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NAVRÁTIL, J. HOSTINSKÝ, V. SODJA, J.
Original Title
Design of morphing wing for aerodynamic performance considering the wing flexibility effects
Type
conference paper
Language
English
Original Abstract
This paper provides an insight into ongoing research aimed at designing a morphing wing with the ability to continuously adapt its aerodynamic shape. The wing is targeted at a general purpose unmanned aerial vehicle. The morphing wing concept outlined in the paper is based on continuous camber changes of the wing leading and trailing edges, allowing optimal performance in different flight regimes. The aeroelastic tailoring method is used to design the load carrying structure of the wing in order to define the optimal stiffness and strength of the structure, which are considered as fixed in subsequent design steps. The research proposes a novel modular design approach that combines aerodynamic shape optimisation and aeroelastic considerations for designing morphing wing surfaces.
Keywords
wing, design, morphing
Authors
NAVRÁTIL, J.; HOSTINSKÝ, V.; SODJA, J.
Released
13. 3. 2024
Publisher
IOP Publishing
ISBN
1742-6596
Periodical
Journal of Physics: Conference Series
Year of study
2716
State
United Kingdom of Great Britain and Northern Ireland
Pages from
1
Pages to
8
Pages count
URL
https://iopscience.iop.org/article/10.1088/1742-6596/2716/1/012029
Full text in the Digital Library
http://hdl.handle.net/11012/245518
BibTex
@inproceedings{BUT188391, author="Jan {Navrátil} and Vladimír {Hostinský} and Jurij {Sodja}", title="Design of morphing wing for aerodynamic performance considering the wing flexibility effects", booktitle="13th EASN International Conference on Innovation in Aviation & Space for opening New Horizons", year="2024", journal="Journal of Physics: Conference Series", volume="2716", number="2716", pages="8", publisher="IOP Publishing", doi="10.1088/1742-6596/2716/1/012029", issn="1742-6596", url="https://iopscience.iop.org/article/10.1088/1742-6596/2716/1/012029" }