1. A design strategy for a 6:1 supersonic mixed-flow compressor stage and its viscous flow-based performance analysis 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 compressormean-line designturbomachinerycomputational fluid dynamicsshock stabilityaerospace propulsionBezier curvesNASA Rotor 37Supersonic Diffuser6:1pressure-ratioblade optimization File: Download MS_thesis_Aravinth_Sadagopan_May_2019.pdf Committee Members: Cengiz Camci, Thesis Advisor/Co-Advisor
