Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/740
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dc.contributor.authorKirby, R-
dc.coverage.spatial37en
dc.date.accessioned2007-05-08T11:20:20Z-
dc.date.available2007-05-08T11:20:20Z-
dc.date.issued2003-
dc.identifier.citationJournal of the Acoustical Society of America 114 (1): 200 - 209, Jul 2003en
dc.identifier.issn0001-4966-
dc.identifier.urihttp://bura.brunel.ac.uk/handle/2438/740-
dc.description.abstractA numerical technique is developed for the analysis of dissipative silencers of arbitrary, but axially uniform, cross section. Mean gas flow is included in a central airway which is separated from a bulk reacting porous material by a concentric perforate screen. The analysis begins by employing the finite element method to extract the eigenvalues and associated eigenvectors for a silencer of infinite length. Point collocation is then used to match the expanded acoustic pressure and velocity fields in the silencer chamber to those in the inlet and outlet pipes. Transmission loss predictions are compared with experimental measurements taken for two automotive dissipative silencers with elliptical cross sections. Good agreement between prediction and experiment is observed both without mean flow and for a mean flow Mach number of 0.15. It is demonstrated also that the technique presented offers a considerable reduction in computational expenditure when compared to a three dimensional finite element analysis.en
dc.format.extent267051 bytes-
dc.format.mimetypeapplication/pdf-
dc.language.isoen-
dc.publisherAmerican Institute of Physicsen
dc.subjectDissipative silencersen
dc.subjectMean flowen
dc.subjectArbitrary cross sectionen
dc.subjectPoint collocationen
dc.subjectAutomotive silenceren
dc.titleTransmission loss predictions for dissipative silencers of arbitrary cross section in the presence of mean flowen
dc.typeResearch Paperen
dc.identifier.doihttp://dx.doi.org/10.1121/1.1582448-
Appears in Collections:Mechanical and Aerospace Engineering
Dept of Mechanical and Aerospace Engineering Research Papers

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