Publication detail

Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials

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

Original Title

Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials

Type

conference paper

Language

English

Original 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.

Keywords

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

Authors

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

Released

28. 1. 2025

Publisher

IEEE

ISBN

979-8-3315-2774-7

Book

2024 New Trends in Aviation Development (NTAD)

ISBN

2836-2764

Periodical

2024 New Trends in Aviation Development (NTAD)

State

United States of America

Pages from

236

Pages to

241

Pages count

6

URL

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

Full text in the Digital Library

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"
}