POSTBUCKLING RESPONSE AND FAILURE PREDICTION OF GRAPHITE-EPOXY PLATES LOADED IN COMPRESSION

被引：64

作者：

ENGELSTAD, SP

REDDY, JN

KNIGHT, NF

机构：

[1] VIRGINIA POLYTECH INST & STATE UNIV, DEPT ENGN SCI & MECH, BLACKSBURG, VA 24061 USA

[2] CLEMSON UNIV, DEPT MECH ENGN, CLEMSON, SC 29634 USA

来源：

AIAA JOURNAL | 1992年 / 30卷 / 08期

基金：

美国国家航空航天局;

关键词：

D O I：

10.2514/3.11187

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The objective of the study is to predict the postbuckling response and failure modes of various graphite-epoxy panels loaded in axial compression. A shear deformable (three-dimensional) shell element is used to analyze the panels. Two panels without holes and one with a hole are studied, and the resulting responses and failure modes correlated well with the experimental results. A progressive damage failure mechanism is applied in the nonlinear analysis, which proved successful in predictions of failure location, mode, and load.

引用

页码：2106 / 2113

页数：8

共 7 条

[1] ANALYSIS OF LAMINATED COMPOSITE SHELLS USING A DEGENERATED 3-D ELEMENT [J].