Results of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edges

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dc.contributor.authorDassen, T.en_US
dc.contributor.authorParchen, R.en_US
dc.contributor.authorBruggeman, J.en_US
dc.contributor.authorHagg, F.en_US
dc.date.accessioned2017-02-14T10:39:52Z
dc.date.available2017-02-14T10:39:52Z
dc.date.issued1996en_US
dc.identifier.otherNLR-TP-1996-350en_US
dc.identifier.urihttp://hdl.handle.net/10921/1359
dc.language.isonlen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;1996-350en_US
dc.subject.otherAeroacousticsen_US
dc.subject.otherWindtunnelsen_US
dc.titleResults of a wind tunnel study on the reduction of airfoil self-noise by the application of serrated blade trailing edgesen_US

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