Composites airframe panel design for post-buckling – An experimental investigation

出版年份 2020 全文链接

标题

作者

关键词

Composite stiffened panel, Compression load, Delamination, Disbond, Impact damage

出版物

Volume 241, Issue -, Pages 112104

出版商

Elsevier BV

发表日期

2020-02-23

DOI

10.1016/j.compstruct.2020.112104

联系作者

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