Characterization of isothermal and cyclic thermal damage of EB‐PVD TBCs with the help of the 3D‐DIC technique
Author:
Affiliation:
1. School of Aerospace Engineering Tsinghua University Beijing 100084 China
2. Tsinghua University, Institute for Aero Engines Beijing 100084 China
Funder
National Natural Science Foundation of China
National Science and Technology Major Project
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1111/ffe.13593
Reference53 articles.
1. Creep‐fatigue behaviour of single‐crystal Ni‐base superalloy CMSX‐8
2. Damage mechanisms, life prediction, and development of EB-PVD thermal barrier coatings for turbine airfoils
3. Thermal barrier coatings technology: critical review, progress update, remaining challenges and prospects
4. Development and analysis of thermal barrier coatings on gas turbine blades – A Review
5. Composite ceramics thermal barrier coatings of yttria stabilized zirconia for aero-engines
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