Theses most similar to An improved blade passage model for estimating off-design axial compressor performance (Brand, Maximilian Lewis; 2013) read it
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- Department of Aeronautics and Astronautics
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- Department of Mechanical Engineering
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- Department of Aeronautics and Astronautics
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- Advisor: Choon Sooi Tan
- Department of Aeronautics and Astronautics
Impact of tip clearance flow on centrifugal pump impeller performance
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- Advisors: Choon S. Tany; Edward M. Greitzer
- Department of Aeronautics and Astronautics
An assessment of computational procedures for eleven-stage compressor response to inlet distortion
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- Advisors: Choon S. Tany; Yifang Gon
- Department of Aeronautics and Astronautics
Impeller loss reduction in multi-stage centrifugal compressors
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- Advisor: Edward M. Greitzer
- Department of Aeronautics and Astronautics
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- Department of Aeronautics and Astronautics
Tip clearance effects on multistage axial compressor performance and flow structure for small core application
Koff, Andrew (Andrew Steven) (2017)
- Advisors: Choon S. Tany; Edward M. Greitzer
- Department of Aeronautics and Astronautics