This paper deals with aero-vibroacoustical effects on the sunroof panel of an automobile.Reductions in internal noise due to panel flexibility have been measured experimentally by the German Consortium of Automobile Manufacturers. Methods for predicting this acoustical impedance due to the structure range from one-way coupling between the flow source excitation and stochastic models of the structural response, to two-way coupling between both the fluid and structural systems. We demonstrate here the use of the Finite Volume method to solve the fully coupled fluid-structure interaction, and thereby directly predict reductions in sunroof buffeting noise due to aero-vibroacoustic interaction with flexible panels. In this paper, we also take the first steps towards analysing the separation between convective and acoustical mechanisms, important for a deeper understanding of how the flow excites the structure. We use spatial Fourier analysis to illustrate the differing wave numbers associated with the flow and acoustics, arising from the single vortex shedding source in two dimensional compressible flow over a cylinder.
NomenclaturedB = deciBel, measure of the intensity of Sound Pressure Level SPL = Sound Pressure Level SEA = Statistical Energy Analysis FEM = Finite Element Method BEM = Boundary Element Method FV = Finite Volume method u = Solid displacement field vector v = Velocity field vector s = Solid stress tensor field e = Strain field b = Body force vector T = Temperature field