DELAMINATIONS IN COMPOSITE PLATES UNDER TRANSVERSE STATIC OR IMPACT LOADS - A MODEL

被引：63

作者：

FINN, SR

SPRINGER, GS

机构：

[1] Department of Aeronautics and Astronautics, Stanford University, Stanford

来源：

COMPOSITE STRUCTURES | 1993年 / 23卷 / 03期

关键词：

D O I：

10.1016/0263-8223(93)90221-B

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

A method is presented for calculating the locations, shapes, and sizes of delaminations which occur in a fiber reinforced composite plate subjected to transverse static or dynamic (impact) loads. The plate may be simply supported, clamped, or free along its edges. A model of the delamination formation was developed. This model was then coupled with a finite element analysis. The model and the finite element analysis were implemented by a computer code which can be used to estimate the load at which damage is initiated as well as the locations, shapes, and sizes of the delaminations.

引用

页码：177 / 190

页数：14

共 44 条

[1] FINITE-ELEMENT ANALYSIS OF A LAMINATED COMPOSITE PLATE SUBJECTED TO CIRCULARLY DISTRIBUTED CENTRAL IMPACT LOADING [J].