Endwall film cooling performance considering the effects of micro-riblets configurations and layouts-Reference-Cited by-同舟云学术

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Endwall film cooling performance considering the effects of micro-riblets configurations and layouts

Published:2024-09 Issue: Volume:108 Page:109440
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Du Kun,Pei Xiangpeng,Li Yuanyong,Liu Cunliang,Sunden Bengt^ORCID

Publisher

Elsevier BV

Reference38 articles.

1. Fan-shaped hole effects on the aero-thermal performance of a film cooled endwall;Barigozzi;ASME J. Turbomach.,2005

2. An experimental study of heat transfer and film cooling on large-scale turbine endwalls;Blair;ASME J. Heat Transfer.,1974

3. Cooling effectiveness and aerodynamic performance in a 2D-Contoured endwall passage with different mass flow ratios;Chen;Int. J. Therm. Sci.,2019

4. Turbine blade platform film cooling with fan-shaped holes under simulated swirl purge flow and slashface leakage conditions;Chen;ASME J. Turbomach.,2018

5. Turbine vane endwall film cooling with slashface leakage and discrete hole configuration;Chowdhury;ASME J. Turbomach.,2017

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation on the differences in unsteady film cooling behaviors of gas turbine blades between mainstream and cooling air pulsations for a cylindrical hole;International Journal of Heat and Fluid Flow;2024-10

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