Aero-thermal performance and enhanced internal cooling of unshrouded turbine blade tips
<p>The tips of unshrouded, high-pressure turbine blades are prone to significantly high heat loads. The gap between the tip and over-tip casing is the root cause of undesirable over-tip leakage flow that is directly responsible for high thermal material degradation and is a major source of...
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| Format: | Thesis |
| Language: | English |
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2015
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