Axial Compressor for a single-shaft jet engine
grabcad
The 3D model showcases the preliminary design of an axial compressor, exhibiting a pressure rise ratio of 6.52 and a high isentropic efficiency of 0.832. The corrected mass flow is 24.189 kg/sec at 15900 rpm. This compressor features subsonic 1st stage, with DCA and NACA 65 profiles utilized for stator vanes and rotor blades. All data provided are the result of hand calculations. If desired, I can share the project in IGES or other formats. Please feel free to provide your thoughts!
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