The impact performance of Vectran/Epoxy composite laminates with a novel non-crimp fabric architecture

被引:9
|
作者
Abdullah, S. I. B. Syed [1 ]
Iannucci, L. [1 ]
Greenhalgh, E. S. [1 ]
Ahmad, Z. [2 ]
机构
[1] Imperial Coll London, Dept Aeronaut, Exhibit Rd, London SW7 2AZ, England
[2] Univ Teknol Malaysia, Fac Engn, Sch Mech Engn, Johor Baharu 81310, Malaysia
关键词
Low velocity impact (LVI); High velocity impact (HVI); Fracture toughness; Non-crimp fabrics (NCFs); Delamination; MECHANICAL-PROPERTIES; COMPRESSION; RESISTANCE; FAILURE; FIBERS;
D O I
10.1016/j.compstruct.2021.113784
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The present research aims to evaluate the impact performance of novel non-crimp fabrics Vectran/Epoxy composite laminates under low and high velocity impact loading conditions. Extensive experimental works consisting of low and high velocity impact tests have been conducted to examine the load-deflection response and the damage mechanism. The impact performance is also compared with GF/Epoxy laminates, having similar fabric architecture and areal weight. Superior impact response was observed for Vectran/Epoxy under both velocity regimes, mainly due to the fabric architecture and fibre properties. It is evident that the results from this work may be beneficial and useful as a secondary component or reinforcement where impact protection is required.
引用
收藏
页数:17
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