Research on the effect of the swirling coolant within endwall passage on film cooling/heat transfer and aerodynamic losses-Reference-Cited by-同舟云学术

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Research on the effect of the swirling coolant within endwall passage on film cooling/heat transfer and aerodynamic losses

Published:2021-11 Issue: Volume:128 Page:105585
ISSN:0735-1933
Container-title:International Communications in Heat and Mass Transfer
language:en
Short-container-title:International Communications in Heat and Mass Transfer

Author:

Hu Ji,Zheng Qun,Dong Ping,Li Zhaolin,Yue Guoqiang

Funder

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics

Reference31 articles.

1. High free-steam turbulence effects on endwall heat transfer for a gas turbine stator vane;Radomsky;J. Turbomach.,2000

2. Turbine endwall aerodynamics and heat transfer;Simon;J. Propuls. Power,2006

3. The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane;Lynch;J. Turbomach.,2008

4. Experimental investigation of heat transfer characteristics on turbine endwall with full coverage film cooling;Liu;Appl. Therm. Eng.,2018

5. Study of secondary flow and coolant film interaction in a high subsonic cascade;Mahadevan;Int. J. Heat Fluid Flow,2016

Cited by 9 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. Research progress of mixing loss model for film cooling on turbine blade;International Journal of Heat and Fluid Flow;2024-12

2. Effects of rim seal exit geometry on the cooling characteristics of turbine endwall and blade suction side;Thermal Science and Engineering Progress;2024-09

3. Numerical simulation of composite swirl/film double-wall cooling structures and chamber designs for enhanced overall cooling effectiveness;International Journal of Heat and Mass Transfer;2024-08

4. Effects of vortex generators on endwall film cooling in a turbine vane;International Communications in Heat and Mass Transfer;2024-04

5. Aerothermal characteristics evaluation for different tip configurations without and with film cooling on transonic turbine;International Communications in Heat and Mass Transfer;2024-04

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