New strategies for improvement of structural gas turbine engine parts
Özet
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
Kaynak
Applied Mechanics and MaterialsCilt
327Bağlantı
https://dx.doi.org/10.4028/www.scientific.net/AMM.325-326.1368https://hdl.handle.net/11421/21912