GrabCAD 模型信息
Aircraft wing structure analyses and cfd model (AİRFOİL NACA 63012A) · 模型 236783
NACA 63012A AİRFOİL I type Spar CFD and Structure analyses model 2 spar (rear spar and front spar) 10 ribs 4,5 meters wing length 1.86 meters spar length
- 格式
- SOLIDWORKS、STEP / IGES、Rendering
- 分类
- Aerospace、Aviation、Tech
- 标签
- 未标注
- 数据更新
- 2026-10-30T09:40:22Z