Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/106352
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dc.contributorDepartment of Mechanical Engineering-
dc.creatorArif, I-
dc.creatorWu, D-
dc.creatorLam, GCY-
dc.creatorLeung, RCK-
dc.date.accessioned2024-05-09T00:52:57Z-
dc.date.available2024-05-09T00:52:57Z-
dc.identifier.urihttp://hdl.handle.net/10397/106352-
dc.language.isoenen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics, Inc.en_US
dc.rightsCopyright (c) 2020 by Randolph C. K. Leung and Garret C. Y. Lam. 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: Arif, I., Wu, D., Lam, G. C. Y., & Leung, R. C. K. (2020). Exploring Airfoil Tonal Noise Reduction with Elastic Panel Using Perturbation Evolution Method. AIAA Journal, 58(11), 4958-4968, which has been published in final form at https://doi.org/10.2514/1.J059191.en_US
dc.titleExploring airfoil tonal noise reduction with elastic panel using perturbation evolution methoden_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage4958-
dc.identifier.epage4968-
dc.identifier.volume58-
dc.identifier.issue11-
dc.identifier.doi10.2514/1.J059191-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationAIAA journal, Nov. 2020, v. 58, no. 11, p. 4958-4968-
dcterms.isPartOfAIAA journal-
dcterms.issued2020-11-
dc.identifier.scopus2-s2.0-85095117462-
dc.identifier.eissn0001-1452-
dc.description.validate202405 bcch-
dc.description.oaAccepted Manuscripten_US
dc.identifier.FolderNumberME-0220en_US
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextPhilip K. H. Wong Foundation; The Hong Kong Polytechnic Universityen_US
dc.description.pubStatusPublisheden_US
dc.identifier.OPUS26459330en_US
dc.description.oaCategoryGreen (AAM)en_US
Appears in Collections:Journal/Magazine Article
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