Numerical investigation on flow and heat transfer characteristics of impingement/swirl cooling structures in a turbine blade leading edge-Reference-Cited by-同舟云学术

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Numerical investigation on flow and heat transfer characteristics of impingement/swirl cooling structures in a turbine blade leading edge

Published:2024-09 Issue: Volume:108 Page:109474
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:

Han Feng^ORCID,Wang Lingyang,Song Yi,Mao Junkui

Publisher

Elsevier BV

Reference39 articles.

1. ANSYS FLUENT 2020 Help Document, ANSYS Inc., 2020.

2. Flow and heat transfer measurements in swirl tubes with one and multiple tangential inlet jets for internal gas turbine blade cooling;Biegger;Int. J. Heat Fluid Flow,2018

3. Considerations for the design of swirl chambers for the cyclone cooling of turbine blades and for other applications with high swirl intensity;Bruschewski;Int. J. Heat Fluid Flow,2020

4. Pareto optimal design of swirl cooling chambers with tangential injection using CFD, GMDH-type of ANN and NSGA-II algorithm;Damavandi;Int. J. Therm. Sci.,2017

5. Flow and heat transfer in a rotating channel with impingement cooling and film extraction;Deng;Int. J. Heat Mass Transf.,2021

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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