2008
DOI: 10.1016/j.jmps.2008.05.002
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Inelastic deformation and energy dissipation in ceramics: A mechanism-based constitutive model

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Cited by 138 publications
(125 citation statements)
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“…Having determined l and a, the triaxial failure envelope (r 1 vs. r 3 at failure) was fit (at low confining stress) by varying the parameter b and the value of the initial damage D o as discussed further in a subsequent section. DESHPANDE and EVANS (2008) added a term to the strain energy density in Eq. 5 that represents the increase in elastic energy density associated with a pair of wing cracks each of length l…”
Section: Regime 3: Wing Cracks Nucleate and Grow From The Tips Of Thementioning
confidence: 99%
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“…Having determined l and a, the triaxial failure envelope (r 1 vs. r 3 at failure) was fit (at low confining stress) by varying the parameter b and the value of the initial damage D o as discussed further in a subsequent section. DESHPANDE and EVANS (2008) added a term to the strain energy density in Eq. 5 that represents the increase in elastic energy density associated with a pair of wing cracks each of length l…”
Section: Regime 3: Wing Cracks Nucleate and Grow From The Tips Of Thementioning
confidence: 99%
“…The formulations of ASHBY and SAMMIS (1990) and DESHPANDE and EVANS (2008) assume that the growing wing cracks are all parallel. We still assume all starter flaws are at the same angle W with respect to x 1 , but now assume that the components of their normal vectors in the x 1 and x 1 directions are randomly distributed as in Fig.…”
Section: Allowing Non-parallel Initial Flawsmentioning
confidence: 99%
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