DC Field | Value | Language |
---|---|---|
dc.contributor.author | 조창민 | ko |
dc.contributor.author | 홍창선 | ko |
dc.date.accessioned | 2013-02-27T03:35:14Z | - |
dc.date.available | 2013-02-27T03:35:14Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1985-08 | - |
dc.identifier.citation | 한국항공우주학회지, v.13, no.2, pp.17 - 31 | - |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | http://hdl.handle.net/10203/66214 | - |
dc.description.abstract | A finite element formulation for the analysis of fiber reinforced laminated shell structures is presented. The element adopted is a doubly curved 8-node shell element. Shear deformation and coupling terms between bending and extension are included in the formulation. Numerical characteristics of the element with respect to mesh size are checked for a plate with various boundary conditions and a pinched cylinder. Also degeneracy due to thinness of a pinched cylinder is examined. The developed element has demonstrated its applicability by showing the effect of anisotropy on the hoop stress and the displacements for a laminated composite cylinder and the effect of material properties and boundary conditions on the stresses. In addition to the stress analysis, a routine for the interactive first-ply failure load of combined internal pressure and axial tension for some laminated cylinders is also developed. | - |
dc.language | English | - |
dc.publisher | 한국항공우주학회 | - |
dc.title | 복합적층쉘의 유한요소해석 | - |
dc.title.alternative | Finite Element Analysis of Laminated Composite Shell | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 13 | - |
dc.citation.issue | 2 | - |
dc.citation.beginningpage | 17 | - |
dc.citation.endingpage | 31 | - |
dc.citation.publicationname | 한국항공우주학회지 | - |
dc.contributor.localauthor | 홍창선 | - |
dc.contributor.nonIdAuthor | 조창민 | - |
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