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Appropriate modeling of unsteady aerodynamic characteristics is required for the study of aircraft dynamics and stability analysis, especially at higher angles of attack. The article presents an example of using artificial neural networks to model such characteristics. The effectiveness of this approach was demonstrated on the example of a strake-wing micro aerial vehicle. The neural model of unsteady aerodynamic characteristics was identified from the dynamic test cycles conducted in a water tunnel. The aerodynamic coefficients were modeled as a function of the flow parameters. The article presents neural models of longitudinal aerodynamic coefficients: lift and pitching moment as functions of angles of attack and reduced frequency. The modeled and trained aerodynamic coefficients show good consistency. This method manifests great potential in the construction of aerodynamic models for flight simulation purposes.
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Tom
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art. no. e137508
Opis fizyczny
Bibliogr. 43 poz., rys.
Twórcy
autor
- Air Force Institute of Technology, ul. Księcia Bolesława 6, 01-494 Warsaw, Poland
autor
- Air Force Institute of Technology, ul. Księcia Bolesława 6, 01-494 Warsaw, Poland
autor
- Warsaw University of Technology, Faculty of Power and Aeronautical Engineering, ul. Nowowiejska 24, 00-665 Warsaw, Poland
autor
- Wroclaw University of Technology, Faculty Mechanical and Power Engineering, ul. Wyb. Wyspiańskiego 27, 50-370 Wroclaw, Poland
autor
- Wroclaw Aircraft Maintenance Services Ltd., ul. Św. Mikołaja 19, 50-062 Wroclaw, Poland
Bibliografia
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Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2021).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-27460476-f573-471c-bc81-49926f6ffe50