Effects of chromium content on fatigue crack growth behavior of Ti-48Al-xCR alloys

Gamma TiAl alloys are candidate materials for aircraft structural applications due to their inherent high specific stiffness and strength. However, limited room-temperature ductility of these alloys calls for investigation on fatigue crack growth resistance. In this respect, a series of fatigue crac...

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Bibliographic Details
Main Authors: Tamin, Mohd. Nasir, Hamzah, Esah, Ong, Wei Rex
Format: Conference or Workshop Item
Language:English
Published: 2008
Subjects:
Online Access:http://eprints.utm.my/7413/1/NasirTamin2008_EffectsOfChromiumContent.pdf