Numerical approach to film cooling effectiveness over a plate surface with coolant impingement
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-004-0011-x.pdf
Reference8 articles.
1. Camci, C, Arts, T. Experimental Heat Transfer Investigation Around the Film-Cooled Leading Edge of a High-Pressure Gas Turbine Rotor Blade. ASME Journal of Engineering for Gas Turbines and Power, 1985, 107: 1016–1021
2. Walker, L A, Markland, E. Heat Transfer to Turbine Blading in the Presence of Secondary Flow. International Journal of Heat and Mass Transfer, 1965, 8: 729–748
3. Walters, D K, Leylek, J H. A Detailed Analysis of Film-Cooling Physics: Part I-Streamwise Injection with Cylindrical Holes. ASME Journal of Turbomachinery, 2000, 122: 102–112
4. McGovern, K T, Leylek, J H. A Detailed Analysis of Film Cooling Physics: Part II-Compound-Angle Injection with Cylindrical Holes. ASME Journal of Turbomachinery, 2000, 122: 113–121
5. Hyams, D G, Leylek, J H. A Detailed Analysis of Film Cooling Physics: Part III-Streamwise Injection With Shaped Holes. ASME Journal of Turbomachinery, 2000, 122: 122–132
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