2016
DOI: 10.1115/1.4034988
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Edge Debonding in Peeling of a Thin Flexible Plate From an Elastomer Layer: A Cohesive Zone Model Analysis

Abstract: A cohesive zone modeling (CZM) approach with a bilinear traction-separation relation is used to study the peeling of a thin overhanging plate from the edge of an incompressible elastomeric layer bonded firmly to a stationary rigid base. The deformations are approximated as plane strain and the materials are assumed to be linearly elastic, homogeneous, and isotropic. Furthermore, governing equations for the elastomer deformations are simplified using the lubrication theory approximations, and those of the plate… Show more

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Cited by 6 publications
(3 citation statements)
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“…This means that for the cohesive zone model used in [13], the maximum normal debonding stress during uplift,σ , at which interface damage starts, and the Griffith' energy release rates for mode I , G c I , and for mode II, G c II , respectively, have to be varied appropriately. For more advanced cohesive zone models for simulating debonding of the film from the substrate, see [27]. Figure 21 shows, from simulation and experimental results, what happens if the global stretch approaches the critical value and surpasses it.…”
Section: Thin Filmsmentioning
confidence: 99%
“…This means that for the cohesive zone model used in [13], the maximum normal debonding stress during uplift,σ , at which interface damage starts, and the Griffith' energy release rates for mode I , G c I , and for mode II, G c II , respectively, have to be varied appropriately. For more advanced cohesive zone models for simulating debonding of the film from the substrate, see [27]. Figure 21 shows, from simulation and experimental results, what happens if the global stretch approaches the critical value and surpasses it.…”
Section: Thin Filmsmentioning
confidence: 99%
“…For type-1 (edge initiation) debonding ( φ = 1 and 3), the descending portions of the LD curves are smooth. As suggested by an approximate semianalytical model for type-1 debonding process ( Mukherjee et al, 2016c ), the LD curves for such debonding process depend only on the ratio φ/α for a given value of A 0 . The LD data computed for φ/α = 1 and A 0 = 2 .…”
Section: Load-displacement Curvesmentioning
confidence: 99%
“…The further increase in δ A results in the propagation of this debond with a CZ at its front. This edge debonding, named type-1 for later reference, has been studied by a semi-analytical method using a CZM by Mukherjee et al (2016c) who extended techniques of Dillard (1989) and Ghatak et al (2005) . Their results reveal that the CZ size increases with an increase in the quantity α/ φ.…”
Section: Analysis Of Damage Growth and Debondingmentioning
confidence: 99%