Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/19015
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dc.contributor.authorBiedermann, TM-
dc.contributor.authorHintzen, N-
dc.contributor.authorKameier, F-
dc.contributor.authorChong, TP-
dc.contributor.authorPaschereit, CO-
dc.coverage.spatialAtlanta, Georgia, USA-
dc.date.accessioned2019-08-27T12:41:51Z-
dc.date.available2018-06-25-
dc.date.available2019-08-27T12:41:51Z-
dc.date.issued2018-06-25-
dc.identifier.citationAIAA Paper 2018–2803, 2018en_US
dc.identifier.issnhttp://dx.doi.org/10.2514/6.2018-2956-
dc.identifier.urihttp://bura.brunel.ac.uk/handle/2438/19015-
dc.language.isoenen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.source2018 AIAA/CEAS Aeroacoustics Conference-
dc.source2018 AIAA/CEAS Aeroacoustics Conference-
dc.titleOn the transfer of leading edge serrations from isolated aerofoil to ducted low-pressure fan applicationen_US
dc.typeConference Paperen_US
dc.identifier.doihttp://dx.doi.org/10.2514/6.2018-2956-
dc.relation.isPartOfAIAA Paper 2018–2803-
pubs.finish-date2018-06-29-
pubs.finish-date2018-06-29-
pubs.publication-statusPublished-
pubs.start-date2018-06-25-
pubs.start-date2018-06-25-
Appears in Collections:Dept of Electronic and Electrical Engineering Research Papers

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