Abstract
This paper presents a model that predicts the stress field around intergranular corrosion. The stress analysis is conducted in ABAQUS via a Python input script, which is written in Igor Pro. The intergranular corrosion path is described using a Monte-Carlo Markov Chain based on the materials grain size distribution and probability that the corrosion will turn at a grain boundary junction.
The model allows a complete analysis of the stresses resulting from intergranular corrosion around a fastener hole of any size. As fatigue initiation is most likely to occur at the highest stress concentration, this model gives an understanding of which of the features of intergranular corrosion are most critical and can allow for the development of beta solutions for crack growth. This model has been applied to 7075-T651 extruded aluminum alloy from a legacy era aircraft but can be readily applied to any material where the microstructure is known and can be described using a statistical distribution.
Publisher
Trans Tech Publications, Ltd.
Reference13 articles.
1. J.R. Galvele and S.M. de De Micheli, Mechanism of intergranular corrosion of Al-Cu alloys, Corros. Sci., 10 (1970) pp.795-807.
2. S. Maitra and G. English, Mechanism of localized corrosion of 7075 alloy plate, Metall. Mater. Trans. A, 12(3) (1981) pp.535-541.
3. K. Jones and D.W. Hoeppner, The interaction between pitting corrosion, grain boundaries, and constituent particles during corrosion fatigue of 7075-T6 aluminium alloy, Int. J. Fatigue, 2009, 31 (2009) pp.686-92.
4. A. Uebersax, C. Huber, G. Renaud and M. Liao, Structural integrity of a wing upper skin with exfoliation corrosion, in ICAF 2009, Bridging the gap between theory and operational practice, Rotterdam, The Netherlands, (2009) pp.245-61.
5. M. Salagaras, A. Wythe and P. Trathen, Methodology for producing IGC on AA7075-T651, In: Australasian Corrosion Conference, (2012) Melbourne, Australia November.
Cited by
4 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献