Simulation outputs revealed fracture resistance of self healing interleaves in composites, indicating effective modeling for aerospace applications.
The predictive capabilities of the finite element approach were assessed by comparing simulation outputs with experimental results, including load-displacement trends, damage initiation points, and delamination evolution. This comparison validated the effectiveness of the self-healing interleaves and highlighted the strengths and limitations of the adopted numerical framework. The simulations not only reproduced key damage characteristics but also provided a deeper understanding of failure mechanisms in the modified laminates. This modeling strategy contributes to the broader goal of developing high-fidelity virtual testing tools for complex, multifunctional composite structures used in aerospace and related industries.
No takes yet. Share an insight, caveat, or question.
Rouvalis et al. (2025) studied this question.
Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context: