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Crack tip deformation fields and fatigue crack growth rates in Ti-6Al-4V

Abstract:

In this paper we present an overview of experimental and modelling studies of fatigue crack growth rates in aerospace titanium alloy Ti-6Al-4V. We review work done on the subject since the 1980s to the present day, identifying test programmes and procedures and their results, as well as predictive approaches developed over this period. We then present the results of some of our recent experiments and simulations. Fatigue crack growth rates (FCGRs) under constant applied load were evaluated as...

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Publication status:
Published

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Institution:
University of Oxford
Department:
Oxford, MPLS, Engineering Science
Role:
Author
More by this author
Institution:
University of Oxford
Department:
Oxford, MPLS, Engineering Science
Role:
Author
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Volume:
31
Issue:
11-12
Pages:
1771-1779
Publication date:
2009-01-01
DOI:
ISSN:
0142-1123
URN:
uuid:049eb2f5-3d98-4bba-95cf-081aaf342505
Source identifiers:
63705
Local pid:
pubs:63705

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