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
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关键词
Finite element method - Joints (structural components) - Paper laminates - Delamination - Crack closure;
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页码:82 / 88
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