2015
DOI: 10.1016/j.surfcoat.2015.01.063
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A dynamic FEM simulation of the nano-impact test on mono- or multi-layered PVD coatings considering their graded strength properties determined by experimental–analytical procedures

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Cited by 41 publications
(30 citation statements)
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“…In the developed FEA-model, a surface-to-surface contact was applied for describing the interface between the nasal bone and the instrument. In addition, an eroding contact was applied between instrument and nasal bone material [21,22]. In this way, elements involved in the contact definition are subjected to erosion (element deletion) according to a material failure criterion and not directly due to the eroding contact restrictions.…”
Section: Analytical Resultsmentioning
confidence: 99%
“…In the developed FEA-model, a surface-to-surface contact was applied for describing the interface between the nasal bone and the instrument. In addition, an eroding contact was applied between instrument and nasal bone material [21,22]. In this way, elements involved in the contact definition are subjected to erosion (element deletion) according to a material failure criterion and not directly due to the eroding contact restrictions.…”
Section: Analytical Resultsmentioning
confidence: 99%
“…A detailed review of existing papers in the field of crack formation in multilayered coatings, with classification of types of cracks and analysis of the mechanisms of their formation, is given in [17]. The topic of mathematical modeling of cracking in multilayered coatings with the use of an axis-symmetrical finite element method (FEM) model was considered by Skordaris et al [18]. Wu et al [19,20] modeled cracking in single-layer coatings within the framework of linear elastic fracture mechanics (LEFM).…”
Section: Literature Reviewmentioning
confidence: 99%
“…The convection mode would be dominant in consideration of that the droplet particles are heated in the air flow. Physical parameters for numerical analysis are listed in Table 1 [15][16][17][18] . According to the Lagrangian motion, equation of particles can be obtained as follows:…”
Section: Twas Flight Dynamicsmentioning
confidence: 99%