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Active control of doubly curved laminated composite shells using elliptical smart constrained layer damping treatment

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TLDR
In this paper, the performance of the smart constrained layer damping (SCLD) treatment with elliptical geometrical plan form is investigated for controlling the vibrations of various types of doubly curved composite shells.
Abstract
In this paper, performance of the smart constrained layer damping (SCLD) treatment with elliptical geometrical plan form is investigated for controlling the vibrations of various types of doubly curved composite shells. The SCLD treatment is composed of a viscoelastic layer and an advanced constraining piezoelectric composite (PZC) layer attached at the top surface of the composite shell. A mesh free (MF) model of the smart composite shell has been developed based on the element free Galerkin approach to study its dynamic behaviour within the framework of a mixed layerwise displacement field theory considering transverse extensibility. Spherical, paraboloid and hyperboloid type composite shells with antisymmetric/symmetric cross-ply as well as general angle-ply lamination sequences are considered for the analysis. The numerical results demonstrated that the elliptical SCLD patches are more efficient in attenuating the vibration of the spherical and paraboloid laminated shells while the regular rectangular/square plan form patches are effective for the hyperboloid shells. The numerical results also indicate that the elliptical patches are having higher performance index in enhancing the active damping characteristics of the composite shells. Investigations are also carried out to analyze the effect of the variation in orientation of the piezoelectric fibers in the active PZC layers in attenuating the vibration of shells.

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Citations
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Journal ArticleDOI

Nonlinear vibration analysis of fiber reinforced composite cylindrical shells with partial constrained layer damping treatment

TL;DR: In this paper, a novel analytical model capable of accurately predicting the strain-dependent characteristics of fiber reinforced composite shells (FRCSs) with partial constrained layer damping (CLD) treatment was proposed.
Journal ArticleDOI

Higher order semi-analytical solution for bending of angle-ply composite laminated cylindrical shells based on three-dimensional theory of elasticity

TL;DR: In this paper, a semi-analytical numerical model was developed to analyze the bending responses of the angle-ply composite laminated cylindrical shells with the fiber reinforced layers using the scaled boundary finite element method (SBFEM).
Journal ArticleDOI

Nonlinear free and forced vibration of porous piezoelectric doubly-curved shells based on NUEF model

TL;DR: In this article, the nonlinear free and forced vibration of porous piezoelectric doubly-curved shells resting on visco-Pasternak foundation is performed within the framework of the nonuniform electric field (NUEF) model and von Karman geometric nonlinearity assumption.
Journal ArticleDOI

A meshless Hermite weighted least-square method for piezoelectric structures

TL;DR: In this paper, a meshless Hermite weighted least square method is developed to improve the accuracy and stability of the numerical analysis for piezoelectric structures, including the constitutive equation, geometric equations, equilibrium equations and boundary conditions.
References
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Journal ArticleDOI

Element‐free Galerkin methods

TL;DR: In this article, an element-free Galerkin method which is applicable to arbitrary shapes but requires only nodal data is applied to elasticity and heat conduction problems, where moving least-squares interpolants are used to construct the trial and test functions for the variational principle.
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Mesh Free Methods: Moving Beyond the Finite Element Method

TL;DR: In this paper, Galerkin et al. defined mesh-free methods for shape function construction, including the use of mesh-less local Petrov-Galerkin methods.
Journal ArticleDOI

Distributed Piezoelectric-Polymer Active Vibration Control of a Cantilever Beam

TL;DR: In this article, an active vibration damper for a cantilever beam was designed using a distributed-parameter actuator and distributedparameter control theory, and preliminary testing of the damper was performed on the first mode of the beam.
Book

Mechanics of laminated composite plates : theory and analysis

J. N. Reddy
TL;DR: In this paper, the authors present a one-dimensional analysis of fiber-reinforced composite materials and their properties, including the properties of the components of a Lamina and their relationship with other components.
Journal ArticleDOI

Analysis of thickness locking in classical, refined and mixed theories for layered shells

TL;DR: In this article, the analysis of thickness locking mechanism, which is a plate/shell-theory mechanism, caused by the use of simplified kinematic assumptions, is extended to shell geometries.
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