Cohesive zone modeling for mode I facesheet to core delamination of sandwich panels accounting for fiber bridging

Volume: 183, Pages: 568 - 581
Published: Jan 1, 2018
Abstract
A new cohesive zone traction-separation law, which includes the effects of fiber bridging, has been developed, implemented with a finite element (FE) model, and applied to simulate the delamination between the facesheet and core of a composite honeycomb sandwich panel. The proposed traction-separation law includes a standard initial cohesive component, which accounts for the initial interfacial stiffness and energy release rate, along with a new...
Paper Details
Title
Cohesive zone modeling for mode I facesheet to core delamination of sandwich panels accounting for fiber bridging
Published Date
Jan 1, 2018
Volume
183
Pages
568 - 581
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