Detail publikace
Design of morphing wing for aerodynamic performance considering the wing flexibility effects
NAVRÁTIL, J. HOSTINSKÝ, V. SODJA, J.
Anglický název
Design of morphing wing for aerodynamic performance considering the wing flexibility effects
Typ
článek ve sborníku ve WoS nebo Scopus
Jazyk
en
Originální abstrakt
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.
Anglický abstrakt
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.
Klíčová slova anglicky
wing, design, morphing
Vydáno
13.03.2024
Nakladatel
IOP Publishing
ISSN
1742-6596
Kniha
13th EASN International Conference on Innovation in Aviation & Space for opening New Horizons
Ročník
2716
Číslo edice
2716
Strany od–do
1–8
Počet stran
8
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",
volume="2716",
month="March",
pages="1--8",
publisher="IOP Publishing",
issn="1742-6596"
}