Publication:
Aircraft Fuselage Controled by 245 Tuned Vibration Absorbers

cris.virtual.departmentMechatronik
cris.virtual.department#PLACEHOLDER_PARENT_METADATA_VALUE#
cris.virtual.departmentbrowseMechatronik
cris.virtual.departmentbrowseMechatronik
cris.virtualsource.department78c40bb4-440b-4e70-a918-f0d50570078e
cris.virtualsource.department#PLACEHOLDER_PARENT_METADATA_VALUE#
dc.contributor.authorSachau, Delf
dc.contributor.authorKöhne, Clemens
dc.date.issued2017
dc.description.versionNA
dc.identifier.citationEnthalten in: INTER-NOISE 2017. - Hong Kong : Polytechnic University, 2017. - 2017, Seite 5857-5868
dc.identifier.urihttps://openhsu.ub.hsu-hh.de/handle/10.24405/5977
dc.language.isoen
dc.publisherPolytechnic University
dc.relation.conference46th International Congress and Exposition on Noise Control Engineering : INTER-NOISE 2017
dc.relation.orgunitMechatronik
dc.rights.accessRightsmetadata only access
dc.titleAircraft Fuselage Controled by 245 Tuned Vibration Absorbers
dc.typeConference paper
dcterms.bibliographicCitation.originalpublisherplaceHong Kong
dspace.entity.typePublication
hsu.uniBibliography
oaire.citation.endPage5868
oaire.citation.startPage5857
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