Journal of Jilin University(Engineering and Technology Edition) ›› 2019, Vol. 49 ›› Issue (5): 1622-1629.doi: 10.13229/j.cnki.jdxbgxb20180430

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Numerical simulation of strain rate effect of fiber reinforced composites

Hui YE(),Yan-rong ZHU,Yong-feng PU   

  1. State Key Laboratory of Automotive Simulation and Control, Jilin University, Changchun 130022, China
  • Received:2018-05-03 Online:2019-09-01 Published:2019-09-11

Abstract:

In order to study the influence of strain rate effect on the simulation precision of fiber reinforced composites, the Dynamic Enhancement Factor (DIF) is introduced to modify the modulus and strength of the composite. The modified Hashin failure criterion is used to establish a three-dimensional progressive damage constitutive model of composite materials, which considers the strain rate effect. The model is embedded into the Abaqus software by VUMAT subroutine, and the simulation of the projectile penetrating the fiberglass reinforced composite laminates is carried out. The simulation results are compared with the experimental results and the simulation results of the constitutive model without considering the strain rate effect. The results show that the constitutive model considering the strain rate effect can accurately simulate the process of projectile penetrating the laminate. Compared with the simulation results without strain rate effect, the accuracy is increased by 14.1% and 22.7% respectively by the proposed model, at the penetration speed of projectile at 1.8 m/s and 3 m/s. In the simulation of the constitutive model without considering the strain rate effect, the error increases from 28.7% to 36.9% as the penetration speed increases from 1.8 m/s to 3 m/s, however, the simulation error of constitutive model considering strain rate effect is relatively stable.

Key words: compound material, strain rate effect, constitutive model, user material subroutine, simulation accuracy

CLC Number: 

  • U465.6

Fig.1

Finite element model of projectile penetrating composite laminates"

Fig.2

Initial state of model"

Fig.3

Intermediate process state of model"

Fig.4

Force-displacement curve of projectile(0.4 mm)"

Table 1

Comparison of maximum contact force"

参 数 试验值 仿真(含应变率) 仿真(不含应变率)
/ N 407.94 348.39 290.87
/ % 14.6 28.7

Fig.5

Force-displacement curve of projectile(0.8 mm)"

Table 2

Comparison of maximum contact force"

参 数 试验值 仿真(含应变率) 仿真(不含应变率)
/ N 925.86 794.37 584.58
/ % 14.2 36.9
1 汤旭, 李征, 孙程阳, 等 . 先进复合材料在航空航天领域的应用[J]. 中国高新技术企业, 2016(13): 39-42.
Tang Xu , Li Zheng , Sun Cheng-yang , et al . Application of advanced composite materials in aerospace[J]. China High Technology Enterprises, 2016(13): 39-42.
2 Abdul-Latif A , Man M H C , Mansor S . Inclusion of strain-rate effects in low velocity impact simulation of laminated composites[J]. Applied Mechanics & Materials, 2014, 465/466: 1395-1399.
3 Zhang X , Hao H , Shi Y , et al . Static and dynamic material properties of CFRP/epoxy laminates[J]. Construction & Building Materials, 2016, 114: 638-649.
4 辛士红 . 纤维增强树脂基复合材料层合板抗侵彻性能数值模拟研究[D]. 合肥: 中国科学技术大学近代力学系, 2015.
Xin Shi-hong . Numerical study on the penetration resistence of fibre reinforced plastic laminates[D]. Hefei: Department of Modern Mechanics, University of Science and Technology of China, 2015.
5 Fan J , Guan Z , Cantwell W J . Modeling perforation in glass fiber reinforced composites subjected to low velocity impact loading[J]. Polymer Composites, 2011, 32(9): 1380-1388.
6 王正浩, 赵桂平, 马君峰, 等 . 碳/环氧树脂复合材料应变率效应的实验研究[J]. 复合材料学报, 2007, 24(2): 113-119.
Wang Zheng-hao , Zhao Gui-ping , Ma Jun-feng , et, al . Experiment study on the strain rate behavior of carbon/epoxy composite materials[J]. Acta Materiae Compositae Sinica, 2007, 24(2): 113-119.
7 Gebbeken N , Greulich S . A new material model for SFRC under high dynamic loadings[C]∥International Confernce on Interaction of the Effects of Munitions with Structures, Mannheim, Germany, 2003: 1-16.
8 Gama B Z , Stanton R J , Gillespie J W . Perforation mechanics of thin composites[C]∥International SAMPE Technical Conference, Long Beach, 2013: 6-9.
9 汪凌云 . 论纤维增强复合材料的失效准则[J]. 纤维复合材料, 1995(1): 1-8.
Wang Ling-yun . The failure criterion of fiber reinforced composite[J]. Fiber Composites, 1995(1): 1-8.
10 Gama B A , Bogetti T A . Progressive damage modeling of plain-weave composites using LS-Dyna composite damage model MAT162[ EB/OL ]. [2009-01-15]. https:∥
11 Jordan J B , Naito C J , Haque B Z . Progressive damage modeling of plain weave E-glass/phenolic composites[J]. Composites Part B: Engineering, 2014, 61: 315-323.
12 Naik N K , Sekher Y C , Meduri S . Damage in woven-fabric composites subjected to low-velocity impact[J]. Composites Science & Technology, 2000, 60(5): 731-744.
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