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Acta Mechanica
Erschienen in: Acta Mechanica 3/2023

05.12.2022 | Original Paper

Nonlinear vibrations of doubly curved composite sandwich shells with FDM additively manufactured flexible honeycomb core

Erschienen in: Acta Mechanica | Ausgabe 3/2023

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Abstract

Geometrically nonlinear forced vibrations of doubly curved sandwich shell with honeycomb core, which is manufactured by fused deposition modeling (FDM), are analyzed numerically. The higher-order shear deformation theory is used to describe the structure-deflected mode. The dynamic behavior of every layer of the structure is described by five variables (three displacements projections and two rotations of the normal to the middle surface). The system of the nonlinear ordinary differential equations is obtained to describe the sandwich shell forced nonlinear vibrations. The assumed-mode method is used to derive this system. The numerical approach, which is a combination of the continuation technique and the shooting method, is applied to analyze the nonlinear periodic vibrations and their bifurcations. The properties of the nonlinear periodic vibrations and their bifurcations are analyzed numerically in the principal and the sub-harmonic resonances.
Vorheriger Artikel Modified continuum theoretical model for size-dependent piezoelectric properties of nanowires
Nächster Artikel Moving point load on a beam with viscoelastic foundation containing fractional derivatives of complex order
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Metadaten
Titel
Nonlinear vibrations of doubly curved composite sandwich shells with FDM additively manufactured flexible honeycomb core
Publikationsdatum
05.12.2022
Erschienen in
Acta Mechanica / Ausgabe 3/2023
Print ISSN: 0001-5970
Elektronische ISSN: 1619-6937
DOI
https://doi.org/10.1007/s00707-022-03426-w

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