和空气动力学的基本概念、基本理论，以及解决空气动力学问题的基本方法和分析手段。本课程的内容可分为两大部分：低速空气动力学和可压缩空气动力学，包括了空气动力学的基本概念、低速流动和可压缩无粘流动的基本原理、绕翼型和机翼的不可压缩流动的薄翼理论和有限翼理论、激波理论、翼型亚音速和超音速线化理论及应用等。-This course is a clas
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)
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
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.
toolbox
- 这是自己编写的MATLAB的基于神经网络和遗传算法的翼型优化程序。有需要的可以下载，完全是自己编写的。 -matlab wing optimization
2dairfoil
- 二维翼型网格生成 的 fortran程序 非常经典 易于学习 -fortram program
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
- 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
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
2321
- 涡流发生器布局方式对翼型失速流动控制效果影响的实验研究.-Layout of the wing vortex generator flow control stall effects in rats.
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.
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