Progressive Failure Analysis and Experimental Verification of L-Shaped Composite with Initial Defects

被引:0
作者
Xie, Jiawen [1 ]
Chai, Yijun [1 ]
Zhou, Junchen [1 ]
Yang, Xiongwei [1 ]
Li, Yueming [2 ]
机构
[1] Xi An Jiao Tong Univ, Sch Aerosp Engn, State Key Lab Strength & Vibrat Mech Struct, Shaanxi Key Lab Environm & Control Flight Vehicle, 28 Xianning West Rd, Xian 710049, Peoples R China
[2] Xi An Jiao Tong Univ, State Key Lab Strength & Vibrat MechanicalStructur, Shaanxi Key Lab Environm & Control Flight Vehicle, 28 Xianning West Rd, Xian 710049, Peoples R China
基金
国家重点研发计划; 中国博士后科学基金;
关键词
Composite Structures; Stress Concentration; Finite Element Analysis; Composite Laminates; Mechanical Properties; Fracture Mechanics; Machine Learning; Stress-Strain Analysis; Convolutional Neural Network; Image Segmentation; FINITE-ELEMENT-ANALYSIS; COMPUTED-TOMOGRAPHY; DAMAGE EVOLUTION; BRAIDED COMPOSITE; BEHAVIOR; SIMULATION; PREDICTION; CRITERIA; MODELS; FEM;
D O I
10.2514/1.J062613
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Initial defects such as microcracks and pores inevitably exist during the fabrication of carbon fiber composites, which can affect design properties of the composites, resulting in loss of structural mechanical performance. In this paper, we develop an approach with which structure failure can be effectively predicated through exact modeling of composite materials. Specially, an L-shaped composite structure with the initial defects is considered. Its macroscopic properties are obtained through an exact 3D finite element model based on Computed Tomography (CT) images of the composite material, in which the fiber orientations are determined through the machine learning. Numerical prediction of the structure failure is then conducted based on 3D-Hashin failure criterion and bilinear cohesive model, which is in good agreement with experiments. Both results show that crack initiation occurs in the defect dense area, and the structure failure is mainly caused by fiber fracture. Based on the validated approach, we further discuss the mechanical properties of the structure without defects, and found that 2% initial defects in the model can lead to a 12% reduction of the bearing capacity. We expect that our failure analysis approach can be critically useful in designing composite materials and structures.
引用
收藏
页码:3618 / 3632
页数:15
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