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
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.