New Strategies for Improvement of Structural Gas Turbine Engine Parts

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In this study, the basic limitations of superalloys in high temperature performances will be explained and then after giving the important properties of MoSi2 such as oxidation behaviour at relatively low temperatures (500°C-700°C) , some interesting composites of this material will be discussed as a candidate structural material in gas turbine engines.

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1368-1373

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June 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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