Global sensitivity analysis of analytical vibroacoustic transmission models

被引:18
作者
Christen, Jean-Loup [1 ]
Ichchou, Mohamed [1 ]
Troclet, Bernard [2 ,3 ]
Bareille, Olivier [1 ]
Ouisse, Morvan [4 ]
机构
[1] Univ Lyon, Ecole Cent Lyon, 36 Ave Guy de Collongue, F-69130 Ecully, France
[2] Airbus Def & Space, 66 Route Verneuil, F-78133 Les Mureaux, France
[3] Univ Paris Saclay, ENS Cachan, LMT, 61 Ave President Wilson, F-94230 Cachan, France
[4] ENSMM UBFC, FEMTO ST Appl Mech, UMR CNRS 6174, 24 Chemin Epitaphe, F-25000 Besancon, France
关键词
FAST; Sound transmission loss; Composite structures; Diffuse field; COUPLED REACTION SYSTEMS; RATE COEFFICIENTS; SOUND INSULATION; UNCERTAINTIES; PANELS; BEHAVIOR; PLATES;
D O I
10.1016/j.jsv.2016.01.009
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Noise reduction issues arise in many engineering problems. One typical vibroacoustic problem is the transmission loss (TL) optimisation and control. The TL depends mainly on the mechanical parameters of the considered media. At early stages of the design, such parameters are not well known. Decision making tools are therefore needed to tackle this issue. In this paper, we consider the use of the Fourier Amplitude Sensitivity Test (FAST) for the analysis of the impact of mechanical parameters on features of interest. FAST is implemented with several structural configurations. FAST method is used to estimate the relative influence of the model parameters while assuming some uncertainty or variability on their values. The method offers a way to synthesize the results of a multiparametric analysis with large variability. Results are presented for transmission loss of isotropic, orthotropic and sandwich plates excited by a diffuse field on one side. Qualitative trends found to agree with the physical expectation. Design rules can then be set up for vibroacoustic indicators. The case of a sandwich plate is taken as an example of the use of this method inside an optimisation process and for uncertainty quantification. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:121 / 134
页数:14
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