Hamiltonian parametric element and semi-analytical solution for smart laminated plates
Based on the Hellinger-Reissner (H-R) mixed variational principle for piezoelectric material, a unified 4-node Hamiltonian isoparametric element of anisotropy piezoelectric material is established. A new semi-analytical solution for the natural vibration of smart laminated plates and the transient r...
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Published in | Applied mathematics and mechanics Vol. 28; no. 1; pp. 51 - 58 |
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Main Author | |
Format | Journal Article |
Language | English |
Published |
Aeronautical Mechanics and Avionics Engineering College,Civil Aviation University of China, Tianjin 300300, P. R. China%Department of Mechanics and Engineering Measurement, School of Mechanical Engineering, Tianjin University, Tianjin 300072, P. R. China
2007
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Subjects | |
Online Access | Get full text |
ISSN | 0253-4827 1573-2754 |
DOI | 10.1007/s10483-007-0106-z |
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Abstract | Based on the Hellinger-Reissner (H-R) mixed variational principle for piezoelectric material, a unified 4-node Hamiltonian isoparametric element of anisotropy piezoelectric material is established. A new semi-analytical solution for the natural vibration of smart laminated plates and the transient response of the laminated cantilever with piezoelectric patch is presented. The major steps of mathematical model are as follows: the piezoelectric layer and host layer of laminated plate are considered as unattached three-dimensional bodies and discretized by the Hamiltonian isoparametric elements. The control equation of whole structure is derived by considering the compatibility of generalized displacements and generalized stresses on the interface between layers. There is no restriction for the side-face geometrical boundaries, the thickness and the number of layers of plate by the use of the present isoparametric element. Present method has wide application area. |
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AbstractList | O3; Based on the Hellinger-Reissner (H-R) mixed variational principle for piezoelectric material, a unified 4-node Hamiltonian isoparametric element of anisotropy piezoelectric material is established. A new semi-analytical solution for the natural vibration of smart laminated plates and the transient response of the laminated cantilever with piezoelectric patch is presented. The major steps of mathematical model are as follows:the piezoelectric layer and host layer of laminated plate are considered as unattached three-dimensional bodies and discretized by the Hamiltonian isoparametric elements. The control equation of whole structure is derived by considering the compatibility of generalized displacements and generalized stresses on the interface between layers. There is no restriction for the side-face geometrical boundaries, the thickness and the number of layers of plate by the use of the present isoparametric element. Present method has wide application area. Based on the Hellinger-Reissner (H-R) mixed variational principle for piezoelectric material, a unified 4-node Hamiltonian isoparametric element of anisotropy piezoelectric material is established. A new semi-analytical solution for the natural vibration of smart laminated plates and the transient response of the laminated cantilever with piezoelectric patch is presented. The major steps of mathematical model are as follows: the piezoelectric layer and host layer of laminated plate are considered as unattached three-dimensional bodies and discretized by the Hamiltonian isoparametric elements. The control equation of whole structure is derived by considering the compatibility of generalized displacements and generalized stresses on the interface between layers. There is no restriction for the side-face geometrical boundaries, the thickness and the number of layers of plate by the use of the present isoparametric element. Present method has wide application area. Based on the Hellinger-Reissner (H-R) mixed variational principle for piezoelectric material, a unified 4-node Hamiltonian isoparametric element of anisotropy piezoelectric material is established. A new semi-analytical solution for the natural vibration of smart laminated plates and the transient response of the laminated cantilever with piezoelectric patch is presented. The major steps of mathematical model are as follows: the piezoelectric layer and host layer of laminated plate are considered as unattached three-dimensional bodies and discretized by the Hamiltonian isoparametric elements. The control equation of whole structure is derived by considering the compatibility of generalized displacements and generalized stresses on the interface between layers. There is no restriction for the side-face geometrical boundaries, the thickness and the number of layers of plate by the use of the present isoparametric element. Present method has wide application area. |
Author | 卿光辉 邱家俊 刘艳红 |
AuthorAffiliation | Aeroaautical Mechanics and Avionics Engineering College,Civil Aviation University of China, Tianjin 300300, P. R. China Department of Mechanics and Engineering Measurement, School of Mechanical Engineering, Tianjin University, Tianjin 300072, P. R. China |
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Keywords | vibration analysis smart laminated plate piezoelectric material Hamiltonian isoparametric element semi-analytical solution |
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References | G. Zou (106_CR9) 1994 J. N. Reddy (106_CR10) 1983; 19 W. Zhong (106_CR2) 1991; 31 D. A. Saravanos (106_CR7) 1997; 34 G. Qing (106_CR5) 2004; 17 106_CR1 L. Tang (106_CR3) 1991; 8 G. Qing (106_CR12) 2004; 36 A. Benjeddou (106_CR6) 2000; 76 Y. H. Lim (106_CR11) 1997; 6 W. Zhong (106_CR4) 1995 L. Tang (106_CR8) 1992; 9 |
References_xml | – volume: 31 start-page: 373 issue: 4 year: 1991 ident: 106_CR2 publication-title: Journal of Dalian University of Technology – start-page: 11 volume-title: The mixed state equation, hamilton canonical equation and a semi-analytical solution for the analysis of laminated composite plate and shells[D] year: 1994 ident: 106_CR9 – volume: 8 start-page: 343 issue: 4 year: 1991 ident: 106_CR3 publication-title: Computational Structural Mechanics and Applications – volume: 36 start-page: 749 issue: 6 year: 2004 ident: 106_CR12 publication-title: Acta Mechanica Sinica – volume: 76 start-page: 347 issue: 1 year: 2000 ident: 106_CR6 publication-title: Computers and Structures doi: 10.1016/S0045-7949(99)00151-0 – volume: 34 start-page: 359 issue: 3 year: 1997 ident: 106_CR7 publication-title: International Journal of Structures and Solids doi: 10.1016/S0020-7683(96)00012-1 – volume: 9 start-page: 347 issue: 4 year: 1992 ident: 106_CR8 publication-title: Computational Structural Mechanics and Applications – start-page: 155 volume-title: A new systematic methodology for theory of elasticity[M] year: 1995 ident: 106_CR4 – ident: 106_CR1 – volume: 19 start-page: 237 issue: 2 year: 1983 ident: 106_CR10 publication-title: International Journal Numeric Method and Engineering doi: 10.1002/nme.1620190206 – volume: 6 start-page: 53 issue: 1 year: 1997 ident: 106_CR11 publication-title: Smart Material and Structures doi: 10.1088/0964-1726/6/1/007 – volume: 17 start-page: 285 issue: 3 year: 2004 ident: 106_CR5 publication-title: Journal of Vibration Engineering |
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Snippet | Based on the Hellinger-Reissner (H-R) mixed variational principle for piezoelectric material, a unified 4-node Hamiltonian isoparametric element of anisotropy... Based on the Hellinger-Reissner (H-R) mixed variational principle for piezoelectric material, a unified 4-node Hamiltonian isoparametric element of anisotropy... O3; Based on the Hellinger-Reissner (H-R) mixed variational principle for piezoelectric material, a unified 4-node Hamiltonian isoparametric element of... |
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SubjectTerms | Boundaries Cantilever plates Laminates Mathematical analysis Mathematical models Piezoelectricity Plates Vibration 半解析解 各向异性压电材料 振动分析 智能层合扳 汉密尔顿等参元 |
Title | Hamiltonian parametric element and semi-analytical solution for smart laminated plates |
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