Stress analysis of the thermal barrier coating system near a cooling hole considering the free-edge effect-Reference-Cited by-同舟云学术

Stress analysis of the thermal barrier coating system near a cooling hole considering the free-edge effect

Published:2020-01 Issue:1 Volume:46 Page:331-342
ISSN:0272-8842
Container-title:Ceramics International
language:en
Short-container-title:Ceramics International

Author:

Jiang Jishen,Ma Xianfeng,Wang Biao

Funder

China Postdoctoral Science Foundation

Guangdong Education Department Fund

Guangdong Provincial key S&T Special Project

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Materials Chemistry,Surfaces, Coatings and Films,Process Chemistry and Technology,Ceramics and Composites,Electronic, Optical and Magnetic Materials

Reference24 articles.

1. Thermal barrier coatings for gas-turbine engine applications;Padture;Science,2002

2. Thermal-barrier coatings for more efficient gas-turbine engines;Clarke;MRS Bull.,2012

3. Influence of material properties on temperature and thermal stress of thermal barrier coating near a normal cooling hole;Kim;Int. J. Heat Mass Transf.,2011

4. Numerical stress analysis of the TBC-film cooling system under operating conditions considering the effects of thermal gradient and TGO growth;Jiang;Surf. Coat. Technol.,2019

5. Effects of surface deposition, hole blockage, and TBC spallation on vane endwall film-cooling;Sundaram;ASME Turbo Expo 2006: Power Land Sea Air,2006

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