有限元法
凯夫拉
弹道极限
复合数
有效载荷(计算)
结构工程
材料科学
航空航天
环氧树脂
耐久性
数值分析
复合材料
计算机模拟
工程类
计算机科学
射弹
航空航天工程
数学
计算机网络
数学分析
网络数据包
冶金
模拟
作者
Yehia Abdel-Nasser,Ahmed M.H. Elhewy,Islam Almallah
标识
DOI:10.1080/17445302.2015.1131005
摘要
AbstractComposite materials of various types and forms have become important engineering solutions for the construction of a range of mechanical, aerospace and marine structures. The use of laminated composite materials in fabricating these structures has resulted in a significant increase in payload, weight reduction, speed, fire resistance, maneuverability and durability. This paper addresses the numerical simulation of ballistic impact of composite laminated plates, using finite element method (FEM). The aim of this work is to determine the ballistic limit velocity when changing the lay-up of the laminated plate. These changes can be virtually done by numerical simulation using FEM. Two different models utilising E glass fibre/reinforced epoxy are developed to validate the numerical results at low and high impact velocities. After validating numerical results, different materials such as kevlar and carbon composites are utilised in order to investigate the ballistic impact analysis of the composite laminate. The results of analyses are presented and their trends are discussed.Keywords: composite materialslaminated plateimpact analysisfinite element analysis Disclosure statementNo potential conflict of interest was reported by the authors.
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