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Design of Bio-inspired Flexible Wings for Flapping Wing Micro sized Air Vehicle Applications

Title
Design of Bio-inspired Flexible Wings for Flapping Wing Micro sized Air Vehicle Applications
Author
Sunil K.Agrawal
Keywords
Flexible insect wing; finite element analysis; optimization; lift
Issue Date
2009-02
Publisher
VSP BV
Citation
ADVANCED ROBOTICS, v. 23, no. 7/8, page. 979-1002
Abstract
The unmatched performance of insect flight is a motivation for bio-inspired designs of synthetic wings that can undergo large deformations in flapping flight. In this paper, we experimentally study the aerodynamic performance of a bio-inspired flexible flapping wing, which has the static load- deformation characteristics of a hawkmoth (Manduca sexta) wing, and compare it with a similar geometry rigid wing. The bio- inspired wing is designed using finite element analysis, coupled with an optimization solver, to match the static load- deflection characteristics of the synthetic wing with that of real hawkmoth wings. A flexible synthetic wing is constructed using a combination of materials (carbon, nylon and rubber) for the veins and a latex membrane. The aerodynamic performance of the synthetic deformable wing is tested on a robotic flapper, using commonly observed kinematic templates of insect flapping (and rotation). Our results show increased thrust by the flexible wing for all kinematic patterns in comparison to the rigid wing. A host of important advantages provided by wing flexibility are mentioned in the context of flapping flight. (C) Koninklijke Brill NV, Leiden and The Robotics Society of Japan, 2009
URI
https://eds.b.ebscohost.com/eds/detail/detail?vid=0&sid=3193793e-9c20-4dba-9a28-c0b9711bb440%40sessionmgr103&bdata=Jmxhbmc9a28mc2l0ZT1lZHMtbGl2ZQ%3d%3d#AN=41341092&db=a9hhttps://repository.hanyang.ac.kr/handle/20.500.11754/166497
ISSN
0169-1864
DOI
10.1163/156855309X443133
Appears in Collections:
COLLEGE OF ENGINEERING SCIENCES[E](공학대학) > MECHANICAL ENGINEERING(기계공학과) > Articles
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