Influence mechanism of impingement and film on the flow and heat transfer of turbine outer ring with composite cooling structure under different operating parameters-Reference-Cited by-同舟云学术

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Influence mechanism of impingement and film on the flow and heat transfer of turbine outer ring with composite cooling structure under different operating parameters

Published:2024-06 Issue: Volume:246 Page:122883
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Wang Longfei,Lv Chengliang,Mao Junkui^ORCID,Li Ziqiang,Zhang Dewei,Bi Shuai

Publisher

Elsevier BV

Reference33 articles.

1. Future aero engine designs: an evolving vision;Kyprianidis;INTECH,2011

2. Gas turbine film cooling;Bogard;J. Propul. Power,2012

3. P. Brocq, B. Launder, C. Priddin, Discrete hole injection as a means of transpiration cooling; an experimental study, Archive Proceedings of the Institution of Mechanical Engineers. 187 (1973) 149-157.

4. A review of shaped hole turbine film-cooling technology;Bunker;Journal of Heat Transfer Transactions of the ASME.,2005

5. Investigation on film cooling characteristics from a row of converging slot-holes on flat plate;Yao;Sci. China Technol. Sci.,2011

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. Characterization of loss, temperature, and stress on partial admission axial impulse turbines with liquid jet impingement cooling;Applied Thermal Engineering;2024-09

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