Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials
Loading...
Date
2025-01-28
Authors
Zikmund, Pavel
Kofler, Michael
Navrátil, Jan
Hrstka, Miroslav
Pollák, Jakub
Van Kampen, Erik-Jan
0000-0002-5793-8628Advisor
Referee
Mark
Journal Title
Journal ISSN
Volume Title
Publisher
IEEE
Altmetrics
Abstract
Metamaterials 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.
Description
Citation
2024 New Trends in Aviation Development (NTAD). 2025, p. 236-241.
https://ieeexplore.ieee.org/document/10850343
https://ieeexplore.ieee.org/document/10850343
Document type
Peer-reviewed
Document version
Accepted version
Date of access to the full text
Language of document
en
Study field
Comittee
Date of acceptance
Defence
Result of defence
Document licence
(C) IEEE