Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials

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dc.contributor.authorZikmund, Pavelcs
dc.contributor.authorKofler, Michaelcs
dc.contributor.authorNavrátil, Jancs
dc.contributor.authorHrstka, Miroslavcs
dc.contributor.authorPollák, Jakubcs
dc.contributor.authorVan Kampen, Erik-Jancs
dc.date.accessioned2025-03-06T10:53:42Z
dc.date.available2025-03-06T10:53:42Z
dc.date.issued2025-01-28cs
dc.description.abstractMetamaterials offer innovative potential for morphing wing design. This study investigates two approaches: a variable-stiffness leading edge and a trailing edge with a metamaterial lattice hinge, applying Multidisciplinary Design Optimization to compare these designs against a conventional composite wing. Aerodynamic, structural, and control analyses are integrated, with initial findings bridging 2D aero-structural wing rib design and 3D aerodynamic and control evaluations.en
dc.formattextcs
dc.format.extent236-241cs
dc.format.mimetypeapplication/pdfcs
dc.identifier.citation2024 New Trends in Aviation Development (NTAD). 2025, p. 236-241.en
dc.identifier.doi10.1109/NTAD63796.2024.10850343cs
dc.identifier.isbn979-8-3315-2774-7cs
dc.identifier.issn2836-2764cs
dc.identifier.orcid0000-0002-5793-8628cs
dc.identifier.orcid0000-0003-3314-8530cs
dc.identifier.orcid0000-0002-3169-3159cs
dc.identifier.orcid0009-0005-7459-116Xcs
dc.identifier.other193813cs
dc.identifier.researcheridL-5975-2018cs
dc.identifier.researcheridR-9211-2016cs
dc.identifier.scopus57204492594cs
dc.identifier.scopus56218273300cs
dc.identifier.urihttps://hdl.handle.net/11012/250090
dc.language.isoencs
dc.publisherIEEEcs
dc.relation.ispartof2024 New Trends in Aviation Development (NTAD)cs
dc.relation.urihttps://ieeexplore.ieee.org/document/10850343cs
dc.rights(C) IEEEcs
dc.rights.accessopenAccesscs
dc.rights.sherpahttp://www.sherpa.ac.uk/romeo/issn/2836-2764/cs
dc.subjectmetamaterialsen
dc.subjectmorphing wingen
dc.subjectmultidisciplinary design optimizationen
dc.subjectunmanned aerial vehiclesen
dc.titleMultidisciplinary Design Optimization Framework for Morphing Wing using Metamaterialsen
dc.type.driverconferenceObjecten
dc.type.statusPeer-revieweden
dc.type.versionacceptedVersionen
sync.item.dbidVAV-193813en
sync.item.dbtypeVAVen
sync.item.insts2025.03.06 11:53:41en
sync.item.modts2025.03.05 10:32:08en
thesis.grantorVysoké učení technické v Brně. Fakulta strojního inženýrství. Ústav mechaniky těles, mechatroniky a biomechanikycs
thesis.grantorVysoké učení technické v Brně. Fakulta strojního inženýrství. Letecký ústavcs
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