DC Field | Value | Language |
---|---|---|
dc.contributor.author | 조원만 | ko |
dc.contributor.author | 이영신 | ko |
dc.contributor.author | 윤성기 | ko |
dc.date.accessioned | 2013-02-27T05:25:36Z | - |
dc.date.available | 2013-02-27T05:25:36Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1993-01 | - |
dc.identifier.citation | 대한기계학회논문집 A, v.17, no.8, pp.2051 - 2060 | - |
dc.identifier.issn | 1226-4873 | - |
dc.identifier.uri | http://hdl.handle.net/10203/66705 | - |
dc.description.abstract | A finite element program using degenerated shell element was developed to solve the geometric, material and combined nonlinear behaviors of composite laminated shell. The total Lagrangian method was implemented for geometric nonlinear analysis. The material nonlinear behavior was analyzed by considering the matrix degradation due to the progressive failure in the matrix and matrix-fiber interface after initial failure. The result of the geometric nonlinear analysis showed good agreement with the other exact and numerical solutions. The results of the combined analyses considered both geometric and material nonlinear analyses were compared with the experiments in which internal pressure was applied to the filament wound antisymmetric tubes. | - |
dc.language | Korean | - |
dc.publisher | 대한기계학회 | - |
dc.title | 복합재 적층셸의 비선형 수치해석 및 실험 | - |
dc.title.alternative | Nonlinear Numerical Analysis and Experiment of Composite Laminated Shell | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 17 | - |
dc.citation.issue | 8 | - |
dc.citation.beginningpage | 2051 | - |
dc.citation.endingpage | 2060 | - |
dc.citation.publicationname | 대한기계학회논문집 A | - |
dc.contributor.localauthor | 윤성기 | - |
dc.contributor.nonIdAuthor | 조원만 | - |
dc.contributor.nonIdAuthor | 이영신 | - |
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