Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/102544
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dc.contributorDepartment of Civil and Environmental Engineeringen_US
dc.creatorLi, Len_US
dc.creatorXia, Yen_US
dc.creatorChen, Gen_US
dc.date.accessioned2023-10-26T07:19:20Z-
dc.date.available2023-10-26T07:19:20Z-
dc.identifier.issn0893-1321en_US
dc.identifier.urihttp://hdl.handle.net/10397/102544-
dc.language.isoenen_US
dc.publisherAmerican Society of Civil Engineersen_US
dc.rights© 2018 American Society of Civil Engineers.en_US
dc.rightsThis material may be downloaded for personal use only. Any other use requires prior permission of the American Society of Civil Engineers. This material may be found at https://ascelibrary.org/doi/10.1061/(ASCE)AS.1943-5525.0000876.en_US
dc.subjectCondition monitoringen_US
dc.subjectDebondingen_US
dc.subjectElectromechanical impedance (EMI) techniqueen_US
dc.subjectFiber-reinforced polymer (FRP)en_US
dc.subjectPiezoelectricen_US
dc.titleExperimental and numerical studies of debonding monitoring of FRP shear-strengthened beams using EMI techniqueen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.volume31en_US
dc.identifier.issue5en_US
dc.identifier.doi10.1061/(ASCE)AS.1943-5525.0000876en_US
dcterms.abstractFiber-reinforced polymer (FRP) is commonly used to strengthen or retrofit reinforced concrete (RC) structures. FRP debonding may initially occur around tiny cracks and then propagate to other parts of the structure, ultimately leading to the brittle failure of the strengthened structure. Therefore, the secure bonding of FRP onto the strengthened structure should be closely monitored using a reliable approach. In this study, an electromechanical impedance (EMI) technique is applied to monitor early FRP debonding in FRP shear-strengthened RC beams through experimental and numerical studies. Lead zirconate titanate (PZT) patches and strain gauges were bonded onto the surface of the FRP. The admittance and strain data were then collected and used to assess the FRP bonding condition. As the loads were increased, the beams began cracking, leading to FRP debonding and subsequent brittle failure of the beams. A root-mean square deviation index was adopted to quantify the debonding severity. The admittance data of the PZT patches were found more advantageous than the strain data and visual inspection to detect the debonding initiation. The EMI technique was then simulated through finite-element analysis. The FRP-concrete interface was modeled using a bond-slip model. Infinite elements were used to eliminate wave reflections at boundaries. The experimental and numerical results validate the effectiveness of the EMI technique in monitoring FRP debonding.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationJournal of aerospace engineering, Sept 2018, v. 31, no. 5, 04018048en_US
dcterms.isPartOfJournal of aerospace engineeringen_US
dcterms.issued2018-09-
dc.identifier.scopus2-s2.0-85047270052-
dc.identifier.eissn1943-5525en_US
dc.identifier.artn04018048en_US
dc.description.validate202310 bcchen_US
dc.description.oaAccepted Manuscripten_US
dc.identifier.FolderNumberCEE-1706-
dc.description.fundingSourceOthersen_US
dc.description.fundingTextHong Kong Polytechnic University; National Natural Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.identifier.OPUS6840825-
dc.description.oaCategoryGreen (AAM)en_US
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