Abstract
This paper is concerned with the development of mesh free model for the performance analysis of active constrained layered damping (ACLD) treatments on smart laminated composite beams. The overall structure is composed of a substrate laminated composite beam integrated with a viscoelastic layer and a piezoelectric layer attached partially or fully at the top surface of the substrate beam. The piezoelectric layer acts as the active constraining layer of the smart beam and the viscoelastic layer acts as the constrained layer. A layer wise displacement theory has been used to derive the models. Both symmetric cross-ply and antisymmetric angle-ply laminated beams are considered for the numerical analysis. It is observed that ACLD treatment significantly improves the active damping properties of the substrate beam. The numerical results also reveal that the triangular ACLD treatment is more effective than the rectangular ACLD treatment of same thickness and volume for active damping of smart composite beams.
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Appendices
Appendix 1
In Eq. (4), the matrices [Z 1 ], [Z 2 ] and [Z 3 ] are given by:
Appendix 2
In Eq. (22), the matrices \([\varvec{L}_{{\varvec{tb}}} ]\) and \([\varvec{L}_{{\varvec{rb}}} ]\) are given by:
For a rectangular patch of ACLD treatment, the various sub-matrices appearing in Eqs. (24) and (25) are given by:
In case of triangular patch, the above mentioned matrices are to be augmented as follows:
where \(\varvec{b}(\varvec{x}) = \left( {{\mathbf{1}} - \frac{\varvec{x}}{{\varvec{L}_{\varvec{a}} }}} \right)\), \(\varvec{L}_{\varvec{a}}\) is the length of the patch. Various rigidity matrices and the rigidity vectors for electro-elastic coupling appearing in the above equations are given by:
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Sahoo, S.R., Ray, M.C. Analysis of smart damping of laminated composite beams using mesh free method. Int J Mech Mater Des 14, 359–374 (2018). https://doi.org/10.1007/s10999-017-9379-0
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DOI: https://doi.org/10.1007/s10999-017-9379-0