Three-dimensional crack analysis in aeronautical structures using the substructured finite element / extended finite element method
In this thesis, we have developed a Subtructured Finite Element / eXtended Finite Element (S-FE/XFE) method. The S-FE/XFE method consists in decomposing the geometry into safe FE-domains and cracked XFE-domains, and solving the interface problem with the Finite Element Tearing and Interconnecting me...
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Format: | Others |
Language: | en |
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Universite catholique de Louvain
2007
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Online Access: | http://edoc.bib.ucl.ac.be:81/ETD-db/collection/available/BelnUcetd-03222007-182311/ |