A multi-scale modeling framework for impact damage simulation of triaxially braided composites

被引:103
作者
Zhao, Zhenqiang [1 ,2 ,3 ]
Dang, Haoyuan [1 ,2 ,3 ]
Zhang, Chao [1 ,2 ,3 ]
Yun, Gun Jin [4 ]
Li, Yulong [1 ,2 ,3 ]
机构
[1] Northwestern Polytech Univ, Dept Aeronaut Struct Engn, Xian 710072, Shaanxi, Peoples R China
[2] Shaanxi Key Lab Impact Dynam & Its Engn Applicat, Xian 710072, Shaanxi, Peoples R China
[3] Joint Int Res Lab Impact Dynam & Its Engn Applica, Xian 710072, Shaanxi, Peoples R China
[4] Seoul Natl Univ, Dept Mech & Aerosp Engn, Seoul 08826, South Korea
关键词
Polymer-matrix composites (PMCs); Impact behavior; Finite element analysis (FEA); Multi-scale model; TEXTILE COMPOSITES; STRENGTH PREDICTION; PROGRESSIVE DAMAGE; ULTIMATE STRENGTH; FAILURE; COMPRESSION; STIFFNESS;
D O I
10.1016/j.compositesa.2018.04.020
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A multi-scale simulation framework based on finite element method is developed to model the impact failure behavior of triaxially braided composite. The model integrates micromechanical model, meso-mechanical model and macro subcell model for the purpose of determining effective properties of fiber tows, estimating effective properties of subcell components, and simulating impact failure behavior of a braided composite structure, respectively. The meso-mechanical model compares excellently with experiments for mechanical behavior of both single-layer and six-layer specimens under quasi-static loading conditions. A new meso-macro homogenization approach is proposed to estimate effective properties of subcell components with consideration of geometry continuity effect. The subcell model is validated against experiments and utilized to simulate the highspeed impact behavior of a composite panel. The results of the subcell impact model compare well with experimental failure phenomena. The presented multi-scale modeling approach demonstrates its feasibility for impact analysis and design of braided composite structures.
引用
收藏
页码:113 / 125
页数:13
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