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Three-dimensional vibration of laminated cylinders and cylindrical panels with symmetric or antisymmetric cross-ply lay-up

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Three-dimensional vibration of laminated cylinders and cylindrical panels with symmetric or antisymmetric cross-ply lay-up. / Ye, Jianqiao; Soldatos, K P .
In: Composites Part B: Engineering, Vol. 4, No. 4, 1994, p. 429-444.

Research output: Contribution to Journal/Magazine › Journal article › peer-review

Harvard

Ye, J & Soldatos, KP 1994, 'Three-dimensional vibration of laminated cylinders and cylindrical panels with symmetric or antisymmetric cross-ply lay-up', Composites Part B: Engineering, vol. 4, no. 4, pp. 429-444. https://doi.org/10.1016/S0961-9526(09)80016-6

APA

Ye, J., & Soldatos, K. P. (1994). Three-dimensional vibration of laminated cylinders and cylindrical panels with symmetric or antisymmetric cross-ply lay-up. Composites Part B: Engineering, 4(4), 429-444. https://doi.org/10.1016/S0961-9526(09)80016-6

Vancouver

Ye J, Soldatos KP. Three-dimensional vibration of laminated cylinders and cylindrical panels with symmetric or antisymmetric cross-ply lay-up. Composites Part B: Engineering. 1994;4(4):429-444. doi: 10.1016/S0961-9526(09)80016-6

Author

Ye, Jianqiao ; Soldatos, K P . / Three-dimensional vibration of laminated cylinders and cylindrical panels with symmetric or antisymmetric cross-ply lay-up. In: Composites Part B: Engineering. 1994 ; Vol. 4, No. 4. pp. 429-444.

Bibtex

@article{ef3506ab53534db19ac0a7e857105fe7,
title = "Three-dimensional vibration of laminated cylinders and cylindrical panels with symmetric or antisymmetric cross-ply lay-up",
abstract = "A refined formulation of an approach suitable for three-dimensional vibration analyses of homogeneous and cross-ply laminated cylinders and cylindrical panels (Soldatos and Hadjigeorgiou, 1990, J. Sound. Vibr. 137, 369-384) is presented. Based on a recursive rather than a successive approximation formula, the present refined formulation always makes use of a 6 x 6 frequency determinant, regardless of the number of layers of the laminated shell or panel considered. Upon comparing its results with corresponding numerical results available in the literature, the effectiveness of the approach in producing the exact frequencies of vibration is checked. Moreover, further detailed numerical results dealing with flexural vibration frequencies and corresponding mode shapes of laminated cylinders and cylindrical panels having symmetric or regular antisymmetric cross-ply lay-up are presented, studied and discussed.",
author = "Jianqiao Ye and Soldatos, {K P}",
year = "1994",
doi = "10.1016/S0961-9526(09)80016-6",
language = "English",
volume = "4",
pages = "429--444",
journal = "Composites Part B: Engineering",
issn = "0961-9526",
publisher = "ELSEVIER SCI LTD",
number = "4",

}

RIS

TY - JOUR

T1 - Three-dimensional vibration of laminated cylinders and cylindrical panels with symmetric or antisymmetric cross-ply lay-up

AU - Ye, Jianqiao

AU - Soldatos, K P

PY - 1994

Y1 - 1994

N2 - A refined formulation of an approach suitable for three-dimensional vibration analyses of homogeneous and cross-ply laminated cylinders and cylindrical panels (Soldatos and Hadjigeorgiou, 1990, J. Sound. Vibr. 137, 369-384) is presented. Based on a recursive rather than a successive approximation formula, the present refined formulation always makes use of a 6 x 6 frequency determinant, regardless of the number of layers of the laminated shell or panel considered. Upon comparing its results with corresponding numerical results available in the literature, the effectiveness of the approach in producing the exact frequencies of vibration is checked. Moreover, further detailed numerical results dealing with flexural vibration frequencies and corresponding mode shapes of laminated cylinders and cylindrical panels having symmetric or regular antisymmetric cross-ply lay-up are presented, studied and discussed.

AB - A refined formulation of an approach suitable for three-dimensional vibration analyses of homogeneous and cross-ply laminated cylinders and cylindrical panels (Soldatos and Hadjigeorgiou, 1990, J. Sound. Vibr. 137, 369-384) is presented. Based on a recursive rather than a successive approximation formula, the present refined formulation always makes use of a 6 x 6 frequency determinant, regardless of the number of layers of the laminated shell or panel considered. Upon comparing its results with corresponding numerical results available in the literature, the effectiveness of the approach in producing the exact frequencies of vibration is checked. Moreover, further detailed numerical results dealing with flexural vibration frequencies and corresponding mode shapes of laminated cylinders and cylindrical panels having symmetric or regular antisymmetric cross-ply lay-up are presented, studied and discussed.

U2 - 10.1016/S0961-9526(09)80016-6

DO - 10.1016/S0961-9526(09)80016-6

M3 - Journal article

VL - 4

SP - 429

EP - 444

JO - Composites Part B: Engineering

JF - Composites Part B: Engineering

SN - 0961-9526

IS - 4

ER -