Detail publikace

Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials

ZIKMUND, P. KOFLER, M. NAVRÁTIL, J. HRSTKA, M. POLLÁK, J. VAN KAMPEN, E.

Originální název

Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

metamaterials, morphing wing, multidisciplinary design optimization, unmanned aerial vehicles

Autoři

ZIKMUND, P.; KOFLER, M.; NAVRÁTIL, J.; HRSTKA, M.; POLLÁK, J.; VAN KAMPEN, E.

Vydáno

28. 1. 2025

Nakladatel

IEEE

ISBN

979-8-3315-2774-7

Kniha

2024 New Trends in Aviation Development (NTAD)

ISSN

2836-2764

Periodikum

2024 New Trends in Aviation Development (NTAD)

Stát

Spojené státy americké

Strany od

236

Strany do

241

Strany počet

6

URL

https://ieeexplore.ieee.org/document/10850343

Plný text v Digitální knihovně

http://hdl.handle.net/11012/250090

BibTex

@inproceedings{BUT193813,
  author="Pavel {Zikmund} and Michael {Kofler} and Jan {Navrátil} and Miroslav {Hrstka} and Jakub {Pollák} and Erik-Jan {Van Kampen}",
  title="Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials",
  booktitle="2024 New Trends in Aviation Development (NTAD)",
  year="2025",
  journal="2024 New Trends in Aviation Development (NTAD)",
  pages="236--241",
  publisher="IEEE",
  doi="10.1109/NTAD63796.2024.10850343",
  isbn="979-8-3315-2774-7",
  issn="2836-2764",
  url="https://ieeexplore.ieee.org/document/10850343"
}