Free vibration of symmetric angle-ply laminated truncated conical shells using spline function

Free vibration of symmetric angle-ply laminated truncated conical shells using spline function technique is studied. The equations of motion for conical shells can be obtained by deriving and substituting the proper Lamé parameters of conical shells in the general shell equations. The displacements...

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Main Author: Md. Khalid, Nur Aisyah
Format: Thesis
Language:English
Published: 2013
Subjects:
Online Access:http://eprints.utm.my/id/eprint/32106/5/NuraisyahMdKhalidMFS2013.pdf
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spelling my-utm-ep.321062017-09-12T08:46:21Z Free vibration of symmetric angle-ply laminated truncated conical shells using spline function 2013-01 Md. Khalid, Nur Aisyah Q Science (General) Free vibration of symmetric angle-ply laminated truncated conical shells using spline function technique is studied. The equations of motion for conical shells can be obtained by deriving and substituting the proper Lamé parameters of conical shells in the general shell equations. The displacements are assumed in the separable form. Since no closed form solutions are generally possible, a numerical solution procedure is adopted in which the displacement functions are approximated by cubic and quintic splines. A generalized eigenvalue problem is obtained which is solved numerically for an eigenfrequency parameter and an associated eigenvector of spline coefficients. Parametric studies are made to investigate the effect of circumferential mode number, length ratio and cone angle using different number of layers with different ply orientations on the frequency parameter under two different boundary conditions. 2013-01 Thesis http://eprints.utm.my/id/eprint/32106/ http://eprints.utm.my/id/eprint/32106/5/NuraisyahMdKhalidMFS2013.pdf application/pdf en public masters Universiti Teknologi Malaysia, Faculty of Science Faculty of Science
institution Universiti Teknologi Malaysia
collection UTM Institutional Repository
language English
topic Q Science (General)
spellingShingle Q Science (General)
Md. Khalid, Nur Aisyah
Free vibration of symmetric angle-ply laminated truncated conical shells using spline function
description Free vibration of symmetric angle-ply laminated truncated conical shells using spline function technique is studied. The equations of motion for conical shells can be obtained by deriving and substituting the proper Lamé parameters of conical shells in the general shell equations. The displacements are assumed in the separable form. Since no closed form solutions are generally possible, a numerical solution procedure is adopted in which the displacement functions are approximated by cubic and quintic splines. A generalized eigenvalue problem is obtained which is solved numerically for an eigenfrequency parameter and an associated eigenvector of spline coefficients. Parametric studies are made to investigate the effect of circumferential mode number, length ratio and cone angle using different number of layers with different ply orientations on the frequency parameter under two different boundary conditions.
format Thesis
qualification_level Master's degree
author Md. Khalid, Nur Aisyah
author_facet Md. Khalid, Nur Aisyah
author_sort Md. Khalid, Nur Aisyah
title Free vibration of symmetric angle-ply laminated truncated conical shells using spline function
title_short Free vibration of symmetric angle-ply laminated truncated conical shells using spline function
title_full Free vibration of symmetric angle-ply laminated truncated conical shells using spline function
title_fullStr Free vibration of symmetric angle-ply laminated truncated conical shells using spline function
title_full_unstemmed Free vibration of symmetric angle-ply laminated truncated conical shells using spline function
title_sort free vibration of symmetric angle-ply laminated truncated conical shells using spline function
granting_institution Universiti Teknologi Malaysia, Faculty of Science
granting_department Faculty of Science
publishDate 2013
url http://eprints.utm.my/id/eprint/32106/5/NuraisyahMdKhalidMFS2013.pdf
_version_ 1747815922835390464