Author:
Li Weihong,Li Xueying,Ren Jing,Jiang Hongde
Funder
National Natural Science Foundation of China
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference38 articles.
1. G. Liang, Turbine airfoil with multiple near wall compartment cooling, U.S. Patent 7,556,476 B1, 2009.
2. Effect of Reynolds number, hole patterns and hole inclination on cooling performance of an impinging jet array: Part I—convective heat transfer results and optimization;Li;ASME J. Turbomach.,2016
3. Effect of Reynolds number, hole patterns, target plate thickness on cooling performance of an impinging jet array: Part II—conjugate heat transfer results and optimization;Li;ASME J. Turbomach.,2016
4. Experimental investigation of local and average heat transfer coefficients under an inline impinging jet array, including jets with low impingement distance and inclined angle;Li;ASME J. Heat Transfer,2017
5. High resolution measurements of film cooling performance of simple and compound angle cylindrical holes with varying hole length-to-diameter ratio—Part I: Adiabatic film effectiveness;Li;Int. J. Therm. Sci.,2018
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