Coupled effects of typical thermodynamic parameters on the flow and heat transfer in a high-pressure turbine outer ring with impingement-film composite cooling structure-Reference-Cited by-同舟云学术

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Coupled effects of typical thermodynamic parameters on the flow and heat transfer in a high-pressure turbine outer ring with impingement-film composite cooling structure

Published:2024-10 Issue: Volume:204 Page:109243
ISSN:1290-0729
Container-title:International Journal of Thermal Sciences
language:en
Short-container-title:International Journal of Thermal Sciences

Author:

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

Publisher

Elsevier BV

Reference28 articles.

1. Future Aero Engine Designs: an Evolving vision[J];Kyprianidis,2011

2. Review of Platform Cooling technology for high pressure turbine blades[C];Wright,2014

3. Flow visualization in a linear turbine cascade of high performance turbine blades;Wang;J. Turbomach.,1997

4. Experimental decoupled-analysis of overall cooling effectiveness for a turbine endwall with internal and external cooling configurations;Wu;Appl. Therm. Eng.,2023

5. Experimental investigation of endwall heat transfer with film and impingement cooling;Li;J. Eng. Gas Turbines Power,2017

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