A unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints
A semi-analytical method for in-plane vibration analysis of a composite laminated annular and sector plate with elastic constraints is presented. The theoretical model is on the basis of a variational method and a multi-segment technique. Displacement variables are expanded by the Jacobian orthogona...
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SAGE Publishing
2021
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oai:doaj.org-article:4320405ce0ef4a13a69ad37bda28ad182021-12-02T01:34:38ZA unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints1461-34842048-404610.1177/1461348421994419https://doaj.org/article/4320405ce0ef4a13a69ad37bda28ad182021-12-01T00:00:00Zhttps://doi.org/10.1177/1461348421994419https://doaj.org/toc/1461-3484https://doaj.org/toc/2048-4046A semi-analytical method for in-plane vibration analysis of a composite laminated annular and sector plate with elastic constraints is presented. The theoretical model is on the basis of a variational method and a multi-segment technique. Displacement variables are expanded by the Jacobian orthogonal polynomial. Boundary conditions and continuity conditions between segments are characterized by penalty parameters. On this basis, a series of numerical examples are given. The results show that the method has good convergence speed and accuracy. Finally, the parametric study of geometric and material parameters is carried out to provide important support for solving the in-plane characteristics of this kind of composite structure.Xianlei GuanBin QinRui ZhongQingshan WangSAGE PublishingarticleControl engineering systems. Automatic machinery (General)TJ212-225Acoustics. SoundQC221-246ENJournal of Low Frequency Noise, Vibration and Active Control, Vol 40 (2021) |
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DOAJ |
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Control engineering systems. Automatic machinery (General) TJ212-225 Acoustics. Sound QC221-246 |
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Control engineering systems. Automatic machinery (General) TJ212-225 Acoustics. Sound QC221-246 Xianlei Guan Bin Qin Rui Zhong Qingshan Wang A unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints |
description |
A semi-analytical method for in-plane vibration analysis of a composite laminated annular and sector plate with elastic constraints is presented. The theoretical model is on the basis of a variational method and a multi-segment technique. Displacement variables are expanded by the Jacobian orthogonal polynomial. Boundary conditions and continuity conditions between segments are characterized by penalty parameters. On this basis, a series of numerical examples are given. The results show that the method has good convergence speed and accuracy. Finally, the parametric study of geometric and material parameters is carried out to provide important support for solving the in-plane characteristics of this kind of composite structure. |
format |
article |
author |
Xianlei Guan Bin Qin Rui Zhong Qingshan Wang |
author_facet |
Xianlei Guan Bin Qin Rui Zhong Qingshan Wang |
author_sort |
Xianlei Guan |
title |
A unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints |
title_short |
A unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints |
title_full |
A unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints |
title_fullStr |
A unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints |
title_full_unstemmed |
A unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints |
title_sort |
unified solution for in-plane vibration analysis of composite laminated sector and annular plate with elastic constraints |
publisher |
SAGE Publishing |
publishDate |
2021 |
url |
https://doaj.org/article/4320405ce0ef4a13a69ad37bda28ad18 |
work_keys_str_mv |
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1718402954018422784 |