Buckling and Postbuckling of a Delaminated Composite Beam in Bending

被引:8
作者
Kinawy, M. [1 ]
Butler, R. [1 ]
Hunt, G. W. [1 ]
机构
[1] Univ Bath, Dept Mech Engn, Bath BA2 7AY, Avon, England
关键词
BEHAVIOR; PLATES;
D O I
10.2514/1.J050784
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A study was conducted to model the thin delaminated layer using the Elastica theory and investigate the postbuckling behavior for a delaminated beam under compression. Static tests were performed to understand the buckling and propagation behavior of 16-ply, laminated beams with a through-width delamination created by a polytetrafluoroethylene (PTFE) layer of 0.02 mm thickness and 40 mm length placed at the mid length of the beam between the second and third ply. A unidirectional plate made of M21-T800 carbon material was laid up and cured using an autoclave. An INSTRON-1332 servo-hydraulic machine with 10 kN load cell was used for loading application. The strain gauges and loading channel from the servo-hydraulic machine were connected to a SPIDER-8 data acquisition system which was attached to a PC. The specimens were also loaded through a four point bending fixture under displacement control.
引用
收藏
页码:670 / 672
页数:3
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