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dc.contributor.authorGrooteman, F.P.en_US
dc.contributor.authorSchippers, H.en_US
dc.contributor.authorBoer, A. deen_US
dc.date.accessioned2017-02-14T10:39:52Z
dc.date.available2017-02-14T10:39:52Z
dc.date.issued1996en_US
dc.identifier.otherNLR-TP-1996-504en_US
dc.identifier.urihttp://hdl.handle.net/10921/1374
dc.language.isonlen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;1996-504en_US
dc.subject.otherNumerical analysisen_US
dc.subject.otherStructural dynamics / vibrationen_US
dc.titleA symmetrical boundary element formulation for sound transmission through fuselage walls -theory, implemetation and test cases-en_US


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