The effect of specimen thickness on the shock propagation along the in-fibre direction of an aerospace-grade CFRP laminate

被引:35
作者
Hazell, P. J. [1 ]
Stennett, C. [1 ]
Cooper, G. [1 ]
机构
[1] Cranfield Univ, DCMT, Swindon SN6 8LA, Wilts, England
基金
英国工程与自然科学研究理事会;
关键词
Carbon fibre; Impact behaviour; Shock response; WOVEN CARBON/EPOXY COMPOSITES; VELOCITY STEEL SPHERE; STRAIN-RATE; REINFORCED POLYMERS; EPOXY COMPOSITE; IMPACT; BEHAVIOR; PERFORMANCE; COMPRESSION; ORIENTATION;
D O I
10.1016/j.compositesa.2008.11.002
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In-fibre measurements of the Hugoniot have been carried out on a carbon fibre-reinforced polymer composite. For this material, we have shown at high shock stresses, a two component wave was formed consisting of a fast moving ramped portion and a slower moving shock wave. Changing the thickness of test specimen for a given shock stress resulted in a change in the magnitude and duration of the ramped portion of the wave front. As the shock stress imparted to the target was reduced, or the thickness of the target was increased, the steep shock wave in the rear surface gauge was no longer apparent. Instead a relatively slow rising wave was measured. Consequently, to establish a Hugoniot at lower shock stress levels, relatively thin specimens of target material are required. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:204 / 209
页数:6
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