Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/14404
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dc.contributor.authorBiedermann, TM-
dc.contributor.authorChong, TP-
dc.contributor.authorKameier, F-
dc.contributor.authorPaschereit, CO-
dc.date.accessioned2017-04-11T11:20:30Z-
dc.date.available2017-04-11T11:20:30Z-
dc.date.issued2017-
dc.identifier.citationAIAA Journalen_US
dc.identifier.issn0001-1452-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/14404-
dc.description.sponsorshipQuiet Aerofoils of the Next Generation-
dc.language.isoenen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics, (2017) 55(9): 3128 - 3142en_US
dc.rightsCopyright © 2017 by Till Biedermann and Tze Pei Chong. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.-
dc.titleStatistical-Empirical Modelling of Airfoil Noise Subjected to Leading Edge Serrationsen_US
dc.typeArticleen_US
dc.identifier.doihttps://doi.org/10.2514/1.J055633-
dc.relation.isPartOfAIAA Journal-
pubs.publication-statusPublished-
Appears in Collections:Dept of Mechanical and Aerospace Engineering Research Papers

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