Abstract
Fatigue crack-growth is simulated for multiple surface cracks in a plate subjected to different combinations of tension and bending loads. The numerical technique employed is based on the step-by-step integration of a Paris' type of fatigue crack-growth law at a set of points of crack front, which enables the crack shape change during propagation to be traced. The stress intensity factors along the crack front are estimated by the three-dimensional finite element method. The technique has also accommodated an automatic procedure for the regeneration of finite element models as the crack grows, so that the prediction of complex crack shape change undergoing particularly during the crack coalescence is made possible and easy. The fatigue growth behaviours at three typical growth stages, i.e. pre-coalescence, coalescence and post-coalescence, are analysed for two multiple crack configurations. The predicted results are also compared with those obtained by the ASME XI code and a ‘no interaction and immediate transition (NIIT)’ simplified method. It is shown that each individual crack before they touch propagates almost independently and the interaction between them is generally limited despite being dependent on actual crack configurations. The analyses of fatigue lives show that both the ASME XI code and the NIIT method give more conservative results than the present simulation technique; however, the NIIT method is relatively less conservative than the ASME XI code which is excessively conservative for the crack configuration examined.
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Lin, X., Smith, R. Fatigue growth analysis of interacting and coalescing surface defects. International Journal of Fracture 85, 283–299 (1997). https://doi.org/10.1023/A:1007476729339
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DOI: https://doi.org/10.1023/A:1007476729339