Variable-Stiffness Composite Optimization Using Dynamic and Exponential Multi-Fidelity Surrogate Models

•A dynamic multi-fidelity surrogate optimization framework is newly developed.•The proposed initial sampling strategy generates higher values of buckling load.•The new exponential correction function exhibits comparable or better performances.•Computational saving reach 65% and 55% for the plate and...

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Veröffentlicht in:International journal of mechanical sciences 2023-11, Vol.257, p.108547, Article 108547
Hauptverfasser: An, Haichao, Youn, Byeng D., Kim, Heung Soo
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Sprache:eng
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Zusammenfassung:•A dynamic multi-fidelity surrogate optimization framework is newly developed.•The proposed initial sampling strategy generates higher values of buckling load.•The new exponential correction function exhibits comparable or better performances.•Computational saving reach 65% and 55% for the plate and cylinder, respectively. Variable-stiffness composite laminates with spatially varied orientation angles always require refined finite element models to accurately model the spatial variation characteristics, thus resulting in high computation costs. Further, practical restrictions in fiber steering should be imposed to generate manufacturable designs, making the design problem more challenging. To address these challenges, this paper presents a new framework assisted by multi-fidelity surrogate models for variable-stiffness composite optimization with manufacturing constraints. An initial sampling strategy is originally developed for the case of involving the fiber steering constraints, improving the accuracy of the surrogate model in the concerned space. Based on Gaussian process regressions, a new type of multi-fidelity model corrected with an exponential function is proposed by fusing many cheap low-fidelity models and a few expensive high-fidelity models. Using genetic algorithm as the optimizer, new data points are generated from the optimization process and then employed to dynamically update the constructed multi-fidelity model. The proposed optimization strategy is applied to case studies of buckling optimization for both a composite plate and a composite cylinder, demonstrating that the developed framework requires significantly less computation. [Display omitted]
ISSN:0020-7403
1879-2162
DOI:10.1016/j.ijmecsci.2023.108547