Characterisation of thermal barrier coatings
High pressure turbine blades in aircraft are subject to high temperatures, often above 1000˚C, during in-flight operations, thus the base metal requires protection from oxidation by an aluminide coating, which generates a protective oxide layer on top of itself. In this study, research was carried o...
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| 格式: | Final Year Project |
| 語言: | English |
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2015
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| 在線閱讀: | http://hdl.handle.net/10356/65157 |
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