High velocity impact damage investigation of carbon/epoxy/clay nanocomposites using 3D Computed Tomography

被引:24
作者
Murugan, Pushparaja [1 ]
Naresh, K. [2 ]
Shankar, K. [2 ]
Velmurugan, R. [2 ]
Balaganesan, G. [2 ]
机构
[1] Nanyang Technol Univ, Singapore, Singapore
[2] Indian Inst Technol Madras, Madras, Tamil Nadu, India
关键词
Carbon/epoxy; Nano clay; High velocity impact; Non-destructive testing; Scanning electron microscopy; ENERGY-ABSORPTION CHARACTERISTICS; GLASS/EPOXY COMPOSITES;
D O I
10.1016/j.matpr.2018.04.098
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A series of projectile impact tests have been carried out on cross ply carbon/epoxy and different weight percentages (1%, 3% and 5%) of nanoclay dispersed in the carbon/epoxy laminated composites of two different thicknesses (3 mm and 5 mm) with a 9.8 mm diameter hemispherical shaped mild steel projectile for determining the ballistic limit, residual velocity and energy absorption. Velocities far higher than the ballistic limit such as 165 m/s, 195 m/s and 220 m/s are considered for investigation of damage mechanisms. The traditional CFRP composites show poor impact resistance due to their negligible plastic deformation as compared to metals. The impact performance of these composites can be enhanced by the clay effect. The optimum clay content is proposed in the present investigation. There is a significant improvement in impact properties, as the clay content increases from 0 wt% to 3 wt% but beyond 3 wt% of clay, the properties degrade which is due to the high stress concentrations attributed to the clay clustering in the higher clay content. The X-ray computed tomography (X-ray CT) scanning analysis which is an advanced non-destructive technique (NDT) is used to investigate the internal defects such as delamination and porosity of impact damaged specimens whereas fiber breakage and matrix cracks are seen in scanning electron microscopy (SEM) images. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:16946 / 16955
页数:10
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