Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F25%3APU155012" target="_blank" >RIV/00216305:26210/25:PU155012 - isvavai.cz</a>
Result on the web
<a href="https://ieeexplore.ieee.org/document/10850343" target="_blank" >https://ieeexplore.ieee.org/document/10850343</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/NTAD63796.2024.10850343" target="_blank" >10.1109/NTAD63796.2024.10850343</a>
Alternative languages
Result language
angličtina
Original language name
Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials
Original language description
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.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2025
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
2024 New Trends in Aviation Development (NTAD)
ISBN
979-8-3315-2774-7
ISSN
2836-2764
e-ISSN
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Number of pages
6
Pages from-to
236-241
Publisher name
IEEE
Place of publication
neuveden
Event location
Starý Smokovec
Event date
Nov 28, 2024
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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