1. HEAT TRANSFER TO SPORES IN AN ABRUPTLY EXPANDING AXISYMMETRIC FLOW FIELD COMPUTED USING CFD Open Access Author: Saurav, Samarth Title: HEAT TRANSFER TO SPORES IN AN ABRUPTLY EXPANDING AXISYMMETRIC FLOW FIELD COMPUTED USING CFD Graduate Program: Aerospace Engineering Keywords: abruptly expanding internal flowscomputational fluid dynamicsheat transfer File: Download Samarth_MS_thesis.pdf Committee Members: Dr Deborah Levin, Thesis Advisor/Co-AdvisorDr Deborah Levin, Thesis Advisor/Co-Advisor
2. Simulations of the flow generated by fluidic inserts in a converging diverging nozzle Open Access Author: Lampenfield, Jacob John Title: Simulations of the flow generated by fluidic inserts in a converging diverging nozzle Graduate Program: Aerospace Engineering Keywords: CFDcomputational fluid dynamicsconvergingdivergingnozzleaeroacousticsnoise reduction File: Download Lampenfield_MS_Final.pdf Committee Members: Philip John Morris, Thesis Advisor/Co-Advisor
3. Utilizing Transitional CFD to Analyze the Performance of a Racing Sailplane Open Access Author: Axten, Christopher Joseph Title: Utilizing Transitional CFD to Analyze the Performance of a Racing Sailplane Graduate Program: Aerospace Engineering Keywords: computational fluid dynamicssailplaneboundary layer transitionaircraft performanceaircraft design File: Download Axten_C_Master_Thesis_Draft_Final.pdf Committee Members: Mark David Maughmer, Thesis Advisor/Co-AdvisorSven Schmitz, Committee MemberAmy Ruth Pritchett, Program Head/Chair
4. 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
5. 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
