Abstract

This paper presents a multiscale approach to study the nonlinear vibration of fiber reinforced composite laminates containing an embedded, through-width delamination dividing the laminate into four sub-laminates. The equations of motion are established from macroscopic nonlinear mechanics for plates and shells and micro-mechanics of composite material to allow for the influences of large amplitude, membrane stretching in the neutral plane, and the interactions of the sublaminates. Analytical solutions obtained in this paper reveal that the interaction penalty at the interfaces plays a coupling effect between sublaminates, which eventually alters the vibration characters of the four-sublaminate lamina in macroscopic and microscopic mechanism. From a macro perspective, sub-laminates above and below the delamination vibrate in exactly the same mode in spite of their different stiffness and the four-sublaminate lamina has a consistent global vibration mode. In accompanying with the macro vibration, micro buckles occur on the interfaces of the delamination with amplitude about 10−3 times of that of the global mode. It is found that the vibration frequency is an eigenvalue of the delaminated lamina determined only by the geometry of the delamination. Authentication of the multiscale study is fulfilled by comparing the analytical solutions with the FEA results.

Highlights

  • Carbon-fiber-reinforced composite materials consist of two parts: matrices and reinforcements

  • Ovesy et al.[5] suggested a novel layerwise theory to evaluate the buckling and post-buckling behavior of delaminated composite plates with multiple through-the-width delaminations based on the first order shear deformation theory (FSDT)

  • The laminate has a geometry size of 2 m × 2 m × 0.12 m and is composed of 60 plies made of T300/QY8911 carbon fiber reinforced composite material with the density ρ = 2150 kg/m3 stacked in a sequence of [0°/90°/0°]20 with each single-layer thickness h0 = 0.002 m

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Summary

Introduction

Carbon-fiber-reinforced composite materials consist of two parts: matrices and reinforcements. Dynamic responses of laminates with two-dimensional embedded delamination were studied by Dey and Karmakar[19] to examine free vibration of multiple delaminated angle-ply composite conical shells using Mindlin’s theory and the multi-point constraint algorithm and by Noh and Lee[20] to analyze the dynamic stability of laminated skew plates by developing a finite element formulation based on HSDT. Schwarts-Givli et al.[31] further put forward a step function in the nonlinear constrain model to incorporate “with and without contact” conditions in the governing equations, which reflects the nonlinear nature of the contact behavior

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