2014
DOI: 10.1016/j.crme.2014.11.001
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Edge cracking due to a compressive residual stress in ceramic laminates

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Cited by 9 publications
(11 citation statements)
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“…The scattering is large, it extends roughly from 30 to 110 MPa. The analysis in (Leguillon et al, 2015) of the onset of and edge crack in the compressive layers leads to a similar conclusion, residual stresses are more likely corresponding to a cooling lying between 800 −°C ( 1R σ = 74 MPa,…”
Section: The Coupled Thermo-elastic Problemmentioning
confidence: 55%
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“…The scattering is large, it extends roughly from 30 to 110 MPa. The analysis in (Leguillon et al, 2015) of the onset of and edge crack in the compressive layers leads to a similar conclusion, residual stresses are more likely corresponding to a cooling lying between 800 −°C ( 1R σ = 74 MPa,…”
Section: The Coupled Thermo-elastic Problemmentioning
confidence: 55%
“…the edge crack runs parallel to the direction of applied stress. In general, the edge crack depth seems to be smaller or the same order than the thickness of the AMZ layer (Leguillon et al, 2015).…”
Section: The Tested Specimens and The Failure Mechanismsmentioning
confidence: 87%
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“…Some authors have speculated that this phenomenon may be related to crack bifurcation observed in some laminates with relatively high compressive residual stresses [37,38]. In a recent work, the present authors have applied a stress-energy criterion to set the conditions for edge cracking formation and extension within a particular laminate [39]. However, an understanding of the parameters related to the onset and extension of such edge cracks in the compressive layers is still lacking.…”
Section: Introductionmentioning
confidence: 99%