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Optimum Sound Attenuation in Flow Ducts Based on the "Exact" Cremer Impedance
KTH, Skolan för teknikvetenskap (SCI), Farkost och flyg.
KTH, Skolan för teknikvetenskap (SCI), Farkost och flyg, MWL Vibrationsövervakning.ORCID-id: 0000-0001-7898-8643
2016 (engelsk)Inngår i: Acta Acoustica united with Acustica, ISSN 1610-1928, E-ISSN 1861-9959, Vol. 102, nr 5, s. 851-860Artikkel i tidsskrift (Fagfellevurdert) Published
Abstract [en]

The Cremer impedance (Acustica 3, 1953) [1] is the locally reacting boundary condition that maximizes the attenuation of a certain mode in a uniform wave guide taken as the lowest order mode or "plane" wave. This paper presents the analysis of the "exact" Cremer impedance model, i.e., the high frequency asymptotic results proposed by Tester for uniform mean flow (JSV 28(2), 1973) [2] are extended to lower frequencies. It is shown that significantly larger attenuation per unit length can be obtained using the exact instead of the asymptotic solution. However, for sufficiently low frequencies the "exact" Cremer solution and optimum attenuation is requiring a wall impedance with a negative real part, i.e. an active boundary. In addition, the effect of a finite length on the resulting attenuation is studied using a finite element method for solving the convected wave equation. Finally, it is demonstrated how a silencer can be built that realize the optimum Cremer impedance at a given frequency by using a micro-perforated panel and locally reacting cavities. The performance of the optimized silencer is determined experimentally and the results are compared to the prediction of the finite element model.

sted, utgiver, år, opplag, sider
S HIRZEL VERLAG , 2016. Vol. 102, nr 5, s. 851-860
HSV kategori
Identifikatorer
URN: urn:nbn:se:kth:diva-193815DOI: 10.3813/AAA.918999ISI: 000383241200008Scopus ID: 2-s2.0-84987835325OAI: oai:DiVA.org:kth-193815DiVA, id: diva2:1039510
Merknad

QC 20161024

Tilgjengelig fra: 2016-10-24 Laget: 2016-10-11 Sist oppdatert: 2017-11-29bibliografisk kontrollert
Inngår i avhandling
1. Turbocharger Aeroacoustics and Optimal Damping of Sound
Åpne denne publikasjonen i ny fane eller vindu >>Turbocharger Aeroacoustics and Optimal Damping of Sound
2017 (engelsk)Doktoravhandling, med artikler (Annet vitenskapelig)
sted, utgiver, år, opplag, sider
KTH Royal Institute of Technology, 2017. s. 79
Serie
TRITA-AVE, ISSN 1651-7660 ; 2017:36
HSV kategori
Forskningsprogram
Fysik
Identifikatorer
urn:nbn:se:kth:diva-207151 (URN)978-91-7729-442-9 (ISBN)
Disputas
2017-06-09, sal E3, Osquars backe 14, KTH-Campus, Stockholm, 10:15 (engelsk)
Opponent
Veileder
Merknad

QC 20170517

Tilgjengelig fra: 2017-05-17 Laget: 2017-05-17 Sist oppdatert: 2017-05-17bibliografisk kontrollert

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