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Mechanics of Composite Materials
Erschienen in: Mechanics of Composite Materials 5/2012

01.11.2012

Parametric vibration response of foam-filled sandwich plates under periodic loads

verfasst von: Jin-Yih Kao, Chun-Sheng Chen, Wei-Ren Chen

Erschienen in: Mechanics of Composite Materials | Ausgabe 5/2012

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Abstract

In this paper, the dynamic stability of foam-filled sandwich plates with stiff composite laminated faces subjected to an arbitrary periodic load is studied. The load is taken to be a combination of periodic bending and normal stresses. The governing equations are established by using the Galerkin method with a reduced eigenfunctions transformation. The equations of motion of Mathieu type are derived and used to determine the regions of dynamic instability based on Bolotin’s method. A numerical approach is developed to determine the dynamic stability of foam-filled sandwich plates. The effects of load parameters and core layer thickness on the excitation frequency, dynamic stability region and dynamic instability index are discussed.
Vorheriger Artikel Average elastic and strength characteristics of a honeycomb core and a theoretical-experimental method of their determination
Nächster Artikel Mechanical behavior of concrete columns confined by basalt FRP windings

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Metadaten
Titel
Parametric vibration response of foam-filled sandwich plates under periodic loads
verfasst von
Jin-Yih Kao
Chun-Sheng Chen
Wei-Ren Chen
Publikationsdatum
01.11.2012
Verlag
Springer US
Erschienen in
Mechanics of Composite Materials / Ausgabe 5/2012
Print ISSN: 0191-5665
Elektronische ISSN: 1573-8922
DOI
https://doi.org/10.1007/s11029-012-9297-z

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