Instability analysis of a filament-wound composite tube subjected to compression/bending

被引:1
作者
Szabo, Gyula [1 ]
Varadi, Karoly [1 ]
机构
[1] Budapest Univ Technol & Econ, Dept Machine & Prod Design, 1-3 Mu Egyet Quai, H-1111 Budapest, Hungary
关键词
filament-wound composite tube; thick-walled tube; finite element analysis; bending load; buckling; cross-section instability; SHEAR; PRESSURE; TENSILE; TORSION; DAMAGE;
D O I
10.1177/0963693519877417
中图分类号
TB33 [复合材料];
学科分类号
摘要
The aim of this study is to investigate the global buckling of a relatively long composite cord-rubber tube subjected to axial compression and its cross-sectional instability due to bending by a macromechanical nonlinear finite element (FE) model (nonlinear buckling analysis). Composite reinforcement layers are modelled as transversely isotropic ones, while elastomer liners are described by a hyperelastic material model that assumes incompressibility. Force-displacement, equivalent strain, equivalent stress results along with oblateness and curvature results for the complete process have been presented. It is justified that bending leads to ovalization of the cross section and results in a loss of the load-carrying capacity of the tube. Strain states in reinforcement layers have been presented, which imply that the probable failure modes of the reinforcement layers are both delamination and yarn-matrix debonding. There is a significant increase in strains due to cross-sectional instability, which proves that the effect of cross-sectional instability on material behaviour of the tube is crucial. A parametric analysis has been performed to investigate the effect of the member slenderness ratio on cross-sectional instability of the composite tube. It shows that Brazier force is inversely proportional to the slenderness ratio. It further shows that higher oblateness parameters occur in case of a lower slenderness ratio and that cross-sectional instability takes place at a lower dimensionless displacement in case of a lower slenderness ratio. FE results have been validated by a compression/bending test experiment conducted on a tensile test machine.
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页数:13
相关论文
共 31 条
[1]  
adany S, 2017, THESIS
[2]   Flexural stiffness of thick walled composite tubes [J].
Ahmad, M. I. Geuchy ;
Hoa, S. V. .
COMPOSITE STRUCTURES, 2016, 149 :125-133
[3]   Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [J].
Almeida, Jose Humberto S., Jr. ;
Bittrich, Lars ;
Jansen, Eelco ;
Tita, Volnei ;
Spickenheuer, Axel .
COMPOSITE STRUCTURES, 2019, 222
[4]   Buckling and post-buckling of filament wound composite tubes under axial compression: Linear, nonlinear, damage and experimental analyses [J].
Almeida, Jose Humberto S., Jr. ;
Tonatto, Maikson L. P. ;
Ribeiro, Marcelo L. ;
Tita, Volnei ;
Amico, Sandro C. .
COMPOSITES PART B-ENGINEERING, 2018, 149 :227-239
[5]   Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [J].
Almeida, Jose Humberto S., Jr. ;
Ribeiro, Marcelo L. ;
Tita, Volnei ;
Amico, Sandro C. .
COMPOSITE STRUCTURES, 2017, 178 :20-26
[6]   Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [J].
Almeida, Jose Humberto S., Jr. ;
Ribeiro, Marcelo L. ;
Tita, Volnei ;
Amico, Sandro C. .
COMPOSITE STRUCTURES, 2017, 160 :204-210
[7]  
[Anonymous], 2011, 158072011 BSI DIN EN
[8]   Experimental and numerical study of adhesively bonded ±55○ filament wound tubular specimens under uniaxial tensile loading [J].
Braiek, Sonia ;
Zitoune, Redouane ;
Ben Khalifa, Ated ;
Zidi, Mondher .
COMPOSITE STRUCTURES, 2017, 172 :297-310
[10]  
CALLEDINE CR, 1983, THEORY SHELL STRUCTU