Damping induced by fluid entrainment in porous media is the major mechanism
of vibroacoustic energy dissipation within aircraft cabins. Although such
systems are often satisfactorily modelled using an equivalent fluid formula
tion with a mass enhancement to represent the porous frame, at propeller bl
ade pass frequencies for example, the reactive forces generated by the fram
e stiffness and damping also become significant and the structure must be a
nalysed as a full two phase system. In this paper, two different fibrous ma
terials commonly used as fuselage thermal insulation are considered and a s
imple seismic experimental test configuration is modelled to verify the ana
lysis method. The structural frame properties are determined through vacuum
testing and the specific fluid induced effects are developed from flow res
istivity measurements. A finite element model of the two-phase system is fo
rmulated and the response of the model is shown to compare excellently with
experimental test results carried out under atmospheric conditions. (C) 19
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