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Iterative Component Mode Synthesis Using a Priori and a Posteriori Criteria

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dc.contributor.authorKim, Soo Min-
dc.contributor.authorKim, Jin-Gyun-
dc.contributor.authorPark, K. C.-
dc.contributor.authorChae, Soo-Won-
dc.date.accessioned2021-09-01T15:48:19Z-
dc.date.available2021-09-01T15:48:19Z-
dc.date.created2021-06-19-
dc.date.issued2019-05-
dc.identifier.issn0001-1452-
dc.identifier.urihttps://scholar.korea.ac.kr/handle/2021.sw.korea/65890-
dc.description.abstractAn iterative algorithm of component mode synthesis for a rational reduced-order modeling is proposed. The present algorithm consists of three steps: initial mode selection with a priori criterion, model reduction using the selected modes, and a posteriori error evaluation. The algorithm is based on the Craig-Bampton method, which is one of the most widely used techniques. Specifically, the present algorithm uses, in a judicious manner, both an a priori mode selection criterion employing the moment-matching strategy and an a posteriori error estimation technique in evaluating the relative eigenvalue errors. If desired, an optional step of boundary interface reduction offers an additional possibility of obtaining a more compact model. The proposed iterative algorithm is recommended to researchers as well as commercialized software users in developing linear reduced-order structural dynamics models. Numerical examples are presented for its practical usage and performance.-
dc.languageEnglish-
dc.language.isoen-
dc.publisherAMER INST AERONAUTICS ASTRONAUTICS-
dc.subjectCRAIG-BAMPTON METHOD-
dc.subjectINTERFACE-REDUCTION-
dc.subjectSELECTION-
dc.subjectSUBSTRUCTURES-
dc.subjectSUBSYSTEMS-
dc.subjectFRAMEWORK-
dc.titleIterative Component Mode Synthesis Using a Priori and a Posteriori Criteria-
dc.typeArticle-
dc.contributor.affiliatedAuthorChae, Soo-Won-
dc.identifier.doi10.2514/1.J057661-
dc.identifier.scopusid2-s2.0-85078038705-
dc.identifier.wosid000484818400031-
dc.identifier.bibliographicCitationAIAA JOURNAL, v.57, no.5, pp.2145 - 2157-
dc.relation.isPartOfAIAA JOURNAL-
dc.citation.titleAIAA JOURNAL-
dc.citation.volume57-
dc.citation.number5-
dc.citation.startPage2145-
dc.citation.endPage2157-
dc.type.rimsART-
dc.type.docTypeArticle-
dc.description.journalClass1-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryEngineering, Aerospace-
dc.subject.keywordPlusCRAIG-BAMPTON METHOD-
dc.subject.keywordPlusINTERFACE-REDUCTION-
dc.subject.keywordPlusSELECTION-
dc.subject.keywordPlusSUBSTRUCTURES-
dc.subject.keywordPlusSUBSYSTEMS-
dc.subject.keywordPlusFRAMEWORK-
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