The effect of hot-streaks on HP vane surface and endwall heat transfer: An experimental and numerical study
Pronounced nonuniformities in combustor exit flow temperature (hot-streaks), which arise because of discrete injection of fuel and dilution air jets within the combustor and because of endwall cooling flows, affect both component life and aerodynamics. Because it is very difficult to quantitatively...
| Main Authors: | , , , , |
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| Format: | Conference item |
| Published: |
2005
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