Viscoelastic constitutive model related to deformation of insect wing under loading in flapping motion

被引:19
作者
Bao Lin
Hu Jin-Song
Yu Yong-Liang
Cheng Peng
Xu Bo-Qing
Tong Bing-Gang [1 ]
机构
[1] Grad Univ, Chinese Acad Sci, Lab Biomech Anim Locomot, Beijing 100049, Peoples R China
[2] Univ Sci & Technol, Dept Modern Mech, Hefei 230027, Peoples R China
基金
中国国家自然科学基金;
关键词
constitutive relation; viscoelasticity; stress relaxation; finite element analysis; insect wing; passive deformation;
D O I
10.1007/s10483-006-0604-1
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
Flexible insect wings deform passively under the periodic loading during flapping flight. The wing flexibility is considered as one of the specific mechanisms on improving insect flight performance. The constitutive relation of the insect wing material plays a key role on the wing deformation, but. has not been clearly understood yet. A viscoelastic constitutive relation model was established based on the stress relaxation experiment of a dragonfly wing (in vitro). This model was examined by the finite element analysis of the dynamic deformation response for a model insect wing under the action of the periodical inertial force in flapping. It is revealed that the viscoelastic constitutive relation is rational to characterize the biomaterial property of insect wings in contrast to the elastic one. The amplitude and form of the passive viscoelastic deformation of the wing is evidently dependent on the viscous parameters in the constitutive relation.
引用
收藏
页码:741 / 748
页数:8
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