Effect of shelf squealer tip configuration on aerothermal performance of gas turbine blade
Author:
Funder
Korea Institute of Energy Technology Evaluation and Planning
Publisher
Elsevier BV
Subject
General Engineering,Condensed Matter Physics
Reference33 articles.
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3. Heat transfer at the tip of an unshrouded turbine blade;Mayle;Heat Transfer,1982
4. Heat transfer in the tip region of grooved turbine blades;Chyu;J. Turbomach.,1989
5. Cavity heat transfer on a transverse grooved wall in a narrow flow channel;Metzger;J. Heat Tran.,1989
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