Abstract
Fatigue crack growth tests in mixed-mode II + III were performed on maraging steel and Ti-6Al-4V. The 3D evolutions of the crack fronts -measured by SEM after interrupted tests- were analyzed, taking into account the reduction in effective crack driving force by the interlocking and friction of the asperities of the crack surface. Under small-scale yielding conditions, the mixed-mode crack growth rates were found to correlate best with \({\sqrt{{\Delta {\rm K}}_{\rm II}^{{\rm eff}^{2}}+1.2\Delta {\rm K}_{\rm III}^{{\rm eff}^{2}}}}\) in maraging steel, while for Ti-6Al-4V, \({\sqrt{\Delta {\rm K}_{\rm II}^{{\rm eff}^{2}}+0.9\Delta {\rm K}_{\rm III}^{{\rm eff}^{2}}}}\) appeared suitable. For extended plasticity, a crack growth prediction method is proposed and validated for Ti-6Al-4V. This method is based on elastic-plastic F.E. computations and application, ahead of each node of the crack front, of a shear-dominated fatigue criterion.
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Abbreviations
- α :
-
angle between the precrack front and a horizontal axis
- \({\Delta {\rm K}_{\rm II}^{\rm nominal}, \Delta{\rm K}_{\rm III}^{\rm nominal}}\) :
-
Amplitude of Mode II or Mode III stress intensity factor computed for a frictionless crack
- \({\Delta {\rm K}_{\rm II}^{\rm effective}, \Delta{\rm K}_{\rm III}^{\rm effective}}\) :
-
Amplitude of Mode II or Mode III stress intensity factor after friction correction
- E, ν :
-
Young’s modulus, Poisson’s ratio
- G:
-
energy release rate
- Δγ :
-
shear strain range along the critical plane, in Fatemi and Socie’s fatigue criterion
- σ n, max :
-
peak opening stress along the critical plane, in Fatemi and Socie’s fatigue criterion
- σ y :
-
yield stress
- k:
-
a material-dependent constant in Fatemi and Socie’s fatigue criterion
- βFS :
-
fatigue damage parameter, in Fatemi and Socie’s fatigue criterion
- l :
-
length of the segment ahead of a point along the crack front over which the fatigue damage parameter βFS, is averaged before the computation of its fatigue life: Nfracture
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Doquet, V., Bui, Q.H., Bertolino, G. et al. 3D shear-mode fatigue crack growth in maraging steel and Ti-6Al-4V. Int J Fract 165, 61–76 (2010). https://doi.org/10.1007/s10704-010-9504-7
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DOI: https://doi.org/10.1007/s10704-010-9504-7