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Dynamic and aeroelastic analysis of UAV wing with moving force, moving moment and moving torque

Abstract Next-generation UAV wing configurations featuring span morphing or moving mass actuation mechanisms offer solutions to limitations in aerodynamic performance and control authority found in traditional designs. This study investigates the aeroelastic response of such a UAV wing subjected to...

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Detalles Bibliográficos
Principais autores: Debashis Singha, Senthil Murugan
Formato: Artigo
Idioma:Inglês
Publicado: Springer 2025-11-01
Series:Discover Mechanical Engineering
Assuntos:
Acceso en liña:https://doi.org/10.1007/s44245-025-00139-x
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