GrabCAD 模型信息
NACA 0012 Airfoil Wing · 模型 109654
This model represents a NACA 0012 symmetric airfoil wing, widely used in aerodynamic testing, RC aircraft, UAVs, and academic simulations. The NACA 0012 profile features a 12% thickness-to-chord ratio, making it ideal for analyzing lift, drag, and stall characteristics under various flow conditions. The geometry was created with precise NACA equations for accurate aerodynamic behavior and is suitable for CFD simulations, wind tunnel studies, or finite element analysis.
- 格式
- STEP / IGES、STL、Rendering、Fusion 360
- 分类
- 3D printing、Aerospace、Aviation
- 标签
- 3d printing、hobby、fusion 360、airfoil、aerospace、aviation、naca 0012 airfoil wing、naca 0012 airfoil、naca 0012、iges、stl
- 数据更新
- 2026-10-14T19:14:30Z
