2022
DOI: 10.1016/j.engfracmech.2022.108568
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Fracture-based transient thermo-mechanical analysis of reciprocating engine thermal barrier coatings

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Cited by 8 publications
(6 citation statements)
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“…For all of the conditions tested, the maximum energy release rate was found to occur on the cycle that had the highest surface temperature (other criteria tested included cycles with the highest heat flux, highest temperature difference between combustion and oil surface, and highest interface temperature). Additionally, previous results indicated 51 that the peak energy release rate was found to occur later in the cycle than the peak surface temperature. Delamination was often located within the coating as compared to at the coating-substrate interface where there was a mismatch in coefficient of thermal expansion, or at the coating surface where the stress was maximum.…”
Section: Computational Approachmentioning
confidence: 84%
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“…For all of the conditions tested, the maximum energy release rate was found to occur on the cycle that had the highest surface temperature (other criteria tested included cycles with the highest heat flux, highest temperature difference between combustion and oil surface, and highest interface temperature). Additionally, previous results indicated 51 that the peak energy release rate was found to occur later in the cycle than the peak surface temperature. Delamination was often located within the coating as compared to at the coating-substrate interface where there was a mismatch in coefficient of thermal expansion, or at the coating surface where the stress was maximum.…”
Section: Computational Approachmentioning
confidence: 84%
“…where U whole , U bottom , and U top are the strain energy of the intact multilayer, piston substrate, and debonded coating, respectively. The general methodology to calculate the energy release rate and the the equations that estimate each strain energy, which are involved and can not be easily summarized, are given in Koutsakis et al 51,52 The hypothesis is that the crack will advance when G exceeds a threshold that depends only on thermomechanical material properties. This critical parameter is the toughness G c of the material or the interface -it is an experimental measurement, not a calculated parameter.…”
Section: Multilayer Mechanics Analysismentioning
confidence: 99%
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