Micromechanical analysis of fiber-reinforced ceramic matrix composites by a hierarchical quadrature element method

被引:7
作者
Xiang, Wei [1 ]
Li, Xin [1 ]
Ni, Hua [1 ]
Liu, Bo [2 ]
机构
[1] Southwest Jiaotong Univ, Sch Mech Engn, Chengdu 610031, Peoples R China
[2] Beihang Univ BUAA, Solid Mech Res Ctr, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Ceramic matrix composites; Micromechanical analysis; Fiber/matrix interface; Differential quadrature method; Hierarchical finite element method; DIFFERENTIAL QUADRATURE; FINITE-ELEMENTS; PLATES; FAILURE; VIBRATION; INTERFACE; FRACTURE; CRACKING; TOUGH; MODEL;
D O I
10.1016/j.compstruct.2022.116143
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This work performed stress predictions of unidirectional fiber-reinforced ceramic matrix composites (CMCs) subjected to longitudinal tension using a hierarchical quadrature element method (HQEM). The HQEM is a p -version finite element method that can present highly accurate results using only a few sampling points. Para-metric analysis was conducted to investigate the sensitivity of the HQEM model to interface properties and the detailed process of determining the optimal interface parameters for micromechanical analysis of damaged CMCs has been elaborated. By comparison with the analytical results based on the classical shear-lag model which is commonly adopted to analyze the stress distributions of the damaged fiber-reinforced CMCs, the HQEM esti-mates of fiber and matrix stress distributions were validated. For uniformly loaded SiCf/SiC composites with a single matrix crack, the micromechanical behaviors of three typical cases during failure process, namely, interface perfectly bonded, interface debonding and fiber failure were analyzed, illustrating the characteristics of CMC failure and providing insight into the mechanisms relating the microstructural behavior to global failure. The present work offers the foundations of the extension of a promising approach for highly accurate and effi-cient fracture analysis of CMCs.
引用
收藏
页数:13
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