期刊
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING
卷 125, 期 -, 页码 180-187出版社
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.ijimpeng.2018.11.011
关键词
Fibre metal laminate; FML; Titanium; Carbon-fibre; Composite; Progressive failure; Terminal ballistics; Armour
Titanium and carbon-fibre reinforced epoxy fibre metal laminates (FMLs) are investigated to determine their potential as a mass efficient passive armour for countering the threat of explosively formed projectiles (EFPs) travelling in the region of 2000 m/s. A proposed methodology for predicting the effect of the impact is presented, together with the results from test shots. There is good correlation between the predictions and the test results. The tests show that the failure modes of the composite material constituent are influenced by the lamination sequence. The tests also show that one of the contributory mechanisms to the failure in the titanium is the formation of adiabatic shear bands.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据