ANALYSIS OF IMPACT RESPONSE OF BUCKLED COMPOSITE LAMINATES

被引：21

作者：

CHEN, JK

SUN, CT

机构：

[1] Purdue Univ, Sch of Aeronautics, & Astronautics, West Lafayette,, IN, USA, Purdue Univ, Sch of Aeronautics & Astronautics, West Lafayette, IN, USA

来源：

COMPOSITE STRUCTURES | 1985年 / 3卷 / 02期

关键词：

D O I：

10.1016/0263-8223(85)90039-X

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

COMPOSITE MATERIALS

引用

页码：97 / 118

页数：22

共 15 条

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[8] FINITE-ELEMENT ANALYSIS OF GEOMETRICALLY NON-LINEAR PLATE BEHAVIOR USING A MINDLIN FORMULATION [J].

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