Tip-leakage losses in subsonic and transonic blade rows
In this paper the effect of blade-exit Mach number on unshrouded turbine tip-leakage flows is investigated. Previously published experimental data of a high-pressure turbine blade are used to validate a computational fluid dynamics (CFD) code, which is then used to study the tip-leakage flow at blad...
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| Format: | Article |
| Language: | English |
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2012-10-30.
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| Online Access: | Get fulltext |