A new spallation mechanism of thermal barrier coatings on aero-engine turbine blades
ABSTRACT: Laboratory experiments were conducted to study the spallation behaviour of thermal barrier coatings (TBCs) on aero-engine turbine blades manufactured by the electron-beam physical vapour deposition technique (EB-PVD). Intact blades were heated at temperature 1135°C in a furnace for certain...
| 出版年: | Theoretical and Applied Mechanics Letters |
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| 主要な著者: | , , , , |
| フォーマット: | 論文 |
| 言語: | 英語 |
| 出版事項: |
Elsevier
2018-01-01
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| オンライン･アクセス: | http://www.sciencedirect.com/science/article/pii/S2095034918300618 |