Effects of Ribbed-Cavity Tip on the Blade Tip Aerothermal Performance in a High Pressure Turbine Stage
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s11630-023-1771-5.pdf
Reference30 articles.
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5. Han J.C., Fundamental gas turbine heat transfer. Journal of Thermal Science and Engineering Applications, 2013, 5(2): 021007.
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1. Turbine blade tip aerothermal characteristics considering the influences of cavity tip shaping;International Journal of Thermal Sciences;2024-10
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