Theses most similar to Performance limits of axial turbomachine stages (Hall, David Kenneth; 2011) read it
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- Department of Aeronautics and Astronautics
- Advisors: Drela, Mark; Wesley Harris
- Department of Aeronautics and Astronautics
- Advisor: Alan H. Epstein
- Department of Aeronautics and Astronautics
Aircraft engine performance improvements using multistage compressors with actively controlled stall lines
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- Department of Mechanical Engineering
Characterization and design of non-adiabatic micro-compressor impeller and preliminary design of self-sustained micro engine system
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The impact of evaporatively cooled turbine blades on gas turbine performance
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- Department of Aeronautics and Astronautics
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- Department of Aeronautics and Astronautics
Multi-parameter control for centrifugal compressor performance optimization
Mannai, Sébastien (Sébastien Karim) (2014)
- Advisor: Choon Sooi Tan
- Department of Aeronautics and Astronautics
- Advisor: Edward M. Greitzer
- Department of Aeronautics and Astronautics
Characterization of performance-limiting flow mechanisms in a centrifugal compressor stage
Erickson, David W. (2017)
- Advisors: Choon S. Tany; Michael Macrorie
- Department of Aeronautics and Astronautics