Parametric study on nonlinear vibration of composite truss core sandwich plate with internal resonance

Nonlinear vibrations of carbon fiber reinforced composite sandwich plate with pyramidal truss core are investigated. The governing equation of motion for the sandwich plate is derived by using a Zig-Zag theory under consideration of geometrically nonlinear. The natural frequencies of sandwich plates...

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Bibliographic Details
Published inJournal of mechanical science and technology Vol. 30; no. 9; pp. 4133 - 4142
Main Authors Chen, Jianen, Zhang, Wei, Sun, Min, Yao, Minghui, Liu, Jun
Format Journal Article
LanguageEnglish
Published Seoul Korean Society of Mechanical Engineers 01.09.2016
Springer Nature B.V
대한기계학회
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Summary:Nonlinear vibrations of carbon fiber reinforced composite sandwich plate with pyramidal truss core are investigated. The governing equation of motion for the sandwich plate is derived by using a Zig-Zag theory under consideration of geometrically nonlinear. The natural frequencies of sandwich plates with different dimensions are calculated and compared with those obtained from the classic laminated plate theory and Reddy’s third-order shear deformation plate theory. The frequency responses and waveforms of the sandwich plate when 1:3 internal resonance occurs are obtained, and the characteristics of the internal resonance are discussed. The influences of layer number of face sheet, strut radius, core height and inclination angle on the nonlinear responses of the sandwich plate are analyzed. The results demonstrate that the strut radius and inclination angle mainly affect the resonance frequency band of the sandwich plate, and the layer number and core height not only influence the resonance frequency band but also significantly affect the response amplitude.
Bibliography:ObjectType-Article-1
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content type line 23
G704-000058.2016.30.9.041
ISSN:1738-494X
1976-3824
DOI:10.1007/s12206-016-0825-y