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
2. Conceptual development of casing Patterns to reduce the aerodynamic losses in an axial turbine stage Open Access Author: Ranka, Amrat Arvind Title: Conceptual development of casing Patterns to reduce the aerodynamic losses in an axial turbine stage Graduate Program: Aerospace Engineering Keywords: Turbinesaxial gas turbinecasing groovescomputational fluid dynamicsCFDTip-Leakage lossesTip-mitigation studiesTurbomachineryAFTRFleakage VortexHorseshoe Vortex File: Download Final_thesis.pdf Committee Members: Cengiz Camci, Thesis Advisor/Co-AdvisorDr. Sven Schmitz, Committee MemberAmy Ruth Pritchett, Program Head/Chair
