Aero-thermal performance of transonic high-pressure turbine blade tips
<p>This thesis presents an experimental and theoretical study of unshrouded tips on gas turbine blades with and without winglets. The goal of the winglet tip design is to reduce over-tip leakage flow. To assess the potential use of winglets, their effectiveness in reducing loss and the cooling...
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Format: | Thesis |
Language: | English |
Published: |
2010
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