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Research paper | Publishing Language: Chinese | Open Access

A concurrent computational method for multiscale damage evolution in ceramic matrix composites based on self-consistent clustering

Jianxing MAO1,2Guican WANG1Yu LIU3( )Jinchao PAN1,2( )Penghui MA4Xi LIU2,4Dianyin HU1,2Rongqiao WANG2,4
Research Institute of Areo-Engine,Beihang University,Beijing 100191,China
Advanced Aero-Engine Collaborative Innovation Center,Beijing 100191,China
Beijing Institute of Control Engineering,Beijing 100094,China
School of Energy and Power Engineering,Beihang University,Beijing 100191,China
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Abstract

The mechanical properties of ceramic matrix composite structures are predominantly influenced by their micro-scale damage evolution features, given that material failure fundamentally stems from the initiation and progression of microstructural damage. To precisely characterize the micro-damage behavior of composites, multi-scale analysis methods grounded in parameter cross-scale transfer have been extensively employed in the study of composite mechanical properties. Nevertheless, traditional multiscale methods are plagued by low computational efficiency and a geometric increase in computational effort with nested scales, rendering them ill-suited for real-time engineering applications. To tackle this issue, this work puts forward a concurrent multiscale modeling method based on self-consistent clustering analysis. This method utilizes clustering to reduce the dimensionality of the microscale stress/strain field. It substitutes full-scale microscale finite element computations with homogenized response results, thereby substantially enhancing the efficiency of multiscale computations. Numerical results reveal that for both unidirectional and woven composite material cases, the proposed method achieves an overall improvement in computational efficiency of approximately one order of magnitude (10-15 times faster) while keeping computational errors below 3%. By effectively cutting down on computational costs while maintaining high accuracy, this approach provides new insights and technical means for efficient damage analysis and life prediction of composite structures.

CLC number: V254.2 Document code: A Article ID: 1007–7162(2026)9–79–9

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Journal of Aeronautical Materials
Pages 79-87

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Cite this article:
MAO J, WANG G, LIU Y, et al. A concurrent computational method for multiscale damage evolution in ceramic matrix composites based on self-consistent clustering. Journal of Aeronautical Materials, 2026, 46(9): 79-87. https://doi.org/10.11868/j.issn.1005-5053.2025.000237

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Received: 31 December 2025
Accepted: 25 February 2026
Published: 15 September 2026
© Journal of Aeronautical Materials 2026.

This is an open access article under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).