Compressive behavior of composite panels with deeply embedded delamination

被引：0
|
作者：
Fu, Hui-Min [1 ]
Peng, Bo [1 ]
机构：
[1] Research Center of Small Sample Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2012年 / 27卷 / 01期
关键词：
Finite element method - Joints (structural components) - Paper laminates - Delamination - Crack closure;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
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页码：82 / 88
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