An unmanned aerial vehicle (UAV) wing must be strong to support heavy take-off weight and high impact load on landing. Hence, the wing is considered as a crucial structure to deal with lift force. Conventionally, the UAV wings were made from heavy metals. Nowadays, the wing structure should be lightweight to fly a longer distance, improving flight operations. To fill in this research gap, this paper proposes a sustainable utilization of composite materials for constructing UAV wings. The static and model structures of the wing are analyzed. The finite element method is used to analyze the UAV wing structure. The wing structure deformations, stresses, and strains are investigated through the ANSYS® Workbench software. Finally, to avoid the relative UAV component failure, the natural frequency analysis is demonstrated.
Static and Modal Analysis of UAV Composite-Based Structures
Sustainable aviat.
International Symposium On Sustainable Aviation ; 2021 November 25, 2021 - November 27, 2021
30.09.2023
8 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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