Regarding the Use of Finite Element Modeling for Propulsion System Sizing in V.T.O.L. Drones

  • Adrian LEOPA “Dunarea de Jos” University of Galati, Engineering and Agronomy Faculty of Braila, Romania
DOI: https://doi.org/10.35219/mms.2023.3.02

Abstract

At the moment, VTOL drones have proven their efficiency in several areas, for this reason, they have become indispensable tools for a large category of applications. This paper presents aspects related to the dimensioning stage of the propulsion system of a drone based on finite element modeling, to establish the traction force necessary to ensure sustentation.

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Literaturhinweise

[1]. ***, https://grabcad.com/library/low-reynolds-propeller-forultra-light-aircrafts-1.
[2]. Silviu Butnariu, Gheorghe Mogan, Analiza cu elemente finite în ingineria mecanicã, Aplicatii practice în ANSYS, Editura Universităţii Transilvania din Braşov 20.
Veröffentlicht
2023-09-15
Zitationsvorschlag
1.
LEOPA A. Regarding the Use of Finite Element Modeling for Propulsion System Sizing in V.T.O.L. Drones. The Annals of “Dunarea de Jos” University of Galati. Fascicle IX, Metallurgy and Materials Science [Internet]. 15Sep.2023 [zitiert 22Juni2026];46(3):15-9. Available from: https://www.gup.ugal.ro/ugaljournals/index.php/mms/article/view/6246
Ausgabe
Bd. 46 Nr. 3 (2023)
Rubrik
Articles