Assessment of the effect of thermal barrier coating blockage on film cooling effectiveness: An experimental study of full-coverage turbine vane
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Published:2024-08
Issue:
Volume:53
Page:102702
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ISSN:2451-9049
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Container-title:Thermal Science and Engineering Progress
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language:en
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Short-container-title:Thermal Science and Engineering Progress
Author:
Yan Hao-nan,
Ye LinORCID,
Liu Cun-liang,
Li Bing-ran,
Zhang Li,
Huang Qi-he
Reference35 articles.
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3. D.G. Bogard, D.L. Schmidt, M. Tabbita, Characterization and Laboratory Simulation of Turbine Airfoil Surface Roughness and Associated Heat Transfer, In: Proceedings of ASME Turbo Expo 2015. GT-386. https://doi.org/10.1115/96-GT-386.
4. R. S. Bunker, Effect of Partial Coating Blockage on Film Cooling Effectiveness, In: Proceedings of the ASME Turbo Expo 2000. GT-0244. https://doi.org/10.1115/2000-GT-0244.
5. Effects of Surface Deposition, Hole Blockage, and Thermal Barrier Coating Spallation on Vane End-wall Film Cooling;Sundaram;J. Turbomach.,2007