Thermal and aerodynamic investigation of innovative cooling designs of blade tips
<p>The blade tip is a particularly critical part of high-pressure turbine blades, as the hot gas leaking over it causes a loss of efficiency and degrades the blade. This tip degradation is often a limiting factor of engine life. For squealer designs, the pressure side rim near the trailing edg...
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| Format: | Thesis |
| Language: | English |
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2022
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