Theses most similar to Inlet swirl distortion effects on the generation and propagation of fan rotor shock noise (Defoe, Jeff (Jeffrey James); 2011) read it
- Advisor: Jack L. Kerrebrock
- Department of Aeronautics and Astronautics
Influence of Reynolds number and blade geometry on low pressure turbine performance
Bury, Mark Eric (1997)
- Advisor: Choon S. Tany
- Department of Aeronautics and Astronautics
- Advisor: Drela, Mark
- Department of Aeronautics and Astronautics
- Advisor: Choon S. Tany
- Department of Aeronautics and Astronautics
Development of an effective computational methodology for multi-stage compressor map generation
Choi, Taek Jin, 1974- (2001)
- Advisor: Choon Sooi Tan
- Department of Aeronautics and Astronautics
- Advisor: Spakovszky, Zoltán S. (Zoltán Sándor), 1972-
- Department of Aeronautics and Astronautics
An improved blade passage model for estimating off-design axial compressor performance
Brand, Maximilian Lewis (2013)
- Advisor: Spakovszky, Zoltán S. (Zoltán Sándor), 1972-
- Department of Aeronautics and Astronautics
- Advisor: Edward M. Greitzer
- Department of Aeronautics and Astronautics
Two investigations of compressor stability : spike stall inception and transient heat transfer effects
Kiss, Andras Laszlo Andor (2015)
- Advisor: Spakovszky, Zoltán S. (Zoltán Sándor), 1972-
- Department of Aeronautics and Astronautics
- Advisors: Edward M. Greitzer; Steven G. Gegg
- Department of Aeronautics and Astronautics