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Title: Aero-thermal performance of transonic high-pressure turbine blade tips
Author: O'Dowd, Devin Owen
Awarding Body: University of Oxford
Current Institution: University of Oxford
Date of Award: 2010
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Supervisor: He, Li; Oldfield, M. L. G. Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID:  DOI: Not available
Keywords: Aerodynamics and heat transfer ; Aero engines ; Mathematical modeling (engineering) ; Turbomachinery hypersonics and aerodynamics ; High-Pressure Turbine ; Experimental ; High-Speed Linear Cascade ; Transonic Flow Conditions ; Cooled Winglet ; Tip Gap Survey ; Over-tip Leakage Flow ; Heat Transfer Measurement Techniques ; Infrared Thermography ; Spatially-resolved ; Heat Flux Reconstruction ; Impulse Technique ; Unshrouded Blade Tip Heat Transfer ; Film Cooling Effectiveness ; Net Heat Flux Reduction ; Aerodynamic Loss ; Three-hole Probe ; 2-D Corner Conduction ; Lateral Corner Correction Coefficient