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[Mathimatics-Numerical algorithms] NACA DL : 0: 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
Update : 2008-10-13 Size : 1.04kb Publisher : 浩南
[Mathimatics-Numerical algorithms] NACA DL : 0: 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
Update : 2025-02-17 Size : 1kb Publisher : 浩南
[Other] Euler DL : 0: 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
Update : 2025-02-17 Size : 856kb Publisher : 凌维安
[Linux-Unix] PanelCode DL : 0: The source code for the program is offered under the GNU General Public License. Please feel free to download the code, read it, modify it, compile it and run it locally. -Parameter definitions: use_naca: logical, true if we want to generate a NACA 4/5 digit airfoil internally, false if we should read the coordinates from the UIUC database. naca: integer NACA 4/5 digit number. Note, no error checking is performed here to see if it s a valid number. that s done by the perl-script that executes this code, so make sure you give it a valid number. airfoil: string, name of the database airfoil to read, including the relative path-name. smoothing: logical, true if you want to smooth the surface points that you read from a file. Note, smoothing will alter the airfoil data, however, unsmoothed data may result in ripples in the pressure. npanels: integer number of panels for the simulations. If you want to use more than 200, increase the value of ndim in the common.inc file
Update : 2025-02-17 Size : 77kb Publisher : XJ
[AI-NN-PR] NACA DL : 0: 小生境蚁群算法例子，对学习蚁群算法及很好的理解该算法非常有用-Niche ant colony algorithm is an example of learning ant colony algorithm and a good understanding of the algorithm is very useful! ! !
Update : 2025-02-17 Size : 1kb Publisher : 何志军
[matlab] FourSeriesairfoil DL : 0: naca翼型坐标生成程序（Ｍａｔｌａｂ）-naca airfoil coordinates generating program (Matlab)
Update : 2025-02-17 Size : 1kb Publisher : 程远
[transportation applications] naca DL : 0: 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
Update : 2025-02-17 Size : 154kb Publisher : shi xiaotian
[Algorithm] naca4gen DL : 0: NACA 4位数翼型数据的生成 Matlab程序-NACA 4 digit airfoil
Update : 2025-02-17 Size : 2kb Publisher : Big Boss
[Algorithm] naca0012 DL : 0: NACA0012翼型流场计算。结构化网格，AUSM格式。-NACA0012 airfoil flow field
Update : 2025-02-17 Size : 584kb Publisher : newanda
[Algorithm] C-type-gridgeneration-for-naca0012 DL : 1: 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.
Update : 2025-02-17 Size : 3kb Publisher : kiarash
[Algorithm] Drag-Coefficient DL : 0: list of lift coefficeint and drag coefficient for naca 0012 at different reynolds No.
Update : 2025-02-17 Size : 15kb Publisher : kiarash
[Algorithm] NACA0012_Validation_Laminar DL : 0: validation paper for Laminar viscous Compressible flow, Over Naca 0012- validation paper for Laminar viscous Compressible flow, Over Naca 0012
Update : 2025-02-17 Size : 779kb Publisher : kiarash
[Algorithm] naca-0012-drag-prediction DL : 0: Drag prediction for Naca 0012 by use of different source codes and Compare with Experiment results.
Update : 2025-02-17 Size : 715kb Publisher : kiarash
[Algorithm] NACA-series-airfoil-program DL : 0: 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.
Update : 2025-02-17 Size : 123kb Publisher : 杜雁霞
[Software Engineering] The-NACA-airfoil-series DL : 0: NACA Airfoil 4 Series, 5 Series, 6 Series,-NACA Airfoil 4 Series, 5 Series, 6 Series,...
Update : 2025-02-17 Size : 267kb Publisher : Dat Tien Hoang
[transportation applications] naca-airfoil DL : 0: 生成NACA翼型的vb程序，输入4位数naca翼型，得到翼型剖面。-NACA airfoil generates vb program, enter the 4-digit naca airfoil, get airfoil sections.
Update : 2025-02-17 Size : 36kb Publisher : hukaiye
[Algorithm] NACA_profile_generator_Matlab DL : 0: 计算 NACA 系列翼型坐标，已进行 CFD 仿真。(Calculate the coordinates of NACA wings.)
Update : 2025-02-17 Size : 87kb Publisher : Allenlightman
[transportation applications] Vortex2D DL : 0: 输入naca四位数翼型，和环境参数，可以计算得到压力分布和升力系数(Pressure distribution and lift coefficient can be calculated by inputting NACA four-digit airfoil and environmental parameters.)
Update : 2025-02-17 Size : 23kb Publisher : zhanghaot
[Windows Develop] airfoil_profile DL : 0: 使用matlab编程，该代码用于绘制五位数NACA翼型，(Drawing Five-digit NACA Airfoils)
Update : 2025-02-17 Size : 1kb Publisher : Carry~c
[Other] NACA DL : 0: NACA翼型坐标生成文件，可根据输入NACA四位数字，生成NACA坐标(NACA airfoil coordinate generation file, which can generate NACA coordinates based on input NACA four digits)
Update : 2025-02-17 Size : 27kb Publisher : TGZZ

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