Investigations on Performance of Crater Film Cooling with Different Film Hole Configurations at Compound Angles
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-1308-4_13
Reference11 articles.
1. Bunker RS (2005) A review of shaped hole turbine film hole technology. ASME J Heat Transf 127:441–453
2. Lu Y, Ekkad SV (2006) Film cooling for cratered cylindrical inclined holes. In: Proceedings of international mechanical engineering congress and exposition, Illinois, USA, IMECE2006–14406
3. Kim J, Kim K (2016) Surrogate based optimization of a cratered cylindrical hole to enhance film cooling effectiveness. J Therm Sci Technol 11(2):1–14
4. Tran NT, Nguyen CQ, Ho SH, Kapat JS (2010) Prediction of adiabatic effectiveness of various cratered film hole configurations: sensitivity analysis for rectangular shaped mask. In: AIAA aerospace science meeting, Florida, AIAA 2010-404
5. Kalghatgi P, Acharya S (2015) Improved film cooling effectiveness with a round film cooling hole embedded in a contoured crater. ASME J Turbomach 137:101006-1-10
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