Experimental Evaluation of Vibration-Based Damage Identification Methods on a Composite Aircraft Structure with Internally-Mounted Piezodiaphragm Sensors

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dc.contributor.authorHwang, J.S.en_US
dc.contributor.authorLoendersloot, R.en_US
dc.contributor.authorTinga, T.en_US
dc.date.accessioned2016-05-20T11:55:51Z
dc.date.available2016-05-20T11:55:51Z
dc.date.issued2015en_US
dc.identifier.otherNLR-TP-2015-196en_US
dc.identifier.urihttp://hdl.handle.net/10921/1070
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2015-196en_US
dc.subject.otherSM test facilitiesen_US
dc.subject.otherStructural dynamics / vibrationen_US
dc.titleExperimental Evaluation of Vibration-Based Damage Identification Methods on a Composite Aircraft Structure with Internally-Mounted Piezodiaphragm Sensorsen_US

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