2004
DOI: 10.1557/proc-821-p3.13
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Debonding Under Fatigue Loading at Polymer/Inorganic Interfaces

Abstract: The mechanisms associated with cycle-by-cycle damage accumulation resulting in fatigue crack propagation between a highly constrained polymer layer and an adjacent elastic substrate are explored. Specifically, cyclic fatigue-induced crack growth between a bisphenol F model epoxy system and a passivated silicon substrate under Mode I loading is reported. Preliminary findings regarding the effects of fatigue load ratio on interfacial crack growth rates are presented. While intermediate crack growth rates were si… Show more

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Cited by 2 publications
(1 citation statement)
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“…At this critical load where crack growth occurs, the strain energy release rate equals the interfacial fracture energy. This experimental technique was derived by originally Charalambides for laminate composites [19,20] and then further developed to measure the adhesion of thin films for microelectronics by Dauskardt et al [21][22][23][24][25][26][27][28][29][30][31][32][33][34][35][36][37].…”
Section: Four-point Bendingmentioning
confidence: 99%
“…At this critical load where crack growth occurs, the strain energy release rate equals the interfacial fracture energy. This experimental technique was derived by originally Charalambides for laminate composites [19,20] and then further developed to measure the adhesion of thin films for microelectronics by Dauskardt et al [21][22][23][24][25][26][27][28][29][30][31][32][33][34][35][36][37].…”
Section: Four-point Bendingmentioning
confidence: 99%