Crushing of conical composites shells: a numerical analysis of the governing factors

被引：14
|
作者：
Morthorst, M [1 ]
Horst, P [1 ]
机构：
[1] Tech Univ Carolo Wilhelmina Braunschweig, Inst Aircraft Design & Lightweight Struct, D-38108 Braunschweig, Germany
来源：
AEROSPACE SCIENCE AND TECHNOLOGY | 2006年 / 10卷 / 02期
关键词：
composites; crash; material model; multi-layered modelling;
D O I：
10.1016/j.ast.2005.10.001
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A numerical and experimental analysis comparing the influence of specimen geometry, material composition and loading conditions on the crushing response of truncated conical shells is presented. The analysis is based on a new multi-layered numerical modelling composed of shell and solid elements. A material model appropriate for balanced fabrics has been developed including in-plane failure, delamination failure and resulting degradation models. (c) 2005 Published by Elsevier SAS.
引用
收藏
页码：127 / 135
页数：9
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