GrabCAD 模型信息
5th Stage Compressor Rotor Blade – Aerofoil Section · 模型 59393
This CAD model is based on the engineering drawing of a 5th Stage Compressor Rotor Blade and represents the aerofoil section with root geometry used in axial-flow compressors. The model follows the documented blade parameters such as chord length, leading and trailing edge radii, camber, stagger angles, and multiple sectional profiles along the blade height. It is intended for turbomachinery design study, CFD analysis, aerodynamic understanding, and CAD practice.
- 格式
- SOLIDWORKS
- 分类
- Aerospace、Industrial design、Machine design
- 标签
- solidworks、axial co、airfoil、aerofoil、compressor blade、turbine blade
- 数据更新
- 2026-10-07T09:54:08Z
