Buckling and Vibration of Non-Homogeneous Rectangular Plates Subjected to Linearly Varying In-Plane Force

The present work analyses the buckling and vibration behaviour of non-homogeneous rectangular plates of uniform thickness on the basis of classical plate theory when the two opposite edges are simply supported and are subjected to linearly varying in-plane force. For non-homogeneity of the plate mat...

Full description

Bibliographic Details
Main Authors: Roshan Lal, Renu Saini
Format: Article
Language:English
Published: Hindawi Limited 2013-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.3233/SAV-130791
id doaj-5bdc0bab28a34d669313a307fc30eaae
record_format Article
spelling doaj-5bdc0bab28a34d669313a307fc30eaae2020-11-24T23:57:33ZengHindawi LimitedShock and Vibration1070-96221875-92032013-01-0120587989410.3233/SAV-130791Buckling and Vibration of Non-Homogeneous Rectangular Plates Subjected to Linearly Varying In-Plane ForceRoshan Lal0Renu Saini1Department of Mathematics, Indian Institute of Technology Roorkee, Roorkee, IndiaDepartment of Mathematics, Indian Institute of Technology Roorkee, Roorkee, IndiaThe present work analyses the buckling and vibration behaviour of non-homogeneous rectangular plates of uniform thickness on the basis of classical plate theory when the two opposite edges are simply supported and are subjected to linearly varying in-plane force. For non-homogeneity of the plate material it is assumed that young's modulus and density of the plate material vary exponentially along axial direction. The governing partial differential equation of motion of such plates has been reduced to an ordinary differential equation using the sine function for mode shapes between the simply supported edges. This resulting equation has been solved numerically employing differential quadrature method for three different combinations of clamped, simply supported and free boundary conditions at the other two edges. The effect of various parameters has been studied on the natural frequencies for the first three modes of vibration. Critical buckling loads have been computed. Three dimensional mode shapes have been presented. Comparison has been made with the known results.http://dx.doi.org/10.3233/SAV-130791
collection DOAJ
language English
format Article
sources DOAJ
author Roshan Lal
Renu Saini
spellingShingle Roshan Lal
Renu Saini
Buckling and Vibration of Non-Homogeneous Rectangular Plates Subjected to Linearly Varying In-Plane Force
Shock and Vibration
author_facet Roshan Lal
Renu Saini
author_sort Roshan Lal
title Buckling and Vibration of Non-Homogeneous Rectangular Plates Subjected to Linearly Varying In-Plane Force
title_short Buckling and Vibration of Non-Homogeneous Rectangular Plates Subjected to Linearly Varying In-Plane Force
title_full Buckling and Vibration of Non-Homogeneous Rectangular Plates Subjected to Linearly Varying In-Plane Force
title_fullStr Buckling and Vibration of Non-Homogeneous Rectangular Plates Subjected to Linearly Varying In-Plane Force
title_full_unstemmed Buckling and Vibration of Non-Homogeneous Rectangular Plates Subjected to Linearly Varying In-Plane Force
title_sort buckling and vibration of non-homogeneous rectangular plates subjected to linearly varying in-plane force
publisher Hindawi Limited
series Shock and Vibration
issn 1070-9622
1875-9203
publishDate 2013-01-01
description The present work analyses the buckling and vibration behaviour of non-homogeneous rectangular plates of uniform thickness on the basis of classical plate theory when the two opposite edges are simply supported and are subjected to linearly varying in-plane force. For non-homogeneity of the plate material it is assumed that young's modulus and density of the plate material vary exponentially along axial direction. The governing partial differential equation of motion of such plates has been reduced to an ordinary differential equation using the sine function for mode shapes between the simply supported edges. This resulting equation has been solved numerically employing differential quadrature method for three different combinations of clamped, simply supported and free boundary conditions at the other two edges. The effect of various parameters has been studied on the natural frequencies for the first three modes of vibration. Critical buckling loads have been computed. Three dimensional mode shapes have been presented. Comparison has been made with the known results.
url http://dx.doi.org/10.3233/SAV-130791
work_keys_str_mv AT roshanlal bucklingandvibrationofnonhomogeneousrectangularplatessubjectedtolinearlyvaryinginplaneforce
AT renusaini bucklingandvibrationofnonhomogeneousrectangularplatessubjectedtolinearlyvaryinginplaneforce
_version_ 1725453247429214208