| 注册
首页|期刊导航|航空材料学报|基于自洽聚类的陶瓷基复合材料多尺度损伤演化并发计算方法

基于自洽聚类的陶瓷基复合材料多尺度损伤演化并发计算方法

毛建兴 王贵灿 刘昱 潘锦超 马鹏辉 刘茜 胡殿印 王荣桥

航空材料学报2026,Vol.46Issue(9):79-87,9.
✕
航空材料学报2026,Vol.46Issue(9):79-87,9.DOI:10.11868/j.issn.1005-5053.2025.000237

基于自洽聚类的陶瓷基复合材料多尺度损伤演化并发计算方法

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

毛建兴 1王贵灿 2刘昱 3潘锦超 1马鹏辉 4刘茜 5胡殿印 1王荣桥5

作者信息

  • 1. 北京航空航天大学 航空发动机研究院,北京 100191||先进航空发动机协同创新中心,北京 100191
  • 2. 北京航空航天大学 航空发动机研究院,北京 100191
  • 3. 北京控制工程研究所,北京 100094
  • 4. 北京航空航天大学 能源与动力工程学院,北京 100191
  • 5. 先进航空发动机协同创新中心,北京 100191||北京航空航天大学 能源与动力工程学院,北京 100191
  • 折叠

摘要

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.

关键词

陶瓷基复合材料/自洽聚类分析/多尺度建模/降阶计算

Key words

ceramic matrix composites/self-consistent clustering analysis/multiscale modeling/reduced order calculation

分类

航空航天

引用本文复制引用

毛建兴,王贵灿,刘昱,潘锦超,马鹏辉,刘茜,胡殿印,王荣桥..基于自洽聚类的陶瓷基复合材料多尺度损伤演化并发计算方法[J].航空材料学报,2026,46(9):79-87,9.

基金项目

国家自然科学基金(52505144) (52505144)

国家科技重大专项(Y2022-IV-0002-0019) (Y2022-IV-0002-0019)

中国博士后科学基金(2024M764101,GZC20252715) (2024M764101,GZC20252715)

中国科学技术协会青年人才托举工程(YESS20241007AE) (YESS20241007AE)

北京市自然科学基金(3252007) (3252007)

中国太行国家实验室项目(THL-K-25-050) (THL-K-25-050)

中央高校基本科研业务费专项资金 ()

航空材料学报

1005-5053

访问量0
|
下载量0
段落导航相关论文