Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/106468
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dc.contributorDepartment of Mechanical Engineeringen_US
dc.creatorFan, HKHen_US
dc.creatorLeung, RCKen_US
dc.creatorLam, GCYen_US
dc.creatorAurégan, Yen_US
dc.creatorDai, Xen_US
dc.date.accessioned2024-05-09T00:53:43Z-
dc.date.available2024-05-09T00:53:43Z-
dc.identifier.issn0001-1452en_US
dc.identifier.urihttp://hdl.handle.net/10397/106468-
dc.language.isoenen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics, Inc.en_US
dc.rightsCopyright © 2018 by Randolph C. K. Leung and Yves Aurégan. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.en_US
dc.rightsThis is the peer reviewed version of the following article: Fan, H. K. H., Leung, R. C. K., Lam, G. C. Y., Aurégan, Y., & Dai, X. (2018). Numerical Coupling Strategy for Resolving In-Duct Elastic Panel Aeroacoustic/Structural Interaction. AIAA Journal, 56(12), 5033-5040, which has been published in final form at https://doi.org/10.2514/1.J057324.en_US
dc.titleNumerical coupling strategy for resolving in-duct elastic panel aeroacoustic/structural interactionen_US
dc.typeJournal/Magazine Articleen_US
dc.description.otherinformationTitle on author’s file: Coupling Strategy for Resolving In-duct Elastic Panel Aeroacoustic-Structural Interaction with CE/SE Methoden_US
dc.identifier.spage5033en_US
dc.identifier.epage5040en_US
dc.identifier.volume56en_US
dc.identifier.issue12en_US
dc.identifier.doi10.2514/1.J057324en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationAIAA journal, Dec. 2018, v. 56, no. 12, p. 5033-5040en_US
dcterms.isPartOfAIAA journalen_US
dcterms.issued2018-12-
dc.identifier.scopus2-s2.0-85063188072-
dc.identifier.eissn1533-385Xen_US
dc.description.validate202405 bcchen_US
dc.description.oaAccepted Manuscripten_US
dc.identifier.FolderNumberME-0562-
dc.description.fundingSourceRGCen_US
dc.description.pubStatusPublisheden_US
dc.identifier.OPUS21778911-
dc.description.oaCategoryGreen (AAM)en_US
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