Computing the broadband vibroacoustic response of arbitrarily thick layered panels by a wave finite element approach

被引:33
作者
Chronopoulos, D. [1 ,2 ]
Ichchou, M. [2 ]
Troclet, B. [1 ,3 ]
Bareille, O. [2 ]
机构
[1] EADS Astrium ST, F-78133 Les Mureaux, France
[2] Ecole Cent Lyon, F-69134 Ecully, France
[3] Ecole Normale Super, F-94230 Cachan, France
关键词
Aerospace composites; Wave propagation; Sound Transmission Loss; SOUND-TRANSMISSION LOSS; RADIATION EFFICIENCY; RIBBED PLATES; MODAL DENSITY; PROPAGATION; PREDICTION;
D O I
10.1016/j.apacoust.2013.10.002
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
A robust procedure for the prediction of the dynamic response of layered panels within a SEA wave-context approach is proposed hereby. The dispersion characteristics of two dimensional composite orthotropic structures are predicted using a Wave Finite Element method. By manipulating the mass and stiffness matrices of the modelled structural segment a polynomial eigenvalue problem is formed, the solutions of which correspond to the propagation constants of the waves travelling within the structure. The wave-numbers and group velocities for waves comprising out of plane structural displacements can then be calculated. Using the numerically extracted wave propagation data the most important SEA quantities of the structure are calculated, namely the modal density and the radiation efficiency of each wave type. The vibroacoustic response of the structure under a broadband diffused excitation is then computed within a SEA approach. The impact of the symmetric and the antisymmetric vibrational motion of the panel on its Sound Transmission Loss is exhibited and the approach proves robust enough for thin as well as for thick layered structures. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:89 / 98
页数:10
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