Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method
Free vibration of symmetric angle-ply laminated circular cylindrical shells is studied using Spline approximation. The equations of motions in longitudinal, circumferential and transverse displacement components, are derived using Love's first approximation theory. The coupled differential equa...
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2011
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my.utm.458832017-08-30T01:45:42Z http://eprints.utm.my/id/eprint/45883/ Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method Viswanathan, Kodakkal Kannan Abdul Aziz, Zainal H. Z. Amirah, H. Z. Amirah Javed, Saira Free vibration of symmetric angle-ply laminated circular cylindrical shells is studied using Spline approximation. The equations of motions in longitudinal, circumferential and transverse displacement components, are derived using Love's first approximation theory. The coupled differential equations are solved using Spline approximation to obtain the generalized eigenvalue problem. Parametric studies are performed to analyse the frequency response of the shell with reference to the material properties, number of layers, ply orientation, length and circumferential node number and different boundary conditions. 2011 Conference or Workshop Item PeerReviewed Viswanathan, Kodakkal Kannan and Abdul Aziz, Zainal and H. Z. Amirah, H. Z. Amirah and Javed, Saira (2011) Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method. In: The 7th East Asia Siam Conference (Easiam 2011). http://iopscience.iop.org/article/10.1088/1755-1315/19/1/012010/meta |
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Free vibration of symmetric angle-ply laminated circular cylindrical shells is studied using Spline approximation. The equations of motions in longitudinal, circumferential and transverse displacement components, are derived using Love's first approximation theory. The coupled differential equations are solved using Spline approximation to obtain the generalized eigenvalue problem. Parametric studies are performed to analyse the frequency response of the shell with reference to the material properties, number of layers, ply orientation, length and circumferential node number and different boundary conditions. |
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Conference or Workshop Item |
author |
Viswanathan, Kodakkal Kannan Abdul Aziz, Zainal H. Z. Amirah, H. Z. Amirah Javed, Saira |
spellingShingle |
Viswanathan, Kodakkal Kannan Abdul Aziz, Zainal H. Z. Amirah, H. Z. Amirah Javed, Saira Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method |
author_facet |
Viswanathan, Kodakkal Kannan Abdul Aziz, Zainal H. Z. Amirah, H. Z. Amirah Javed, Saira |
author_sort |
Viswanathan, Kodakkal Kannan |
title |
Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method |
title_short |
Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method |
title_full |
Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method |
title_fullStr |
Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method |
title_full_unstemmed |
Free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method |
title_sort |
free vibration of symmetric angle-ply laminated cylindral shells of variable thickness including shear deformation theory : spline method |
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2011 |
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http://eprints.utm.my/id/eprint/45883/ http://iopscience.iop.org/article/10.1088/1755-1315/19/1/012010/meta |
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