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Natural Vibration Analysis of Soft Core Corrugated Sandwich Plates Using Three-Dimensional Finite Element Method

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Mechanics and Properties of Composed Materials and Structures

Part of the book series: Advanced Structured Materials ((STRUCTMAT,volume 31))

Abstract

Nowadays, corrugated plates, sandwich panels, and thin plates stiffened by ribs are commonly available structural materials which allow stiffening flat panels against applied loads and structural vibrations. Response to natural vibration of a soft core corrugated composite skin sandwich plate was investigated in this paper, and the natural frequency of the presented model was obtained using finite element method (FEM). The FEM of the problem has been constructed in the commercial software ANSYS 12.0.A trapezoid corrugated shape was studied on the face sheets of the sandwich structure. The model included a wavy soft core which was located between two wavy trapezoid-shaped skins. The core was assumed as a soft orthotropic material and skins are assumed generally as unequally laminated composites. Comparing the present numerical results with values taken from literature demonstrate the accuracy of the proposed model. The numerical results show that using a trapezoid composite skins increase the natural frequency of the structures.

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Abbreviations

θ :

Angle of trapezoidally model

\( \varphi \) :

Angle of layer layup \( (0/\varphi /{\text{C}}/0/\varphi ) \)

\( h_{t} \) :

Plate thickness

\( h_{s} \) :

Skin thickness

\( h_{c} \) :

Core thickness

E :

Elastic modulus

\( E_{x} ,E_{y} ,E_{z} \) :

Orthotropic elastic modulus

G :

Shear modulus

\( G_{xy,} G_{xy,} G_{xz} \) :

Orthotropic shear modulus

\( \vartheta \) :

Poisson’s rati

\( \vartheta_{xy} ,\vartheta_{yz} ,\vartheta_{xz} \) :

Poisson’s ratio in the x-,y- and z- direction, respectively

a, b :

Panel dimension in the x-(length) and y-directions (width), respectively

\( \rho \) :

Material density

F/2 :

Trapezoidally corrugation amplitude

2C :

Rotation period

\( \sigma_{x} ,\sigma_{y} \) :

Stress in the x, y direction

U :

Displacement in the x-direction

V :

Displacement in the y-direction

W :

Displacement in the z-direction

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Acknowledgments

The work that is described in this chapter was supported by the Islamic Azad University of Qazvin.

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Correspondence to Mohammad Mahdi Kheirikhah .

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Kheirikhah, M.M., Babaghasabha, V., Abkenari, A.N., Edalat, M.E. (2012). Natural Vibration Analysis of Soft Core Corrugated Sandwich Plates Using Three-Dimensional Finite Element Method. In: Öchsner, A., da Silva, L., Altenbach, H. (eds) Mechanics and Properties of Composed Materials and Structures. Advanced Structured Materials, vol 31. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-31497-1_11

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