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Design and Testing of a Wing with a Morphing Trailing Edge

dc.contributor.authorPinho, João
dc.contributor.authorCamacho, Emanuel A. R.
dc.contributor.authorSilva, A. R. R.
dc.date.accessioned2023-06-12T10:19:10Z
dc.date.embargo2060-06-08
dc.date.issued2023-06-08
dc.description.abstractIn recent years, the interest in morphing technologies has been continuously growing. Many designs have been developed, but some are very complex to manufacture. The main goal of this paper is to present a wing design with a morphing trailing edge that is easy to manufacture and control while allowing the execution of appropriate aerodynamic studies in wind tunnel. Using computer-aided design and 3D printing, a wing that is easily controlled with easy-to-use hardware is developed, manufactured, and studied using flow visualization and force acquisition. Flow visualization showed that the presence of curvature delays stall occurrence when compared to the symmetrical configuration, where flow separation starts right at the leading edge. This is validated by force measurements where curvature plays an important role regarding lift enhancement. This design will allow for a wider range of studies, including unsteady conditions, which can offer insights concerning aerodynamic surfaces design.pt_PT
dc.description.sponsorshipFundação para a Ciência e a Tecnologiapt_PT
dc.description.versioninfo:eu-repo/semantics/publishedVersionpt_PT
dc.identifier.citationJoão Pinho, Emanuel A. Camacho and Andre R. Silva, "Design and Testing of a Wing with a Morphing Trailing Edge", AIAA AVIATION 2023 Forum, 12-16 June 2023, San Diego, CA and Online, DOI: 10.2514/6.2023-3752pt_PT
dc.identifier.doi10.2514/6.2023-3752pt_PT
dc.identifier.urihttp://hdl.handle.net/10400.6/13357
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.relationBoundary Layer Control in Plunging and Pitching Airfoils
dc.relation.publisherversionhttps://arc.aiaa.org/doi/10.2514/6.2023-3752pt_PT
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/pt_PT
dc.subject3D printingpt_PT
dc.subjectMorphingpt_PT
dc.subjectWingpt_PT
dc.subjectTrailing edgept_PT
dc.titleDesign and Testing of a Wing with a Morphing Trailing Edgept_PT
dc.typeconference object
dspace.entity.typePublication
oaire.awardTitleAssociate Laboratory of Energy, Transports and Aeronautics
oaire.awardTitleBoundary Layer Control in Plunging and Pitching Airfoils
oaire.awardURIinfo:eu-repo/grantAgreement/FCT/6817 - DCRRNI ID/UIDB%2F50022%2F2020/PT
oaire.awardURIinfo:eu-repo/grantAgreement/FCT/POR_CENTRO/2020.04648.BD/PT
oaire.citation.conferencePlace12-16 June 2023, San Diego, CA, USA and Onlinept_PT
oaire.citation.titleAIAA AVIATION 2023 Forumpt_PT
oaire.fundingStream6817 - DCRRNI ID
oaire.fundingStreamPOR_CENTRO
person.familyNameRodrigues Camacho
person.familyNameResende Rodrigues da Silva
person.givenNameEmanuel António
person.givenNameAndré
person.identifierJ-4185-2012
person.identifier.ciencia-id4416-08D8-F83D
person.identifier.ciencia-id8219-4B2B-E1C7
person.identifier.orcid0000-0002-1648-8368
person.identifier.orcid0000-0002-4901-7140
person.identifier.scopus-author-id11440407500
project.funder.identifierhttp://doi.org/10.13039/501100001871
project.funder.identifierhttp://doi.org/10.13039/501100001871
project.funder.nameFundação para a Ciência e a Tecnologia
project.funder.nameFundação para a Ciência e a Tecnologia
rcaap.embargofctCopyright © 2023 by João Pinho, Emanuel A. R. Camacho and André R. R. Silva. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.pt_PT
rcaap.rightsembargoedAccesspt_PT
rcaap.typeconferenceObjectpt_PT
relation.isAuthorOfPublication38bf759d-639d-44a2-b7da-02e5b6c9774a
relation.isAuthorOfPublication908e150d-3890-457c-b5da-09c84671cb93
relation.isAuthorOfPublication.latestForDiscovery38bf759d-639d-44a2-b7da-02e5b6c9774a
relation.isProjectOfPublicationd3f48e72-49da-44e7-b054-cbdb0644e04d
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