Design of morphing wing for aerodynamic performance considering the wing flexibility effects

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dc.contributor.authorNavrátil, Jancs
dc.contributor.authorHostinský, Vladimírcs
dc.contributor.authorSodja, Jurijcs
dc.coverage.volume2716cs
dc.date.issued2024-03-13cs
dc.description.abstractThis paper provides an insight into ongoing research aimed at designing a morphing wing with the ability to continuously adapt its aerodynamic shape. The wing is targeted at a general purpose unmanned aerial vehicle. The morphing wing concept outlined in the paper is based on continuous camber changes of the wing leading and trailing edges, allowing optimal performance in different flight regimes. The aeroelastic tailoring method is used to design the load carrying structure of the wing in order to define the optimal stiffness and strength of the structure, which are considered as fixed in subsequent design steps. The research proposes a novel modular design approach that combines aerodynamic shape optimisation and aeroelastic considerations for designing morphing wing surfaces.en
dc.formattextcs
dc.format.extent1-8cs
dc.format.mimetypeapplication/pdfcs
dc.identifier.citationJournal of Physics: Conference Series. 2024, vol. 2716, p. 1-8.en
dc.identifier.doi10.1088/1742-6596/2716/1/012029cs
dc.identifier.issn1742-6596cs
dc.identifier.orcid0000-0003-3314-8530cs
dc.identifier.orcid0000-0002-6547-6750cs
dc.identifier.other188391cs
dc.identifier.researcheridL-5975-2018cs
dc.identifier.scopus56218273300cs
dc.identifier.urihttp://hdl.handle.net/11012/245518
dc.language.isoencs
dc.publisherIOP Publishingcs
dc.relation.ispartofJournal of Physics: Conference Seriescs
dc.relation.urihttps://iopscience.iop.org/article/10.1088/1742-6596/2716/1/012029cs
dc.rightsCreative Commons Attribution 4.0 Internationalcs
dc.rights.accessopenAccesscs
dc.rights.sherpahttp://www.sherpa.ac.uk/romeo/issn/1742-6596/cs
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/cs
dc.subjectwingen
dc.subjectdesignen
dc.subjectmorphingen
dc.titleDesign of morphing wing for aerodynamic performance considering the wing flexibility effectsen
dc.type.driverconferenceObjecten
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen
sync.item.dbidVAV-188391en
sync.item.dbtypeVAVen
sync.item.insts2025.02.03 15:47:32en
sync.item.modts2025.01.17 15:14:15en
thesis.grantorVysoké učení technické v Brně. Fakulta strojního inženýrství. Letecký ústavcs
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