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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

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

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

  • 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

  • e-ISSN

  • 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