A novel centresymmetric honeycomb composite structure

被引:122
作者
Bezazi, A
Scarpa, F
Remillat, C
机构
[1] Univ Sheffield, Dept Mech Engn, Multidomain Cellular Solids Lab, Sheffield S1 3JD, S Yorkshire, England
[2] Univ Bristol, Dept Aerosp Engn, Bristol BS8 2QL, Avon, England
基金
英国工程与自然科学研究理事会;
关键词
auxetic; honeycomb; mechanical properties; young's moduli; Poisson's ratio; finite element; analytical model; DESIGN;
D O I
10.1016/j.compstruct.2005.09.035
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this paper analytical and finite element (FE) simulations are carried out to calculate the in-plane Poisson's ratio and Young's moduli of a new centresymmetric honeycomb configuration under uniaxial loading. Opposite to similar re-entrant honeycomb structures studied in the past, the new re-entrant unit cell topology takes into account possible manufacturing constraints typical of production routes like Resin Transfer Moulding (RTM) or Rapid Prototyping (RP). The results obtained through the analytical and FE analysis show a significant decrease of the Poisson's ratio for the internal cell angle between -20 degrees and +20 degrees compared to the classical re-entrant configurations exhibited in literature. The results also show that the presence of edge corners in the unit cell honeycomb configuration gives rise to a cellular structure with enhanced flexibility compared to the classical centresymmetric one. The results obtained by the analytical model show good agreement with the Gibson and Ashby rib-bending model when the honeycomb configuration reduces to the theoretical layout without modifications due to manufacturing constraints. (C) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:356 / 364
页数:9
相关论文
共 11 条
[1]  
Ashby MF., 1997, CELLULAR SOLIDS STRU, DOI DOI 10.1017/CBO9781139878326
[2]  
BEZAZI A, 2004, C INT MEC AV CIMA 04
[3]   Functionally graded beam for attaining Poisson-curving [J].
Lim, TC .
JOURNAL OF MATERIALS SCIENCE LETTERS, 2002, 21 (24) :1899-1901
[4]   Models for the elastic deformation of honeycombs [J].
Masters, IG ;
Evans, KE .
COMPOSITE STRUCTURES, 1996, 35 (04) :403-422
[5]   Numerical and experimental uniaxial loading on in-plane auxetic honeycombs [J].
Scarpa, F ;
Panayiotou, P ;
Tomlinson, G .
JOURNAL OF STRAIN ANALYSIS FOR ENGINEERING DESIGN, 2000, 35 (05) :383-388
[6]   Design of smart composite materials using topology optimization [J].
Sigmund, O ;
Torquato, S .
SMART MATERIALS & STRUCTURES, 1999, 8 (03) :365-379
[7]  
*SWANS INC, 1998, ANSYS REL 5 4 US MAN
[8]   Towards the design of sandwich panel composites with enhanced mechanical and thermal properties by variation of the in-plane Poisson's ratios [J].
Whitty, JPM ;
Alderson, A ;
Myler, P ;
Kandola, B .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2003, 34 (06) :525-534
[9]   On auxetic materials [J].
Yang, W ;
Li, ZM ;
Shi, W ;
Xie, BH ;
Yang, MB .
JOURNAL OF MATERIALS SCIENCE, 2004, 39 (10) :3269-3279
[10]  
Zenkert D., 1997, HDB SANDWICH CONSTRU