GrabCAD 模型信息
airfoil with 2 spars · 模型 309092
airfoil coordinates were given, skin thickness and number of spars and their thickness , as well as material selection were required. the spars are jutting out the aiefoil skin because of the offsetting of the spars in either direction. shell didn't work, and extrude cut would make variying the thickness of each of the elemnts hard. having different parts altogether for the spars and skin would've been very useful especially in material selection. but was impossible to mate in the assembly. if you have better ideas for modelling this please share. useful links:
- 格式
- SOLIDWORKS、Rendering、STEP / IGES
- 分类
- Aerospace、Aviation、Construction
- 标签
- airfoil、torque、thickness、spar、skin
- 数据更新
- 2026-09-10T12:34:23Z
