Experimental Evaluation of Vibration-Based Damage Identification Methods on a Composite Aircraft Structure with Internally-Mounted Piezodiaphragm Sensors
Experimental Evaluation of Vibration-Based Damage Identification Methods on a Composite Aircraft Structure with Internally-Mounted Piezodiaphragm Sensors
| dc.contributor.author | Hwang, J.S. | en_US |
| dc.contributor.author | Loendersloot, R. | en_US |
| dc.contributor.author | Tinga, T. | en_US |
| dc.date.accessioned | 2016-05-20T11:55:51Z | |
| dc.date.available | 2016-05-20T11:55:51Z | |
| dc.date.issued | 2015 | en_US |
| dc.identifier.other | NLR-TP-2015-196 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/1070 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2015-196 | en_US |
| dc.subject.other | SM test facilities | en_US |
| dc.subject.other | Structural dynamics / vibration | en_US |
| dc.title | Experimental Evaluation of Vibration-Based Damage Identification Methods on a Composite Aircraft Structure with Internally-Mounted Piezodiaphragm Sensors | en_US |
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