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dc.contributor.authorHuang, Lin
dc.contributor.authorHe, Rongguang
dc.contributor.authorZeng, Zhiwei
dc.contributor.author曾志伟
dc.date.accessioned2013-03-18T03:19:52Z
dc.date.available2013-03-18T03:19:52Z
dc.date.issued2012-07
dc.identifier.citationIEEE TRANSACTIONS ON MAGNETICS,2012,48(7):2161-2165zh_CN
dc.identifier.issn0018-9464
dc.identifier.urihttp://dx.doi.org/10.1109/TMAG.2012.2186311
dc.identifier.uriWOS:000305834100007
dc.identifier.urihttps://dspace.xmu.edu.cn/handle/2288/15153
dc.description.abstractThis paper presents a new finite element (FE) model for three-dimensional simulation of eddy current testing of aircraft skin structure. More specifically, scanning of ferrite-core probe over aluminum plates riveted by steel fasteners is simulated. The model uses different FE meshes to discretize the ferrite core, the aluminum plates, and the fasteners. The coil is not meshed. The reduced magnetic vector potential generated by the induced currents and/or magnetization in each domain is calculated and updated by an iterative procedure. Re-meshing due to changing probe position in conventional models is avoided. Efficiency of the model is demonstrated.zh_CN
dc.language.isoenzh_CN
dc.publisherIEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INCzh_CN
dc.subjectAircraft skin structurezh_CN
dc.subjecteddy current testingzh_CN
dc.subjectextended iterative modelzh_CN
dc.subjectfinite element methodzh_CN
dc.titleAn Extended Iterative Finite Element Model for Simulating Eddy Current Testing of Aircraft Skin Structurezh_CN
dc.typeArticlezh_CN


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