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Effect of parametric uncertainties on sound transmission of composite structures
Jean-Loup Christen  1@  , Mohamed Ichchou  2@  , Bernard Troclet  3@  , Olivier Bareille  4@  , Morvan Ouisse  5@  
1 : Laboratoire de Tribologie et Dynamique des Systèmes  (LTDS)  -  Website
Ecole Centrale de Lyon
36 Avenue Guy de Collongue, 69134 Ecully Cedex -  France
2 : École Centrale de Lyon  (ECL / LTDS)  -  Website
Université Lyon
36 Avenue Guy de Collongue, 69134 Écully -  France
3 : AIRBUS Defence & Space  -  Website
AIRBUS Defence & Space
51-61 Route de Verneuil, 78133 Les Mureaux Cedex -  France
4 : École Centrale de Lyon  (ECL/LTDS)
Université de Lyon
5 : Franche-Comté Électronique Mécanique, Thermique et Optique - Sciences et Technologies  (FEMTO-ST)  -  Website
CNRS : UMR6174, Université de Franche-Comté, Université de Technologie de Belfort-Montbeliard, Ecole Nationale Supérieure de Mécanique et des Microtechniques
32 avenue de l'Observatoire 25044 BESANCON CEDEX -  France

Composite materials are widely used in the aerospace industry, for their low mass and high stiffness, however, these characteristics tend to increase noise transmission. Sound protection must therefore be added, in the form of porous material layers. Uncertainties may affect both the structural and sound package parameters. It is therefore important to assess the influence of these uncertain parameters on the sound transmission properties of the assembly. The sound transmission loss through a composite plate-foam assembly is first computed with the transfer matrix method. The effect of uncertainty of several parameters such as the porosity, flow resistivity and mechanical parameters is then analysed with the FAST (Fourier amplitude sensitivity test) method. The effect of adding a thin screen at the interface between the porous and the air is also investigated.


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