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Axial Compressor for a single-shaft jet engine

Axial Compressor for a single-shaft jet engine

grabcad

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!

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