{"title":"Data-driven inverse design of C/C honeycombs via multiscale damage modeling","authors":"Lijia Guo , Weijie Li , Ying Liu , Ying Li","doi":"10.1016/j.ijmecsci.2025.110835","DOIUrl":null,"url":null,"abstract":"<div><div>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.</div></div>","PeriodicalId":56287,"journal":{"name":"International Journal of Mechanical Sciences","volume":"306 ","pages":"Article 110835"},"PeriodicalIF":9.4000,"publicationDate":"2025-09-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Mechanical Sciences","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0020740325009178","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0
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.
期刊介绍:
The International Journal of Mechanical Sciences (IJMS) serves as a global platform for the publication and dissemination of original research that contributes to a deeper scientific understanding of the fundamental disciplines within mechanical, civil, and material engineering.
The primary focus of IJMS is to showcase innovative and ground-breaking work that utilizes analytical and computational modeling techniques, such as Finite Element Method (FEM), Boundary Element Method (BEM), and mesh-free methods, among others. These modeling methods are applied to diverse fields including rigid-body mechanics (e.g., dynamics, vibration, stability), structural mechanics, metal forming, advanced materials (e.g., metals, composites, cellular, smart) behavior and applications, impact mechanics, strain localization, and other nonlinear effects (e.g., large deflections, plasticity, fracture).
Additionally, IJMS covers the realms of fluid mechanics (both external and internal flows), tribology, thermodynamics, and materials processing. These subjects collectively form the core of the journal's content.
In summary, IJMS provides a prestigious platform for researchers to present their original contributions, shedding light on analytical and computational modeling methods in various areas of mechanical engineering, as well as exploring the behavior and application of advanced materials, fluid mechanics, thermodynamics, and materials processing.