Multi-objective optimization of transpiration cooling for high pressure turbine vane-Reference-Cited by-同舟云学术

Multi-objective optimization of transpiration cooling for high pressure turbine vane

Published:2024-06 Issue: Volume:246 Page:122926
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Wang Wen,Tao Guocheng,Ke Dandan,Ruan Zhigang,Liu Jian,Luo Jiaqi,Cui Jiahuan^ORCID

Funder

NSFC

Publisher

Elsevier BV

Reference59 articles.

1. Review of advanced effusive cooling for gas turbine blades;Wang;Energies,2022

2. Computational optimization of the internal cooling passages of a guide vane by a gradient-based algorithm;Xie;Numerical Heat Transfer, Part a: Applications,2016

3. Turbine blade cooling passages optimization using reduced conjugate heat transfer methodology;Mazaheri;Appl. Therm. Eng.,2016

4. Probabilistic CFD computations of gas turbine vane under uncertain operational conditions;Karimi;Appl. Therm. Eng.,2019

5. Large-eddy simulation of film cooling performance enhancement using vortex generator and semi-sphere;Wang;Proceedings of the ASME Turbo Expo 2020,2020

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