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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