2013 14th International Conference on Thermal, Mechanical and Multi-Physics Simulation and Experiments in Microelectronics and 2013
DOI: 10.1109/eurosime.2013.6529951
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Finite element analysis of fatigue cracks formation in power metallisation of a semiconductor device subjected to active cycling

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Cited by 12 publications
(17 citation statements)
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“…As can be observed, the crack emerges at the transition from the convex to the straight segment of the interface. It is interesting to note that this location was also predicted in (Kravchenko et al, 2013) for formation of fatigue crack in Cu using the Fatemi-Socie shear strain based fatigue indicator parameter. Further cycling (figure 3b) results in growth of delamination along the straight segment of the interface (indicated by points A and B in the figure) and emergence of the second crack after 220 cycles.…”
Section: Fem Model Descriptionmentioning
confidence: 97%
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“…As can be observed, the crack emerges at the transition from the convex to the straight segment of the interface. It is interesting to note that this location was also predicted in (Kravchenko et al, 2013) for formation of fatigue crack in Cu using the Fatemi-Socie shear strain based fatigue indicator parameter. Further cycling (figure 3b) results in growth of delamination along the straight segment of the interface (indicated by points A and B in the figure) and emergence of the second crack after 220 cycles.…”
Section: Fem Model Descriptionmentioning
confidence: 97%
“…A more detailed discussion of the structural BCs can be found in (Kravchenko et al, 2013). The model was meshed with two-dimensional isoparametric elements with quadratic shape functions.…”
Section: Fem Model Descriptionmentioning
confidence: 99%
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“…The critical plane is identified as the plane experiencing the maximum value of the Fatigue Indicator. In case of non-proportional loading the determination of the shear strain amplitude usually requires numerical search algorithm, which makes the identification of the FIP computational expensive [7]. For lifetime estimations in the LCF regime the maximum FIP can be expressed as,…”
Section: A Fatigue Crack Nucleationmentioning
confidence: 99%
“…Hence, they cannot provide an insight into the mechanism leading to material degradation. Mechanical quantities in terms of thermo-mechanical fatigue considerations seem to be more physically sound for the prediction of material degradation [6], [7].…”
Section: Introductionmentioning
confidence: 99%