Non-linear calculation of the wing in general manoeuvre
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F25%3A00563881" target="_blank" >RIV/60162694:G43__/25:00563881 - isvavai.cz</a>
Result on the web
<a href="https://lib.unob.cz/UNOB_CZ/FVT/K206/MDSPSL/Sborniky/MDSPSL2024_Sbornik.pdf" target="_blank" >https://lib.unob.cz/UNOB_CZ/FVT/K206/MDSPSL/Sborniky/MDSPSL2024_Sbornik.pdf</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Non-linear calculation of the wing in general manoeuvre
Original language description
One of the key aspects of the design process of UAVs is arguably aerodynamic analysis. This usually includes the determination of flight performance as well as stability and control characteristics in all 6 DoF. Low-fidelity methods of aerodynamic analysis are usually a satisfactory tool to perform such calculations. However, upon reviewing currently available literature, it was found out that there is currently no low-fidelity method capable of such task in sufficient depth. This paper presents a first step in developing such an algorithm. It presents a new non-linear algorithm, specifically designed to be able to calculate aerodynamic characteristics of three-dimensional wing with nonzero twist, sweep and dihedral in all 6 DoF. The results obtained with the model implemented in MATLAB are then compared with high-fidelity results for several wings, obtained with wind tunnel measurements.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach<br>I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2024
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Sborník příspěvků 22. mezinárodní vědecké konference
ISBN
978-80-7582-515-5
ISSN
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e-ISSN
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Number of pages
20
Pages from-to
277-296
Publisher name
Univerzita obrany
Place of publication
Brno
Event location
Brno
Event date
Oct 23, 2024
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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