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Bending and vibration analysis of skew sandwich plate

Pankaj V. Katariya (Department of Mechanical Engineering, National Institute of Technology Rourkela, India)
Subrata Kumar Panda (Department of Mechanical Engineering, National Institute of Technology Rourkela, India)
Trupti Ranjan Mahapatra (Department of Production Engineering, VSSUT Burla, Sambalpur, Odisha, India)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 8 October 2018

Issue publication date: 19 October 2018

269

Abstract

Purpose

The purpose of this paper is to develop a general mathematical model for the evaluation of the bending and vibration responses of the skew sandwich composite plate using higher-order shear deformation theory. The sandwich structural components are highly preferable in modern engineering application because of their desirable structural advantages despite the manufacturing and analysis complexities. The present model is developed to solve the bending and vibration problem of the skew sandwich composite plate with adequate accuracy numerically in the absence of the experimental analysis.

Design/methodology/approach

The skew sandwich composite plate structure is modelled in the present analysis by considering laminated face sheet in conjunction with isotropic and/or orthotropic core numerically with the help of the higher-order mathematical model. Further, the responses are computed numerically with the help of in-house computer code developed in matrix laboratory (MATLAB) environment in conjunction with finite element (FE) steps. The system governing equations are derived via variational technique for the computation of the static and the frequency responses.

Findings

The skew sandwich composite plate is investigated using the higher-order kinematic model where the transverse displacement through the thickness is considered to be linear. The convergence and the validation study of the bending and the frequency values of the sandwich structure indicate the necessary accuracy. Further, the current model has been used to highlight the applicability of the higher-order kinematics for the evaluation of the sandwich structural responses (frequency and static deflections) for different design parameters.

Originality/value

In the present paper, the bending and the vibration responses of the skew sandwich composite plate are analysed numerically using the equivalent single-layer higher-order kinematic theory for the isotropic and the orthotropic core numerically with the help of isoparametric FE steps. Finally, it is understood that the present model is capable of solving the sandwich structural responses with less computation cost and adequate accuracy.

Keywords

Citation

Katariya, P.V., Panda, S.K. and Mahapatra, T.R. (2018), "Bending and vibration analysis of skew sandwich plate", Aircraft Engineering and Aerospace Technology, Vol. 90 No. 6, pp. 885-895. https://doi.org/10.1108/AEAT-05-2016-0087

Publisher

:

Emerald Publishing Limited

Copyright © 2018, Emerald Publishing Limited

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