Assessment of delamination fracture load of stringer stiffened composite panel

被引：2
|
作者：
Kumar, RR [1 ]
Praveen, KS [1 ]
Rao, GV [1 ]
机构：
[1] Vikram Sarabhai Space Ctr, Struct Engn Grp, Thiruvananthapuram 695022, Kerala, India
来源：
AIAA JOURNAL | 2003年 / 41卷 / 03期
关键词：
D O I：
10.2514/2.1982
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：551 / 554
页数：4
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