Comparisons on flow characteristics and film cooling performance of cylindrical and sister holes with/without internal coolant crossflow
Author:
Funder
National Natural Science Foundation of China
Higher Education Discipline Innovation Project
Publisher
Elsevier BV
Subject
General Engineering,Condensed Matter Physics
Reference31 articles.
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2. Flow structure and heat exchange analysis in internal cooling channel of gas turbine blade;Szwaba;J. Therm. Sci.,2016
3. Flow structure and heat transfer in a square passage with offset mid-truncated ribs;Xie;Int. J. Heat Mass Tran.,2014
4. Effect of film hole geometry and blowing ratio on film cooling performance;Cao;Appl. Therm. Eng.,2020
5. Numerical study on flow and heat transfer characteristics of jet array impingement cooling in turbine blade leading edge;Xi;J. Eng. Thermophys.,2021
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