Effect of leakage flow on the endwall cooling performance in high subsonic turbine cascade
Author:
Funder
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
General Engineering,Condensed Matter Physics
Reference28 articles.
1. Adiabatic effectiveness measurements of endwall film-cooling for a first-stage vane;Knost;J. Turbomach.,2005
2. The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane;Lynch;J. Turbomach.,2008
3. The effects of varying the combustor-turbine gap;Cardwell;J. Turbomach.,2007
4. The interaction of turbine inter-platform leakage flow with the mainstream flow;Reid;J. Turbomach.,2007
5. Experimental investigation of turbine leakage flows on the three-dimensional flow field and endwall heat transfer;Rehder;J. Turbomach.,2007
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