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Numerical investigation of the optimum placement locations of optical Fiber Bragg Grating sensors for the health monitoring of bonded composite repairs

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dc.contributor.author Tsamasphyros, G en
dc.contributor.author Kanderakis, GN en
dc.contributor.author Vrettos, C en
dc.contributor.author Kalkanis, K en
dc.date.accessioned 2014-03-01T02:44:52Z
dc.date.available 2014-03-01T02:44:52Z
dc.date.issued 2007 en
dc.identifier.issn 10221360 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/31983
dc.subject Adhesive debonding en
dc.subject Bonded composite repair en
dc.subject FEA en
dc.subject Fiber bragg gratings sensors en
dc.subject Structural health monitoring en
dc.subject.other Bond strength (materials) en
dc.subject.other Composite materials en
dc.subject.other Computer simulation en
dc.subject.other Elasticity en
dc.subject.other Fiber Bragg gratings en
dc.subject.other Structural health monitoring en
dc.subject.other Adhesive debonding en
dc.subject.other Bonded composite repairs en
dc.subject.other Fiber bragg gratings sensors en
dc.subject.other Fiber optic sensors en
dc.title Numerical investigation of the optimum placement locations of optical Fiber Bragg Grating sensors for the health monitoring of bonded composite repairs en
heal.type conferenceItem en
heal.identifier.primary 10.1002/masy.200750125 en
heal.identifier.secondary http://dx.doi.org/10.1002/masy.200750125 en
heal.publicationDate 2007 en
heal.abstract the use of optical Fiber Bragg Grating sensors (FBG) embedded into composite laminates has proven to be an efficient way for the monitoring of the strain field inside composite laminates. The current work focuses on the use of such sensors for structural health monitoring of bonded composite repairs, often used in the aerospace as well as in the maritime industry. In such applications, the embedding location of the FBG sensors is of great importance, since apart from general strain measurements of the composite, they provide the ability of detecting whether a crack has propagated in the metal or a debonding has occurred between the metal and the composite. Within the current work, a representative case of bonded composite repair of a cracked metallic structure is examined and a series of 3D elasticity linear static finite element models are developed. Various crack lengths and patch disbond sizes have been studied while varying strain distributions were recorded along numerous paths inside the structure. Having recorded and analyzed these strain distributions, certain guidelines have been derived concerning the optimum FBG placement inside the patch, in order to ensure efficient structural health monitoring. Copyright © 2007 WILEY-VCH Verlag GmbH & Co. KGaA. en
heal.journalName Macromolecular Symposia en
dc.identifier.doi 10.1002/masy.200750125 en
dc.identifier.volume 247 en
dc.identifier.spage 221 en
dc.identifier.epage 229 en


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