GrabCAD 模型信息
Compressor for jet engine · 模型 175706
3D model of 2 stage transsonic axial compressor Inlet diameter = 276mm; Number of stages- 2; Number of blades: R1-23, S1-37, R2-35, S2-53; Tip clearance in CFD analysis - 0.5 mm. DESIGN PARAMETERS (From CFD analysis): pressure ratio = 2.38; massflow = 7 kg/s; isentropic efficiency > 0.83; corrected spool speed = 29200 rpm.
- 格式
- STEP / IGES、Rendering、Parasolid
- 分类
- Aerospace、Aviation、Energy and Power
- 标签
- cfx、numeca、ansys、cfd、turbine、turbo、turbofan、aviation、aircraft、engine、jet、turbojet、blade、multustage、compressor
- 数据更新
- 2026-10-13T19:20:09Z
