GrabCAD 模型信息
Axial Compressor for a single-shaft jet engine · 模型 231071
3D model based on preliminary design of axial compressor: Pressure rise ratio: 6.52 izentropic efficiency: 0.832 mass flow(corrected): 24.189 kg/sec 15900rpm 1st stage-subsonic DCA and NACA 65 profiles used for stator vanes and rotor blades all data based on hand calculations If You wish I will upload project as an Iges or other formats Feel free to comment!
- 格式
- CATIA、CATIA、Rendering
- 分类
- Aerospace、Aviation
- 标签
- disc、blade、pressure、blades、compressor、discs、axial
- 数据更新
- 2026-10-24T21:55:04Z
