Heat Transfer and Flow Structure of a Turbine Blade’s Air-cooled Leading Edge Considering Different Hole Shapes and Additional Flow Angles
Author:
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s11630-024-1958-4.pdf
Reference52 articles.
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4. Liu C-l., Zhu H-r., Zhang Z-w., Xu D-c., Experimental investigation on the leading edge film cooling of cylindrical and laid-back holes with different hole pitches. International Journal of Heat and Mass Transfer, 2012, 55(23–24): 6832–6845.
5. Monge-Concepción I., Siroka S., Berdanier RA., Barringer M.D., Thole KA., Robak C., Influence of Vane trailing edge flow on the formation of cavity cells and rim sealing. Journal of Turbomachinery, 2022, 144(6): 061014.
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