## On the comparison of an axial flow compressor with one of constant tip Mach number |

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15 stage absolute velocities angular velocity approximation arithmetical means aspect ratio Axial Chord axial component axial compressor axial flow compressor axial velocity blade speed blading diagrams calculated channel shape compressor stage computed conical surface constant tip Mach Cornell University decrease density design radius diameter equivalent centrifugal compressor equivalent flow exit conditions given compression ratio guide vane entrance half vortex blading Hence high compression ratios hub radius hub/tip ratio last stage lift coefficient Mach number compressor Mamba 2 compressor mass flow number of blades number of stages number type compressor overall pressure ratio plot pressure rise Prom psia radii ratio per stage Reynolds number rim stress rotor blades rotor wheel School of Aeronautical small stage efficiency speed of sound stage Mamba static temperature stator blades tangent tensile stresses thru the compressor thru the stage tip blade velocity tip Mach number total temperature type of blading velocity diagrams viscosity