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	A numerical method for the ballistic performance prediction of the sandwiched open cell aluminum foam under hypervelocity impact
	Zhang, Xiaotian; Wang, Ruiqing; Liu, Jiaxin; Li, Xiaogang; Jia, Guanghui
刊名	AEROSPACE SCIENCE AND TECHNOLOGY
	2018
卷号	75页码:254-260
关键词	Aluminum foam Hypervelocity impact Stress wave Voronoi tessellation SPH
ISSN号	1270-9638
DOI	10.1016/j.ast.2017.12.034
URL标识	查看原文
收录类别	SCIE ; EI
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5935192
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Zhang, Xiaotian,Wang, Ruiqing,Liu, Jiaxin,et al. A numerical method for the ballistic performance prediction of the sandwiched open cell aluminum foam under hypervelocity impact[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2018,75:254-260.
APA	Zhang, Xiaotian,Wang, Ruiqing,Liu, Jiaxin,Li, Xiaogang,&Jia, Guanghui.(2018).A numerical method for the ballistic performance prediction of the sandwiched open cell aluminum foam under hypervelocity impact.AEROSPACE SCIENCE AND TECHNOLOGY,75,254-260.
MLA	Zhang, Xiaotian,et al."A numerical method for the ballistic performance prediction of the sandwiched open cell aluminum foam under hypervelocity impact".AEROSPACE SCIENCE AND TECHNOLOGY 75(2018):254-260.

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