Compositionally graded thermal barrier coatings for high temperature aero gas turbine components-Reference-Cited by-同舟云学术

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Compositionally graded thermal barrier coatings for high temperature aero gas turbine components

Published:1992-11 Issue: Volume:54-55 Page:58-63
ISSN:0257-8972
Container-title:Surface and Coatings Technology
language:en
Short-container-title:Surface and Coatings Technology

Author:

Jamarani F.,Korotkin M.,Lang R.V.,Ouellette M.F.,Yan K.L.,Bertram R.W.,Parameswaran V.R.

Publisher

Elsevier BV

Subject

Materials Chemistry,Surfaces, Coatings and Films,Surfaces and Interfaces,Condensed Matter Physics,General Chemistry

Reference14 articles.

1. The durability and performance of coatings in gas turbine and diesel engines

2. High temperature coatings for gas turbine blades: A review

3. Ionization assisted physical vapor deposition of zirconia thermal barrier coatings

4. Thermal barrier coatings for turbine airfoils

Cited by 12 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Evaluating the oxidation resistance of bond coats on thermal barrier coatings;Welding International;2017-03

2. Avaliação da Resistência à Oxidação de Camadas de Ligação de Revestimentos Utilizados em Barreiras Térmicas;Soldagem & Inspeção;2015-12

3. Ceramic matrix composite thermal barrier coatings for turbine parts;Advances in Ceramic Matrix Composites;2014

4. Effects of High Temperature Treatment on Thermal Cyclic Behavior of Thermal Barrier Coatings;Key Engineering Materials;2013-11

5. Thermal barrier coatings prepared by electron beam physical vapor deposition (EB–PVD);Thermal Barrier Coatings;2011

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