Numerical simulation of fatigue‐driven delamination using interface elements
By P. Robinson, Ugo Galvanetto, D. Tumino, G. Bellucci, D. Violeau. 2005
192 citations recorded by the source corpus.
Subfields: Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/1b8e140d5b869ff42cc8b6af7aa2a129c50e9fb3
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In Mechanics of Materials
- S. Hallett
- M. Wisnom
- Pedro P. Camanho
- L. Kawashita
- Paul W. Harper
- F. P. van der Meer
- Lambertus J. Sluys
- C. Dávila
Citations in the corpus
- Methods for the prediction of fatigue delamination growth in composites and adhesive bonds: A critical review (2013, background): “[180] proposed a damage parameter that was split into two parts: one for the static portion of delamination growth and one for the fatigue portion.”
- A concise interface constitutive law for analysis of delamination and splitting in composite materials and its application to scaled notched tensile specimens (2007, background): “quickly for very small values of the relative displacement [15], and it even varies with initial stiffness values.”
- Predicting fatigue damage in adhesively bonded joints using a cohesive zone model (2010, methodology): “Alternatively, some other researchers [23,24] developed fatigue damage models based on maximum fatigue load conditions.”
- A fatigue degradation law for cohesive interface elements – Development and application to composite materials (2010, methodology): “Whilst formulations have been developed to account for damage under cyclic loading [20,21,22,23,24], these tend to”
- A crack tip tracking algorithm for cohesive interface element analysis of fatigue delamination propagation in composite materials (2012, methodology): “Previous implementations of fatigue cohesive elements reported in the literature (Robinson et al., 2005; Turon et al., 2007; Harper and Hallett, 2010) used instantaneous values of strain energy release rate to compute the fatigue degradation rate, i.”
- Simulation of delamination in composites under high-cycle fatigue (2007, methodology): “The material properties are shown in Table 3 [11,38,39].”