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Compressor for jet engine

Compressor for jet engine

grabcad

3D model of 2 stage transsonic axial compressorInlet 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.

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