Effect of injection angle on film cooling characteristics and loss mechanism of contracted double-jet hole in a flat plate
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference31 articles.
1. Influence of hole geometry on film cooling effectiveness for a constant exit flow area;Sun;Appl. Therm. Eng.,2017
2. Experimental investigation of film cooling from compound angle holes supplemented by secondary holes;Abdelmohimen;Int. J. Heat Mass Tran.,2019
3. Comparisons on flow characteristics and film cooling performance of cylindrical and sister holes with/without internal coolant crossflow;Zhu;Int. J. Therm. Sci.,2022
4. Comparisons of cooling performance and flow characteristics of a combustor liner plate with compound angle and simple angle effusion holes;Kwon;Int. J. Therm. Sci.,2023
5. Numerical analysis of cooling efficiency for turboshaft engines with converging-diverging film cooling holes;Wang;Int. J. Therm. Sci.,2023
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