유한요소법에 의한 복합적층 원통쉘의 좌굴해석 Buckling Analysis of Laminated Composite Cylindrical Shell by the Finite Element Method

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Publisher
한국항공우주학회
Issue Date
1984-04
Language
Korean
Citation

한국항공우주학회지, v.12, no.1, pp.85 - 94

ISSN
1225-1348
URI
http://hdl.handle.net/10203/63462
Appears in Collection
AE-Journal Papers(저널논문)
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