Unsteady leading edge suction effects on rotor-stator interaction noise

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dc.contributor.authorSchulten, J.B.H.M.en_US
dc.date.accessioned2017-02-03T13:10:12Z
dc.date.available2017-02-03T13:10:12Z
dc.date.issued1999en_US
dc.identifier.otherNLR-TP-1999-064en_US
dc.identifier.urihttp://hdl.handle.net/10921/1116
dc.language.isonlen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;1999-064en_US
dc.subject.otherAeroacousticsen_US
dc.subject.otherTurbomachinery flowen_US
dc.titleUnsteady leading edge suction effects on rotor-stator interaction noiseen_US

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