GrabCAD 模型信息
NACA 0015 TAPED AIRFOIL · 模型 100655
These are files used for fluid simulation to determinate the lift and drag coefficients of the Airfoil NACA 0015. There is the NACA 0015 model and the Boundaries Model. The Boundary Model it is in distinct angles of attack, as 0º, 2º, 4º, 6º, 8º, 10º, 12º, 14º, 16º, 18º, 20º, 22º and 24º
- 格式
- Autodesk Inventor、STEP / IGES、AutoCAD
- 分类
- Aviation、Educational、Energy and Power
- 标签
- 0015、naca、fluent、ansys、airfoil
- 数据更新
- 2026-10-08T07:40:37Z
