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.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.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.urihttp://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.subjectmetamaterials
dc.subjectmorphing wing
dc.subjectmultidisciplinary design optimization
dc.subjectunmanned aerial vehicles
dc.titleMultidisciplinary Design Optimization Framework for Morphing Wing using Metamaterialsen
dc.title.alternativeMultidisciplinary 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.insts2025.10.14 14:53:13en
sync.item.modts2025.10.14 10:15:00en
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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Letecký ústav
Ústav mechaniky těles, mechatroniky a biomechaniky