Peridynamic Method for Simulating Damage Evolution of Thermal Barrier Coatings in Aero-Engine Turbine Blades

Author:

Wu Haoqi,Qi Hongyu,Li Shaolin,Shi Duoqi,Yang Xiaoguang

Publisher

Elsevier BV

Reference40 articles.

1. Gadolinium zirconate/YSZ thermal barrier coatings: Mixed-mode interfacial fracture toughness and sintering behavior;Martin Frommherz;Surface and Coatings Technology,2016

2. Composite ceramics thermal barrier coatings of yttria stabilized zirconia for aero-engines;Qiaomu Liu;Journal of Materials Science & Technology,2019

3. CMAS Corrosion Behavior and Protection Method of Thermal Barrier Coatings for Aeroengine;Guo Lei;Acta Metallurgica Sinica,2021

4. Research on Failure Behavior and Life Prediction of Thermal Barrier Coatings;Jianan Song;Aeronautical Manufacturing Technology,2019

5. Thermal Barrier Coatings for Gas-Turbine Engine Applications;Nitin P Padture;Science,2002

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