Effects of laminate stacking sequence on the free vibration of carbon/epoxy composite plates subjected to in-plane loads

被引：0

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作者：

Attaf, B

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来源：

RECHERCHE AEROSPATIALE | 1996年 / 02期

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中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

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页码：149 / 153

页数：5

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