Simulation and Experiment on the Low-Velocity Impact Response of Flax Fabric Reinforced Composites

被引:0
|
作者
Xiong, Xiaoshuang [1 ,2 ]
Wang, Zisheng [2 ]
Zhang, Zihao [2 ]
Li, Qiaomin [1 ,2 ]
Shen, Chen [1 ,2 ]
Fan, Fei [1 ,2 ]
Li, Xiang [3 ]
Chen, Mingzhang [4 ]
机构
[1] Wuhan Text Univ, Hubei Key Lab Digital Text Equipment, Wuhan 430200, Peoples R China
[2] Wuhan Text Univ, Sch Mech Engn & Automat, Wuhan 430200, Peoples R China
[3] China Special Equipment Inspect & Res Inst, Beijing 100029, Peoples R China
[4] Wuhan Univ Technol, Hubei Key Lab Adv Technol Automot Components, Wuhan 430070, Peoples R China
关键词
flax fabric reinforced composites; low-velocity impact; multi-scale; numerical simulation; NATURAL FIBER COMPOSITES; WIND TURBINE BLADE; GREEN COMPOSITES; BEHAVIOR; COMPRESSION; DESIGN; DAMAGE; STRENGTH; DENSITY;
D O I
10.3390/ma16093489
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Natural fiber reinforced composites are increasingly used to fabricate structural components prone to suffering low-velocity impacts. The low-velocity impact response of flax fabric reinforced composites under different impact energies is experimentally studied and numerically simulated. A multi-scale finite element analysis strategy for the progressive damage prediction of flax fabric reinforced composites is developed. Micro- and meso-scale analyses are conducted to predict the effective properties of the woven unit cell. Macro-scale analysis is carried out subsequently to predict the impact response of composite laminates using the results of micro- and meso-scale analyses as inputs. Simulation results and experimental results both show that most of the impact energy is absorbed by the specimens when the impact energy is lower than 4 J, and the absorption ratio of impact energy slightly increases with the increase in impact energy. On the contrary, a dramatic decrease occurs in the absorption ratio when the impact energy is 6 J, due to the severe damage to the specimen. In addition, simulation results indicate that matrix shear damage and interlaminar damage are the primary failure modes of composites under high impact energy. The numerical results of impact force, absorbed energy, and damage morphologies on both sides for all specimens show good agreement with the experimental results.
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页数:16
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