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

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Autoria(s): Hwang, J.S.; Loendersloot, R.; Tinga, T.

Data(s)	20/05/2016 20/05/2016 2015
Identificador	NLR-TP-2015-196 http://hdl.handle.net/10921/1070
Idioma(s)	en
Publicador	National Aerospace Laboratory NLR
Relação	NLR Technical Publication;2015-196
Palavras-Chave	#SM test facilities #Structural dynamics / vibration