Experimental and numerical investigation of aramid fibre reinforced laminates subjected to low velocity impact

被引:58
作者
Yang, Lei [1 ]
Yan, Ying [1 ]
Kuang, Naihang [2 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
[2] Harbin FRP Inst, Harbin 150036, Peoples R China
关键词
Aramid fibre; Laminates; Low velocity impact; Finite element analysis (FEA); PROGRESSIVE FAILURE MODEL; BALLISTIC PERFORMANCE; THICKNESS; COMPOSITES; MECHANISMS; BEHAVIOR; DAMAGE;
D O I
10.1016/j.polymertesting.2013.07.010
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The low velocity impact performance of domestic aramid fibre reinforced laminates is investigated experimentally and numerically. Laminates with different thicknesses are impacted by drop-weight test machine under different impact energies. The time histories of impact force are recorded and ultrasonic C-scan technology is used to inspect the internal damage of the laminates. Numerical simulation is conducted using finite element method (FEM), taking into account both intralaminar and interlaminar damage. The intralaminar damage model is based on the continuum damage mechanics (CDM) approach, which consists of the strain-based Hashin failure criteria and the exponential damage evolution law, and considers the nonlinear shear behaviour of the material. The interlaminar damage is simulated by interface elements with cohesive zone model. The numerical results show good agreements with the experiments, thus verifying the validity of the presented numerical model. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1163 / 1173
页数:11
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