Progressive damage of an open-hole NCF/epoxy laminate subjected to tensile load

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作者
Wang, Zhenyu [1 ]
Liu, Ling [1 ]
Gong, Zhanfeng [2 ]
Xue, Yuande [1 ]
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[1] School of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092, China
[2] Shanghai Aircraft Design and Research Institute, Commercial Aircraft Corporation of China, Ltd., Shanghai 201210, China
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页码:147 / 152
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