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Data-driven inverse design of C/C honeycombs via multiscale damage modeling

  • Lijia Guo
  • , Weijie Li*
  • , Ying Liu
  • , Ying Li
  • *Corresponding author for this work
  • Beijing Jiaotong University
  • Beijing Institute of Technology

Research output: Contribution to journal › Article › peer-review

Abstract

Carbon/carbon honeycomb sandwich structures (C/C-HSS) represent a next-generation solution for load-bearing platforms in space systems, offering superior mechanical performance, lightweight characteristics and excellent thermal stability. However, their design optimization poses a significant challenge due to highly nonlinear, multiscale interactions and conflicting objectives such as strength, stiffness, low weight, and thermal reliability. This study proposes a novel data-driven inverse design framework that integrates three key components: a multiscale thermo-mechanical-damage model, an interpretable deep learning surrogate, and multi-objective evolutionary optimization. A multiscale thermo-mechanical-damage model is first employed to accurately simulate the thermo-mechanical responses of C/C-HSS under varying thermal conditions, thus generating a comprehensive dataset. A deep neural network (DNN) surrogate is then trained on this dataset to predict eight critical structural properties with high accuracy (R² > 0.99, RMSE < 5 %). Feature importance is interpreted using SHapley Additive exPlanations (SHAP), revealing dominant design factors such as wall thickness and side length. Subsequently, a Non-dominated Sorting Genetic Algorithm II (NSGA-II) is employed to efficiently explore the design space and identify Pareto-optimal configurations that achieve significant weight reduction and high load-bearing capacity, while maintaining excellent thermal stability across a wide temperature range. This integrated approach achieves a 95 % reduction in computational expenditure compared to conventional finite element (FE) based optimization, while establishing a generalizable paradigm for multiscale inverse design of C/C-HSS operating under extreme aerospace thermal-mechanical conditions. The optimized configurations demonstrate 22 % mass reduction relative to baseline designs, while achieving uncompromised thermal stability, with computational efficiency exceeding traditional FE methods by an order of magnitude.

Original languageEnglish
Article number110835
JournalInternational Journal of Mechanical Sciences
Volume306
DOIs
Publication statusPublished - 15 Nov 2025

Keywords

  • Data-driven design
  • Deep neural network surrogate
  • Honeycomb sandwich structures
  • Inverse design
  • Multiscale thermo-mechanical-damage model
  • NSGA-II optimization

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