Affiliation:
1. Université de Poitiers
2. Airbus Operations SAS
Abstract
This paper reports on investigations on the residual fatigue resistance of a 2024 aluminium alloy of an A320 aircraft at the end of life. The fatigue data (S-N and da/dN curves) are compared with data obtained on a pristine alloy using a similar procedure. The results are analysed on the basis of fracture surfaces observations and of AFGROW fatigue life computations.
Publisher
Trans Tech Publications, Ltd.
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2 articles.
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