2019
DOI: 10.1016/j.tafmec.2019.102303
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Development of a physics-based theory for mixed mode I/II delamination onset in orthotropic laminates

Abstract: This paper demonstrates how the critical strain energy density in the delamination tip vicinity may be used to explain the physics of delamination growth under mixed mode I/II. A theory previously proposed to physically relate mode I and mode II delamination growth is further extended towards describing the onset of mixed mode I/II delamination. Subsequently, data from the literature is used to demonstrate that this new concept of the critical strain energy density approach indeed explains, based on the physic… Show more

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Cited by 13 publications
(8 citation statements)
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References 50 publications
(77 reference statements)
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“…It is obvious that there is no general model that can comprehensively consider influence factors of fatigue delamination onset. There are few phenomenological models [1,2,58,80,90] for fatigue delamination onset in composite materials, and there is a lack of experimental verification.…”
Section: Delamination Onset Phenomenological Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…It is obvious that there is no general model that can comprehensively consider influence factors of fatigue delamination onset. There are few phenomenological models [1,2,58,80,90] for fatigue delamination onset in composite materials, and there is a lack of experimental verification.…”
Section: Delamination Onset Phenomenological Modelmentioning
confidence: 99%
“…Moreover, the damage caused by fatigue delamination is irreversible and often leads to a serious decline in the performance of components and even flight accidents. Therefore, research on the initiation and propagation law [1,2], the failure mechanism [3,4], and the numerical simulation [5,6] of delamination under fatigue loads is important for the damage tolerance and durability design of composite laminated structures.…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, the damage of fatigue delamination is irreversible, which often leads to a serious decline in the performance of components and even flight accidents. Therefore, the researches on initiation and propagation law [1,2], the failure mechanism [3,4] and the numerical simulation [5,6] of delamination under fatigue loads are the significant issues to the damage tolerance and durability design of composite laminated structures.…”
Section: Introductionmentioning
confidence: 99%
“…In the FPZ, several mechanisms such as the nucleation of micro-cracks cause the dissipation of energy and prevent catastrophic failure [55][56][57][58][59]. The effects of the FPZ, where micro-cracks nucleate and propagate, have been studied and a criterion derived based on dissipated energy in the FPZ [60]. Given the fracture toughness based on the maximum strain energy release rate (SERR), a rather accurate approximation of fracture based on the fracture mechanics becomes possible [61].…”
Section: Introductionmentioning
confidence: 99%