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dc.contributor.authorSunil K.Agrawal-
dc.date.accessioned2021-11-30T00:53:02Z-
dc.date.available2021-11-30T00:53:02Z-
dc.date.issued2009-02-
dc.identifier.citationADVANCED ROBOTICS, v. 23, no. 7/8, page. 979-1002en_US
dc.identifier.issn0169-1864-
dc.identifier.urihttps://eds.b.ebscohost.com/eds/detail/detail?vid=0&sid=3193793e-9c20-4dba-9a28-c0b9711bb440%40sessionmgr103&bdata=Jmxhbmc9a28mc2l0ZT1lZHMtbGl2ZQ%3d%3d#AN=41341092&db=a9h-
dc.identifier.urihttps://repository.hanyang.ac.kr/handle/20.500.11754/166497-
dc.description.abstractThe 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, 2009en_US
dc.description.sponsorshipThis work was supported by National Science Foundation Grant numbers 0705419 and 0625367. This research was also supported by WCU (World Class University) program through the Korea Science and Engineering Foundation funded by the Ministry of Education, Science and Technology (No. R32-2008-000-10022-0). We sincerely thank Zaeem Khan for help during flapper experiments and insightful comments of the reviewers.en_US
dc.language.isoen_USen_US
dc.publisherVSP BVen_US
dc.subjectFlexible insect wingen_US
dc.subjectfinite element analysisen_US
dc.subjectoptimizationen_US
dc.subjectliften_US
dc.titleDesign of Bio-inspired Flexible Wings for Flapping Wing Micro sized Air Vehicle Applicationsen_US
dc.typeArticleen_US
dc.identifier.doi10.1163/156855309X443133-
dc.relation.journalADVANCED ROBOTICS-
dc.contributor.googleauthorAgrawal, Arun-
dc.contributor.googleauthorAgrawal, Sunil K.-
dc.relation.code2009200214-
dc.sector.campusE-
dc.sector.daehakCOLLEGE OF ENGINEERING SCIENCES[E]-
dc.sector.departmentDEPARTMENT OF MECHANICAL ENGINEERING-
dc.identifier.pidagrawal-
Appears in Collections:
COLLEGE OF ENGINEERING SCIENCES[E](공학대학) > MECHANICAL ENGINEERING(기계공학과) > Articles
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