MAE 248

Advanced Turbomachinery

University of California Davis · UGRD · Fall 2026

1 section
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Course Description: Preliminary aerodynamic design of axial and radial flow compressors and turbines. Design of diffusers. Selection of turbomachine and configurations and approximations to optimum dimensions and flow angles. Introduction to through flow analysis. Rotating stall and surge, and aeromechanical considerations.

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Class #california_davis-6902Fall 2026UGRD4 credits
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