Abstract
The structural integrity of thick fiber-reinforced polymer (FRP) laminates in naval applications relies on effective repair strategies. While stepped repairs provide aerodynamic and hydrodynamic continuity, optimizing their geometry involves a complex trade-off between strength recovery and material removal. High-fidelity Finite Element Method (FEM) simulations are essential to capture non-linear compressive failure modes but are computationally prohibitive for traditional iterative optimization. This study proposes a Deep Kernel Bayesian Optimization framework to accelerate the geometric design of stepped repairs. We employ a Deep Kernel Gaussian Process (DKGP) that couples a deep neural network feature extractor with a Gaussian Process to quantify epistemic uncertainty, guiding the search toward high-performance regions. To mitigate overfitting on sparse data, a novel progressive complexity strategy is introduced, dynamically adapting the neural architecture depth. Validated against parametric Cohesive Zone Modeling (CZM) simulations, the framework reduces computational cost by approximately 96% compared to Genetic Algorithms (GA) and 80% compared to static sampling. Crucially, the framework autonomously identified a strength-recovery limit (≈ 95% strength recovery) and learned to avoid premature adhesive debonding in complex off-axis ply configurations.
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Stamatelatos, G., Billaudeau, E., Sergolle, M., Balutch, T., Kostopoulos, V., Loutas, T., & Psarras, S. (2026). Deep Kernel Bayesian Optimization for the design of stepped composite repairs under compression. Composites Part A: Applied Science and Manufacturing, 210. https://doi.org/10.1016/j.compositesa.2026.110099
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