Optimization of crescent-shaped block downstream a row of cylindrical holes to enhance film cooling effectiveness
Author:
Funder
national natural foundation of china
natural science foundation of tianjin city
Publisher
Springer Science and Business Media LLC
Subject
Physical and Theoretical Chemistry,Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s10973-022-11346-z.pdf
Reference36 articles.
1. Bogard DG, Thole KA. Gas turbine film cooling. J Propul Power. 2012;22(2):314–9.
2. Goldstein RJ, Eckert ERG, Burggraf F. Effects of hole geometry and density on three-dimensional film cooling. Int J Heat Mass Transf. 1974;17(5):195–607.
3. Bunker RS. A review of shaped hole turbine film-cooling technology. J Heat Transf. 2005;127(4):441–53.
4. Na S, Shih TIP. Increasing adiabatic film-cooling effectiveness by using an upstream ramp. J Heat Transf. 2007;129(4):464–71.
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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