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摘要:
In this study,we propose a novel and simple exact semi-analytical model for superelastic Shape Memory Alloy (SMA) wire reinforced composites subjected to bending loads.In order to study the mechanical response of the composite during loading/unloading,a Representative Vol-ume Element (RVE) is extracted to examine the bending response of the composite.Analytical moment-curvature,and shear force-shear strain relations are derived based on a 3-Dimensional(3D) thermomechanical SMA model and Timoshenko beam theory.The composite Simpson's rule is adopted to numerically solve the exact analytical moment-curvature and shear force-shear strain relationships.Results including the moment-curvature response,axial stress distribution along the vertical and longitudinal directions,martensite volume fraction,and the tip deflection are reported and validated against 3D finite element simulations.The influence of temperature,martensite vol-ume fraction distribution,and matrix stiffness on the mechanical performance of the composite is also investigated.In particular,the composite is found to behave superelastically under certain con-ditions of temperature,SMA volume fraction,and elastic stiffness of the matrix.Such behavior is advantageous in applications requiring large recoverable strains or high energy dissipation density.
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篇名 Modeling bending behavior of shape memory alloy wire-reinforced composites:Semi-analytical model and finite element analysis
来源期刊 中国航空学报(英文版) 学科
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年,卷(期) 2021,(8) 所属期刊栏目 Special Topic-Modeling and Simulation in Design and Manufacture of Composite Structures
研究方向 页码范围 176-191
页数 16页 分类号
字数 语种 英文
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中国航空学报(英文版)
月刊
1000-9361
11-1732/V
大16开
北京学院路37号西小楼
80-675
1988
eng
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2997
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