Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures

出版年份 2016 全文链接

标题

作者

关键词

Carbon fibre, Damage tolerance, Finite element analysis (FEA), Joints/joining

出版物

COMPOSITES PART B-ENGINEERING

Volume 100, Issue -, Pages 68-77

出版商

Elsevier BV

发表日期

2016-06-22

DOI

10.1016/j.compositesb.2016.06.061

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