Effect of hole configurations on film cooling performance
Author:
Affiliation:
1. School of Energy and Environmental Engineering, Hebei University of Technology, Tianjin, P.R. China;
2. Division of Heat Transfer, Department of Energy Sciences, Lund University, Lund, Sweden
Funder
National Natural Science Foundation of China
Publisher
Informa UK Limited
Subject
Condensed Matter Physics,Numerical Analysis
Link
https://tandfonline.com/doi/pdf/10.1080/10407782.2019.1608762
Reference22 articles.
1. Evolution of Ni-based superalloys for single crystal gas turbine blade applications
2. Large eddy simulation for predicting turbulent heat transfer in gas turbines
3. Recent Development in Turbine Blade Film Cooling
4. Gas Turbine Blade Tip Heat Transfer and Cooling: A Literature Survey
5. Effect of coolant–mainstream blowing ratio on leading edge film cooling flow and heat transfer – LES investigation
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