Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/92136
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dc.contributorDepartment of Mechanical Engineering-
dc.creatorShen, C-
dc.creatorYang, S-
dc.creatorFan, HKH-
dc.creatorLeung, RCK-
dc.date.accessioned2022-02-08T02:18:13Z-
dc.date.available2022-02-08T02:18:13Z-
dc.identifier.issn1070-9622-
dc.identifier.urihttp://hdl.handle.net/10397/92136-
dc.language.isoenen_US
dc.publisherHindawi Publishing Corporationen_US
dc.rights© 2021 Cheng Shen et al. This is an open access article distributed under the Creative Commons Attribution License (https://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.en_US
dc.rightsThe following publication Cheng Shen, Shasha Yang, Harris K. H. Fan, Randolph C. K. Leung, "Investigation on a Duct Noise Control Method through Membranes in Tandem", Shock and Vibration, vol. 2021, Article ID 5533228, 6 pages, 2021 is available at https://doi.org/10.1155/2021/5533228en_US
dc.titleInvestigation on a duct noise control method through membranes in tandemen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage1-
dc.identifier.epage6-
dc.identifier.volume2021-
dc.identifier.doi10.1155/2021/5533228-
dcterms.abstractDuct noise control is an important practical problem. This paper explores the vibro-acoustic mechanism of duct noise through the membrane in tandem. Validity and feasibility of the proposed analytical model is demonstrated by comparing existing simplified models and full direct aeroacoustic simulation solved with the CE/SE model. It is shown that the coupling effect between two membranes in tandem is not negligible to predict system response. Moreover, introduction of multimembranes is important or even the only efficient way to apply this passive control method in practice.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationShock and vibration, 2021, v. 2021, 5533228, p. 1-6-
dcterms.isPartOfShock and vibration-
dcterms.issued2021-
dc.identifier.scopus2-s2.0-85111511033-
dc.identifier.eissn1875-9203-
dc.identifier.artn5533228-
dc.description.validate202202 bcvc-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Scopus/WOSen_US
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextThis work was supported by the National Natural Science Foundation of China (11502110), Open Fund of the State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi?an Jiaotong University (nos. SV2018-KF-01 and SV2018-KF-22), and Open Project of Space Structure and Mechanism Technology Laboratory of China Aerospace Science and Technology Group Co., Ltd. The third and fourth authors are grateful to the support from the Research Grants Council of the Government of Hong Kong Special Administrative Region, under Grant no. A-PolyU 503/15.en_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryCCen_US
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