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Start Over Keyword pressure-ratio Keyword computational fluid dynamics Keyword Supersonic Diffuser Keyword turbomachinery Keyword NASA Rotor 37

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Author:: Sadagopan, Aravinth
Title:: A design strategy for a 6:1 supersonic mixed-flow compressor stage and its viscous flow-based performance analysis
Graduate Program:: Aerospace Engineering
Keywords:: mixed-flow compressor
mean-line design
turbomachinery
computational fluid dynamics
shock stability
aerospace propulsion
Bezier curves
NASA Rotor 37
Supersonic Diffuser
6:1
pressure-ratio
blade optimization
File:: Download MS_thesis_Aravinth_Sadagopan_May_2019.pdf
Committee Members:: Cengiz Camci, Thesis Advisor/Co-Advisor

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