GrabCAD 模型信息
NACA 2412 3D Aerofoil · 模型 171190
NACA 2412 airfoil has a maximum camber of 2% located 40% (0.4 chords) from the leading edge with a maximum thickness of 12% of the chord.
- 格式
- CATIA
- 分类
- Aerospace、Aviation、Construction
- 标签
- 未标注
- 数据更新
- 2026-10-15T20:29:17Z
