Compression behaviour of flat stiffened panels made of composite material

被引：6
作者：
Chiarelli, M
Lanciotti, A
Lazzeri, L
机构：
[1] Dipartimento Ing. Aerospaziale, University of Pisa, 56126 Pisa
来源：
COMPOSITE STRUCTURES | 1996年 / 36卷 / 1-2期
关键词：
D O I：
10.1016/S0263-8223(96)00075-X
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
In certain structural applications, such as stiffened panels loaded in compression, a better exploitation of the properties of composite materials requires the development of design methodologies that allow the component to work in the post-critical range. This paper describes the results of a research activity with such an objective, carried out at the Department of Aerospace Engineering of the University of Pisa in collaboration with Alenia-Transport Aircraft Group. A group of tests has been carried out on 10 flat stiffened panels, made in composite material, and the results have been analysed with two computer codes, providing useful information concerning their capabilities. (C) 1997 Elsevier Science Ltd.
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页码：161 / 169
页数：9
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