Tip gap size effects on thermal performance of cavity-winglet tips in transonic turbine cascade with endwall motion
The thermal performance of two cavity-winglet tips with endwall motion is investigated in a transonic high pressure turbine cascade, which operates at an engine representative exit Mach number of 1.2 and an exit Reynolds number of 1.7 × 106. The numerical method is first validated with experimental...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
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Global Power and Propulsion Society
2017-06-01
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| Series: | Journal of the Global Power and Propulsion Society |
| Subjects: | |
| Online Access: | https://www.gppsjournal.org/journals/journal-of-the-global-power-and-propulsion-society/thermal-performance-of-cavity-winglet-tips/ |