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

被引：0
|
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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