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Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports

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

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Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports. / Ye, J Q ; Soldatos, K P .
In: International Journal of Mechanical Sciences, Vol. 38, No. 3, 03.1996, p. 271-281.

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

Harvard

Ye, JQ & Soldatos, KP 1996, 'Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports', International Journal of Mechanical Sciences, vol. 38, no. 3, pp. 271-281. https://doi.org/10.1016/0020-7403(95)00056-9

APA

Ye, J. Q., & Soldatos, K. P. (1996). Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports. International Journal of Mechanical Sciences, 38(3), 271-281. https://doi.org/10.1016/0020-7403(95)00056-9

Vancouver

Ye JQ, Soldatos KP. Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports. International Journal of Mechanical Sciences. 1996 Mar;38(3):271-281. doi: 10.1016/0020-7403(95)00056-9

Author

Ye, J Q ; Soldatos, K P . / Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports. In: International Journal of Mechanical Sciences. 1996 ; Vol. 38, No. 3. pp. 271-281.

Bibtex

@article{38a07bb7065d47b194728789ba1f2df1,
title = "Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports",
abstract = "On the basis of fully three-dimensional elasticity considerations, this paper presents a free vibration analysis of simply supported, cross-ply laminated plates and cylindrical panels that are subjected to an arbitrary number of lateral surfaces point supports. The analysis is based on a recursive approach suitable for the vibration analysis of corresponding unconstrained structural elements. By means of dynamic equilibrium considerations, the reaction of the point supports is imposed by using the Lagrange multipliers method. This yields the eigendeterminant of a constrained panel by appropriately coupling the response of a suitably large number of natural vibration modes of the corresponding unconstrained structural element.",
author = "Ye, {J Q} and Soldatos, {K P}",
year = "1996",
month = mar,
doi = "10.1016/0020-7403(95)00056-9",
language = "English",
volume = "38",
pages = "271--281",
journal = "International Journal of Mechanical Sciences",
issn = "0020-7403",
publisher = "Elsevier Limited",
number = "3",

}

RIS

TY - JOUR

T1 - Three-dimensional vibration of laminated composite plates and cylindrical panels with arbitrarily located lateral surfaces point supports

AU - Ye, J Q

AU - Soldatos, K P

PY - 1996/3

Y1 - 1996/3

N2 - On the basis of fully three-dimensional elasticity considerations, this paper presents a free vibration analysis of simply supported, cross-ply laminated plates and cylindrical panels that are subjected to an arbitrary number of lateral surfaces point supports. The analysis is based on a recursive approach suitable for the vibration analysis of corresponding unconstrained structural elements. By means of dynamic equilibrium considerations, the reaction of the point supports is imposed by using the Lagrange multipliers method. This yields the eigendeterminant of a constrained panel by appropriately coupling the response of a suitably large number of natural vibration modes of the corresponding unconstrained structural element.

AB - On the basis of fully three-dimensional elasticity considerations, this paper presents a free vibration analysis of simply supported, cross-ply laminated plates and cylindrical panels that are subjected to an arbitrary number of lateral surfaces point supports. The analysis is based on a recursive approach suitable for the vibration analysis of corresponding unconstrained structural elements. By means of dynamic equilibrium considerations, the reaction of the point supports is imposed by using the Lagrange multipliers method. This yields the eigendeterminant of a constrained panel by appropriately coupling the response of a suitably large number of natural vibration modes of the corresponding unconstrained structural element.

U2 - 10.1016/0020-7403(95)00056-9

DO - 10.1016/0020-7403(95)00056-9

M3 - Journal article

VL - 38

SP - 271

EP - 281

JO - International Journal of Mechanical Sciences

JF - International Journal of Mechanical Sciences

SN - 0020-7403

IS - 3

ER -