搜索资源列表
naca0012
- NACA0012翼型流场计算。结构化网格，AUSM格式。-NACA0012 airfoil flow field
naca4gen
- NACA 4位数 翼型数据的生成 Matlab程序-NACA 4 digit airfoil
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.
Drag-Coefficient
- list of lift coefficeint and drag coefficient for naca 0012 at different reynolds No.
NACA0012_Validation_Laminar
- validation paper for Laminar viscous Compressible flow, Over Naca 0012- validation paper for Laminar viscous Compressible flow, Over Naca 0012
naca-0012-drag-prediction
- Drag prediction for Naca 0012 by use of different source codes and Compare with Experiment results.
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.
oblique
- Interactive oblique shock calculator for a double wedge. References: John, J.E.A., "Gas Dynamics," 2nd Edition, 1984: pp 123-134. Ames Research Staff, "Equations, Tables, and Charts for Compresssible Flow," NACA Report 1135, pp 8-12. -Intera
naca456
- GENERATE NACA 4,5,6 SERIES AIRFOIL COORDINATES. PROGRAM WRITTEN IN FORTRAN
AirFoil
- NASA翼型仿真器的汉化版，JAVA APPLET(NASA AIRFOIL SIMULATOR)
NACA_profile_generator_Matlab
- 计算 NACA 系列翼型坐标，已进行 CFD 仿真。(Calculate the coordinates of NACA wings.)