4.5 Article

Phase-field modelling for fatigue crack growth under laser shock peening-induced residual stresses

Journal

ARCHIVE OF APPLIED MECHANICS
Volume 91, Issue 8, Pages 3709-3723

Publisher

SPRINGER
DOI: 10.1007/s00419-021-01897-2

Keywords

Laser shock peening; Fatigue crack growth; Phase-field modelling; Residual stresses

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Funding

  1. German Research Foundation DFG [KA 3309/7-2]

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The paper focuses on the application of the phase-field fatigue model in estimating the fatigue life of thin-walled components and the influence of residual stresses on crack growth. By calibrating and comparing the predictions with fatigue crack growth experiments on aluminum sheet material, the study confirms the accuracy of the model. Additionally, the research shows that residual stresses can affect crack growth rate by retarding or accelerating the crack, and a strategy to incorporate residual stresses in the phase-field fatigue model is proposed and tested.
For the fatigue life of thin-walled components, not only fatigue crack initiation, but also crack growth is decisive. The phase-field method for fracture is a powerful tool to simulate arbitrary crack phenomena. Recently, it has been applied to fatigue fracture. Those models pose an alternative to classical fracture-mechanical approaches for fatigue life estimation. In the first part of this paper, the parameters of a phase-field fatigue model are calibrated and its predictions are compared to results of fatigue crack growth experiments of aluminium sheet material. In the second part, compressive residual stresses are introduced into the components with the help of laser shock peening. It is shown that those residual stresses influence the crack growth rate by retarding and accelerating the crack. In order to study these fatigue mechanisms numerically, a simple strategy to incorporate residual stresses in the phase-field fatigue model is presented and tested with experiments. The study shows that the approach can reproduce the effects of the residual stresses on the crack growth rate.

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