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Figure 2 Pre-stretched thin membrane with an interface crack of length a.
Then, the stress intensity factor is derived from the interface crack innano electrodes during galvanostatic charging.
The effects of coating architecture and surface crack morphology on interface crack growth were assessed.
In this paper, the mixed-mode Dugdale model is extended to investigate an interface crack problem.
An interfacial gap, say an opened interface crack, will be considered as a displacement discontinuity in Eq. (10).
An electrically conductive interface crack with a contact zone in a magnetoelectroelastic (MEE) bimaterial system is considered.
A novel crack model, i.e., an interface crack with pre-fracture zones is introduced for magnetoelectroelastic bimaterial system.
(c) An unelectroded rather than electroded outer surface is beneficial to reducing the stress intensity factor of the interface crack.
Explicit solutions of the stress intensity factors are obtained for a semi-infinite interface crack and a circular composite disk with an interface crack.
The location of the interface crack within the stress transfer zone and the cohesive stress transfer during the propagation of the interface crack are determined.
In straight-ahead propagation case, the interface is relatively weaker than the bordering materials, meaning that the interface crack propagates along the least resistance path, interface.
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