Experimental Investigation on the Adiabatic Film Effectiveness for Counter-Inclined Simple and Laid-Back Film-Holes of Leading Edge
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-020-1287-1.pdf
Reference33 articles.
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3. Zhou J., Wang X., Li, J., Li, Y., Effects of film cooling hole locations on flow and heat transfer characteristics of impingement/effusion cooling at turbine blade leading edge. International Journal of Heat and Mass Transfer, 2018, 126: 192–205.
4. Zhou J., Wang X., Li, J., Influences of effusion hole diameter on impingement/effusion cooling performance at turbine blade leading edge. International Journal of Heat and Mass Transfer, 2019, 134: 1101–1118.
5. Bogard D.G., Thole K.A., Gas turbine cooling. Journal of Propulsion Power, 2006, 22: 249–270.
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