Numerical study of the film cooling effectiveness and flow loss of a shark-skin-inspired composite structure-Reference-Cited by-同舟云学术

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Numerical study of the film cooling effectiveness and flow loss of a shark-skin-inspired composite structure

Published:2024-10 Issue: Volume:204 Page:109248
ISSN:1290-0729
Container-title:International Journal of Thermal Sciences
language:en
Short-container-title:International Journal of Thermal Sciences

Author:

Zhang Runsheng^ORCID,Xiang Zhen,Han Shaohua,Huang Xin,Zhou Leping^ORCID,Li Li,Zhang Hui,Du Xiaoze

Publisher

Elsevier BV

Reference35 articles.

1. Impact of thermal radiation on turbine blades with film cooling structures;Li;Appl. Therm. Eng.,2023

2. Thermal barrier coated surface modifications for gas turbine film cooling: a review;Krishna Anand;J. Therm. Anal. Calorim.,2021

3. Experimental study of combined influences of wall curvature and compound angle on film cooling effectiveness of a fan-shaped film-hole;Pu;Int. Commun. Heat Mass Tran.,2022

4. Investigation on overall performance of double-jet film cooling holes with various spanwise distance;He;Int. J. Therm. Sci.,2023

5. Experimental and numerical investigations of the NEKOMIMI film cooling technology;Kusterer,2012

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