ME 564 - Aerodynamic Design of Turbines and Compressors

3 credit(s)
Thermodynamic and aerodynamic theory applied to the design of turbomachinery. Gas turbine system analysis, centrifugal compressors, axial flow compressors, axial and radial flow turbines, compressor and turbine matching.
Prerequisite(s): Either ME 422 or ME 532.

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