A concept for the generation of out-of-plane distortion from tailored FRP laminates

被引:70
作者
Potter, KD [1 ]
Weaver, PM [1 ]
机构
[1] Univ Bristol, Dept Aerosp Engn, Bristol BS8 1TR, Avon, England
基金
英国工程与自然科学研究理事会;
关键词
residual/internal stress; analytical modelling; prepreg;
D O I
10.1016/j.compositesa.2004.06.022
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The phenomenon of thermally induced distortions in unsymmetrical laminates is well understood, and it may be shown that a square, unsymmetrical 0.90 laminate will tend to form two stable geometries with a snap-through phenomenon between them. This paper discusses laminates in which at each point the lay-up is symmetrical across the laminate mid-plane, but which still exhibit multiple stable geometries. The number of stable geometries can be controlled by the details of the lay-up from the minimum of two to, in principle, an unlimited number. In addition it will be shown how a similar process can be used to generate multiple stable stress states and geometries in unidirectional laminates. This paper represents a very preliminary experimental investigation of the design space available for such composite laminates. Possible applications of composites with multiple stable geometries are noted. (C) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1353 / 1361
页数:9
相关论文
共 11 条
[1]  
Gigliotti M, 2004, COMPOS SCI TECHNOL, V64, P109, DOI 10.1016/S0566-3538(03)00213-6
[2]   Development of curvature during the cure of AS4/8552 [0/90] unsymmetric composite plates [J].
Gigliotti, M ;
Wisnom, MR ;
Potter, KD .
COMPOSITES SCIENCE AND TECHNOLOGY, 2003, 63 (02) :187-197
[3]   SOME OBSERVATIONS ON THE CURED SHAPE OF THIN UNSYMMETRIC LAMINATES [J].
HYER, MW .
JOURNAL OF COMPOSITE MATERIALS, 1981, 15 (MAR) :175-194
[4]  
IQBAL K, 2000, P 4 AIAA ASME ASCE A
[5]   RESIDUAL-STRESS DEVELOPMENT DURING PROCESSING OF GRAPHITE EPOXY COMPOSITES [J].
KIM, KS ;
HAHN, HT .
COMPOSITES SCIENCE AND TECHNOLOGY, 1989, 36 (02) :121-132
[6]  
POTTER KD, 2003, P ICCM14 2003 SAN DI
[7]  
Reddy J. N., 1984, Energy and variational methods in applied mechanics with an introduction to the finite element method
[8]  
SCHLECHT M, 1993, P ECCM SMART COMP WO
[9]  
WEAVER PM, 2002, 43 AIAA ASCE ASME AH
[10]   PROCESS MODELING OF COMPOSITE-MATERIALS - RESIDUAL-STRESS DEVELOPMENT DURING CURE .2. EXPERIMENTAL VALIDATION [J].
WHITE, SR ;
HAHN, HT .
JOURNAL OF COMPOSITE MATERIALS, 1992, 26 (16) :2423-2453