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Wing Design and Analysis for Micro Air Vehicle Development

2021-12-29Journal article Embargoed access
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dc.contributor.authorFerreira, Rúben
dc.contributor.authorCamacho, Emanuel
dc.contributor.authorNeves, Fernando M. S. P.
dc.contributor.authorBarata, Jorge M M
dc.contributor.authorSilva, André
dc.date.accessioned2022-04-04T09:46:24Z
dc.date.embargo2060-12-29
dc.date.issued2021-12-29
dc.description.abstractNatural flight was always a source of inspiration to human beings, and by observing it, new technologies emerged, especially in bioinspired aerial vehicle design. The main objective of the present work is to experimentally evaluate the influence of the wing shape on their behavior and power consumption. To accomplish that goal, four wings were selected and an experimental rig was developed. Airflow velocities tested ranged from 0 up to 4 m s−1 with four different throttle positions. Flapping frequency and amplitude were obtained from high-speed camera tests and the power consumption of the wings tested was measured. It is observed that amplitude is between 0.12 m and 0.25 m, frequency between 4 and 15 Hz. Regarding power consumption, the design wings presented lower averaged power-to-weight ratio values when compared to BionicBird wings.pt_PT
dc.description.sponsorshipFundação para a Ciência e a Tecnologiapt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationRúben Ferreira, Emanuel A. Camacho, Fernando P. Neves, Jorge M. M. Barata, André R R Silva Wing Design and Analysis for Micro Air Vehicle Development AIAA SciTech 2022 Forum and Exposition, Evento Hibrido, San Diego, CA, EUA, 3-7 janeiro, 2022pt_PT
dc.identifier.doi10.2514/6.2022-1057pt_PT
dc.identifier.issn978-162410631-6
dc.identifier.urihttp://hdl.handle.net/10400.6/12155
dc.language.isoengpt_PT
dc.peerreviewedyespt_PT
dc.publisherAmerican Institute of Aeronautics and Astronautics Incpt_PT
dc.relationAssociate Laboratory of Energy, Transports and Aeronautics
dc.relation.publisherversionhttps://arc.aiaa.org/doi/abs/10.2514/6.2022-1057pt_PT
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/pt_PT
dc.subjectMicro Air Vehiclept_PT
dc.subjectFlapping Frequencypt_PT
dc.subjectWing Rootpt_PT
dc.subjectAerodynamic Performancept_PT
dc.subjectWing Loadingpt_PT
dc.subjectStructural Analysispt_PT
dc.subjectStructural Designpt_PT
dc.subjectWing Configurationspt_PT
dc.subjectAir Vehiclept_PT
dc.subjectAirfoil Chordpt_PT
dc.titleWing Design and Analysis for Micro Air Vehicle Developmentpt_PT
dc.typejournal article
dspace.entity.typePublication
oaire.awardTitleAssociate Laboratory of Energy, Transports and Aeronautics
oaire.awardURIinfo:eu-repo/grantAgreement/FCT/6817 - DCRRNI ID/UIDB%2F50022%2F2020/PT
oaire.citation.conferencePlaceSan Diego, CA & Virtualpt_PT
oaire.citation.titleAIAA SCITECH 2022 Forumpt_PT
oaire.fundingStream6817 - DCRRNI ID
person.familyNameRodrigues Camacho
person.familyNameSilva Pereira das Neves
person.familyNameMartins Barata
person.familyNameResende Rodrigues da Silva
person.givenNameEmanuel António
person.givenNameFernando Manuel da
person.givenNameJorge Manuel
person.givenNameAndré
person.identifierhFY_5JYAAAAJ&hl
person.identifierJ-4185-2012
person.identifier.ciencia-id4416-08D8-F83D
person.identifier.ciencia-idBC15-D534-3DCC
person.identifier.ciencia-idF611-BBCC-DAA8
person.identifier.ciencia-id8219-4B2B-E1C7
person.identifier.orcid0000-0002-1648-8368
person.identifier.orcid0000-0002-5826-7459
person.identifier.orcid0000-0001-9014-5008
person.identifier.orcid0000-0002-4901-7140
person.identifier.scopus-author-id11439470600
person.identifier.scopus-author-id11440407500
project.funder.identifierhttp://doi.org/10.13039/501100001871
project.funder.nameFundação para a Ciência e a Tecnologia
rcaap.embargofctAmerican Institute of Aeronautics and Astronautics Inc. All rights reserved.pt_PT
rcaap.rightsembargoedAccesspt_PT
rcaap.typearticlept_PT
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