On the vein-stiffening membrane structure of a dragonfly hind wing
On the vein-stiffening membrane structure of a dragonfly hind wing作者机构:Institute of Structural Engineering Zhejiang University Hangzhou 310058 China Department of Mechanical and Aerospace Engineering University of Florida Gainesville FL 32611 USA
出 版 物:《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 (浙江大学学报(英文版)A辑(应用物理与工程))
年 卷 期:2009年第10卷第1期
页 面:72-81页
核心收录:
学科分类:0810[工学-信息与通信工程] 12[管理学] 1201[管理学-管理科学与工程(可授管理学、工学学位)] 08[工学] 080203[工学-机械设计及理论] 0805[工学-材料科学与工程(可授工学、理学学位)] 0802[工学-机械工程] 0812[工学-计算机科学与技术(可授工学、理学学位)] 080201[工学-机械制造及其自动化]
基 金:Project supported by the National Natural Science Foundation of China(No. 50408022) the Visiting Scholarship from the Future Academic Star Project of Zhejiang University the Scientific Research Foundation for the Returned Overseas Chinese Scholars,MOE and Zhejiang Province,China
主 题:Dragonfly wing Venation pattern Wing membrane Pterostigma Bionics Quivering effect
摘 要:Aiming at exploring the excellent structural performance of the vein-stiffening membrane structure of dragonfly hind wings,we analyzed two planar computational models and three 3D computational models with cambered corrugation based on the finite element *** is shown that the vein size in different zones is proportional to the magnitude of the vein internal force when the wing structure is subjected to uniform out-of-plane transverse *** membrane contributes little to the flexural stiffness of the planar wing models,while exerting an immense impact upon the stiffness of the 3D wing models with cambered *** a lumped mass of 10% of the wing is fixed on the leading edge close to the wing tip,the wing fundamental fre-quency decreases by 10.7%~13.2%;if a lumped mass is connected to the wing via multiple springs,the wing fundamental fre-quency decreases by 16.0%~18.0%.Such decrease in fundamental frequency explains the special function of the wing pterostigma in alleviating the wing quivering *** particular features of dragonfly wings can be mimicked in the design of new-style reticulately stiffening thin-walled roof systems and flapping wings in novel intelligent aerial vehicles.