Numerical study on flow and heat transfer characteristics of swirling jet on a dimpled surface with effusion holes at turbine blade leading edge-Reference-Cited by-同舟云学术

Numerical study on flow and heat transfer characteristics of swirling jet on a dimpled surface with effusion holes at turbine blade leading edge

Published:2022-06 Issue: Volume:209 Page:118243
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Kong De-hai^ORCID,Zhang Chang-xian,Ma Zhen-yuan^ORCID,Liu Cun-liang,Isaev S.A.,Guo Tao,Xie Fan

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference48 articles.

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3. Study on analogy principle of overall cooling effectiveness for composite cooling structures with impingement and effusion;Liu;Int. J. Heat Mass Transf.,2018

4. Effects of impingement gap and hole arrangement on overall cooling effectiveness for impingement/effusion cooling;Xie;Int. J. Heat Mass Transf.,2020

5. An experimental evaluation of advanced leading edge impingement cooling concepts;Taslim;J. Turbomach.,2001

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