Viscoelastic constitutive model related to deformation of insect wing under loading in flapping motion
文献类型：期刊论文
| 作者 | Bao, L; Hu, JS; Yu, YL; Cheng, P; Xu, BQ; Tong, BG |
| 刊名 | Applied mathematics and mechanics-english edition
 |
| 出版日期 | 2006-06-01 |
| 卷号 | 27期号:6页码:741-748 |
| 关键词 | Constitutive relation Viscoelasticity Stress relaxation Finite element analysis Insect wing Passive deformation |
| ISSN号 | 0253-4827 |
| DOI | 10.1007/s10483-006-0604-1 |
| 通讯作者 | Tong, bg() |
| 英文摘要 | 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. |
| WOS关键词 | HAWKMOTH MANDUCA-SEXTA ; FUNCTIONAL-MORPHOLOGY ; FLIGHT ; AERODYNAMICS ; KINEMATICS |
| WOS研究方向 | Mathematics ; Mechanics |
| WOS类目 | Mathematics, Applied ; Mechanics |
| 语种 | 英语 |
| WOS记录号 | WOS:000238366800004 |
| 出版者 | SHANGHAI UNIV |
| URI标识 | http://www.irgrid.ac.cn/handle/1471x/2379299 |
| 专题 | 中国科学院大学 |
| 通讯作者 | Tong, BG |
| 作者单位 | 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 |
| 推荐引用方式 GB/T 7714 | Bao, L,Hu, JS,Yu, YL,et al. Viscoelastic constitutive model related to deformation of insect wing under loading in flapping motion[J]. Applied mathematics and mechanics-english edition,2006,27(6):741-748. |
| APA | Bao, L,Hu, JS,Yu, YL,Cheng, P,Xu, BQ,&Tong, BG.(2006).Viscoelastic constitutive model related to deformation of insect wing under loading in flapping motion.Applied mathematics and mechanics-english edition,27(6),741-748. |
| MLA | Bao, L,et al."Viscoelastic constitutive model related to deformation of insect wing under loading in flapping motion".Applied mathematics and mechanics-english edition 27.6(2006):741-748. |
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来源：中国科学院大学
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