Large, lightweight deployable structures are key enablers for next-generation space systems, but reliable prediction of their natural frequencies remains difficult when ultra-Thin components, geometric nonlinearity, and prestress interact at scale. This paper investigates the natural frequencies and mode shapes of a representative fully deployed SSPP-inspired array segment using a refined CUF-based beam model. The study focuses on the undeformed deployed configuration and on one representative prestressed case introduced through a prescribed displacement. The results highlight the persistence of the fundamental global mode shape and the sensitivity of higher modes to prestress-induced mode reordering. A qualitative comparison with the literature is also provided.
Natural Frequencies and Mode Shapes of Prestressed Elastically Foldable Flat Arrays / Augello, R., Carrera, E.. - (2026). (ASME 2026 4th Aerospace Structures, Structural Dynamics, and Materials Conference, SSDM 2026 Long Beach, California (USA) June 8–10, 2026) [10.1115/ssdm2026-183232].
Natural Frequencies and Mode Shapes of Prestressed Elastically Foldable Flat Arrays
Augello, Riccardo;Carrera, Erasmo
2026
Abstract
Large, lightweight deployable structures are key enablers for next-generation space systems, but reliable prediction of their natural frequencies remains difficult when ultra-Thin components, geometric nonlinearity, and prestress interact at scale. This paper investigates the natural frequencies and mode shapes of a representative fully deployed SSPP-inspired array segment using a refined CUF-based beam model. The study focuses on the undeformed deployed configuration and on one representative prestressed case introduced through a prescribed displacement. The results highlight the persistence of the fundamental global mode shape and the sensitivity of higher modes to prestress-induced mode reordering. A qualitative comparison with the literature is also provided.| File | Dimensione | Formato | |
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https://hdl.handle.net/11583/3017475
