Aeroelastic model of a morphing wing for control design and optimization

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F21%3A00354289" target="_blank" >RIV/68407700:21220/21:00354289 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1109/ICMERR54363.2021.9680832" target="_blank" >http://dx.doi.org/10.1109/ICMERR54363.2021.9680832</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/ICMERR54363.2021.9680832" target="_blank" >10.1109/ICMERR54363.2021.9680832</a>

Result language
angličtina
Original language name
Aeroelastic model of a morphing wing for control design and optimization
Original language description
Two dimensional unsteady aerodynamic model in time domain is derived using approximated Wagner function. Strip theory is used to obtain three dimensional aeroelastic model of high aspect ratio morphing wing in state space form. Several simulations are performed to demonstrate the model properties including flutter analysis and influence of longitudinal maneuver on the wing. Aim of this paper is to obtain a aeoroelastic model of a wing that will be used for design and optimization of control strategies.
Czech name
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Czech description
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Project
<a href="/en/project/GA19-16772S" target="_blank" >GA19-16772S: Aerodynamic bodies with actively controlled morphing</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2021
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
2021 6th International Conference on Mechanical Engineering and Robotics Research
ISBN
978-1-6654-0642-0
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
130-135
Publisher name
IEEE
Place of publication
Piscataway
Event location
Krakov (Virtuálně)
Event date
Dec 11, 2021
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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