Effect of upstream slot leakage on turbine endwall film cooling characteristics
Author:
Funder
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
General Engineering,Condensed Matter Physics
Reference25 articles.
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3. The effects of varying the combustor-turbine gap;Cardwell;J. Turbomach.,2006
4. Adiabatic effectiveness measurements of endwall film cooling for a first stage vane;Knost;J. Turbomach.,2005
5. Measurements of net change in heat flux as a result of leakage and steps on the contoured endwall of a gas turbine first stage nozzle;Piggush;Appl. Therm. Eng.,2007
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