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Description: 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
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Size: 117760 |
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Description: 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 Gmbit generated, calculated results can Tecplot Views
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Size: 876544 |
Author: 凌维安 |
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Description: 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.
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Size: 72704 |
Author: 陆群峰 |
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Description: 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 of easy-to-read
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Size: 460800 |
Author: 袁振伟 |
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Description: 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
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Size: 6144 |
Author: 王宏伟 |
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Description: ROUTINES FOR GENERATION OF A C-TYPE GRID SYSTEM USE FOR FLOWS PAST AN AIRFOIL
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Size: 429056 |
Author: Nha |
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Description: 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
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Size: 3072 |
Author: 杨晓泉 |
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Description: Multi-Element Airfoil Sections program design
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Size: 574464 |
Author: NENO |
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Description: 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
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Size: 2048 |
Author: wangwei |
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Description: 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
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Size: 4660224 |
Author: 黄晓青 |
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Description: 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
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Size: 366592 |
Author: 大波 |
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Description: 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
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Size: 305152 |
Author: 大波 |
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Description: 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
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Size: 3072 |
Author: ywc |
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Description: 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.
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Size: 3072 |
Author: 程鹏 |
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Description: 采用贴体坐标转换实现翼型网格生成，其C/C++程序在.RAR中-Airfoil grid generation ，Its C/C++ program include the file .rar
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Size: 1024 |
Author: 吴俊 |
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Description: 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)
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Size: 12288 |
Author: 云清风 |
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Description: 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.
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Size: 2048 |
Author: Irfan |
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Description: 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
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Size: 3072 |
Author: 程熠 |
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Description: this fortran code can be used for analyse Inviscid flow over naca0012 airfoil with C_type grid. this code is developed by AUSM+ method.
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Size: 3072 |
Author: kiarash |
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Description: Airfoil-Design-and-Data.pdf
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Size: 9869312 |
Author: lighkning |
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