Experimental simulations of effects of surface roughness level of TBC on overall effectiveness of film cooling under typical vane environment
Author:
Publisher
Springer Science and Business Media LLC
Subject
Physical and Theoretical Chemistry,Condensed Matter Physics,Polymers and Plastics,Materials Chemistry
Link
https://link.springer.com/content/pdf/10.1007/s10973-023-12409-5.pdf
Reference36 articles.
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3. Wang F, Pu J, Wang J, Xia W. Numerical investigation of effects of blockage, inclination angle and hole-size on film cooling effectiveness at concave surface. J Turbomach. 2021;143: 021007.
4. Colón S, Ricklick M, Nagy D, Lafleur A. Geometric Effects of thermal barrier coating damage on turbine blade temperatures. In: Proceedings of ASME turbo expo. 2019; GT2019-90886.
5. Krishna Anand VG, Parammasivam KM. Thermal barrier coated surface modifications for gas turbine film cooling: a review. J Therm Anal Calorim. 2021;146(2):545–80.
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