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 model is verified for mode I, mode II and mixed-mode benchmark problems. A debonding problem is analyzed with both standard 3D cohesive elements and the proposed element. The results show that the element size in the proposed models can be much larger than that in the standard model, with more than 95% reduction in CPU time, while retaining prediction accuracy. The debonding analysis of a complex stiffened panel is also presented to demonstrate the intended use of the proposed element for simulating debonding in structural components.

翻译：暂无翻译