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-Reference-Cited by-同舟云学术

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

Published:2018-02 Issue: Volume:124 Page:146-161
ISSN:1290-0729
Container-title:International Journal of Thermal Sciences
language:en
Short-container-title:International Journal of Thermal Sciences

Author:

Li Weihong,Lu Xunfeng,Li Xueying,Ren Jing,Jiang Hongde

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

General Engineering,Condensed Matter Physics

Reference36 articles.

1. Turbine airfoil with multiple near wall compartment cooling;Liang,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 Transf,2017

5. Film-cooling effectiveness downstream of a single row of holes with variable density ratio;Sinha;ASME J Turbomach,1991

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