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Start Over Keyword Bezier curves Keyword mean-line design Keyword mixed-flow compressor Keyword pressure-ratio Keyword pressure-ratio Access Level open_access

1. A design strategy for a 6:1 supersonic mixed-flow compressor stage and its viscous flow-based performance analysis

open_access
Open Access
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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