A Shell-to-Shell Cohesive Line Element for Efficient Modeling of Interfacial Cracking in Overmolded Stiffened Panels
S\'ergio G. F. Cordeiro, Boyang Chen, Frans P. van der Meer

TL;DR
This paper introduces a novel shell-to-shell cohesive element that enables efficient and accurate modeling of interfacial debonding in thermoplastic composite panels with stiffeners, significantly reducing computational cost.
Contribution
A new cohesive element design for shell models that allows larger element sizes and reduces CPU time in simulating interfacial debonding in stiffened panels.
Findings
Over 95% reduction in CPU time compared to standard models.
Accurate prediction of debonding in benchmark problems.
Successful application to complex stiffened panel analysis.
Abstract
The wide adoption of thermoplastic composites to reduce weight in structural parts requires reliable numerical methods to account for debonding between overmolded parts. Although cohesive elements are effective for debonding, the need for very fine meshes in the cohesive zone limits their practical use. In the present work, a novel structural cohesive element is proposed for the efficient modeling of debonding in thermoplastic composite panels with overmolded stiffeners. Three-node triangular Kirchhoff-Love shell elements are employed for the modelling of thin panels and stiffeners. The proposed cohesive element perpendicularly connects the shell elements representing the rib to those representing the plate. The displacement discontinuity is defined from the evaluation of the shell fields at the elements edges, while allowing for transmission of cohesive forces and cohesive couples. The…
Peer Reviews
No public reviews on file for this paper yet. If you reviewed it on a platform where reviews are public (OpenReview, ICLR, NeurIPS, ICML), you can paste yours below so the community can read it here.
Videos
No videos yet. Explain this paper in a talk, walkthrough, or lecture? Add one.
