지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 테크노프레스 Structural engineering and mechanics : An international journal Structural engineering and mechanics : An international journal 제15권 제2호
- 발행연도
- 2003.1
- 수록면
- 199 - 223 (25page)
이용수
초록· 키워드
오류제보하기
The formulation of a non-linear shear deformable shell element is presented for the solution of stability problems of stiffened plates and shells. The formulation of the geometrical stiffness presented here is exactly defined on the midsurface and is efficient for analyzing stability problems of thick plates and shells by incorporating bending moment and transverse shear resultant force. As a result of the explicit integration of the tangent stiffness matrix, this formulation is computationally very efficient in incremental nonlinear analysis. The element is free of both membrane and shear locking behaviour by using the assumed strain method such that the element performs very well in the thin shells. By using six degrees of freedom per node, the present element can model stiffened plate and shell structures. The formulation includes large displacement effects and elasto-plastic material behaviour. The material is assumed to be isotropic and elasto-plastic obeying Von Mises's yield condition and its associated flow rules. The results showed good agreement with references and computational efficiency.
목차
등록된 정보가 없습니다.
참고문헌 (0)
참고문헌 신청함께 읽어보면 좋을 논문
논문 유사도에 따라 DBpia 가 추천하는 논문입니다. 함께 보면 좋을 연관 논문을 확인해보세요!
-
An 8-node assumed strain element with explicit integration for isotropic and laminated composite shells
Structural engineering and mechanics : An international journal
2002 .01
-
A 4-node Shell Element with Enhanced Assumed Strain and Assumed Natural Strain
대한토목학회 학술대회
2006 .10
-
보강된 쉘 구조의 후좌굴 및 탄소성 유한요소해석
한국강구조학회지
1994 .12
-
An element-based 9-node resultant shell element for large deformation analysis of laminated composite plates and shells
Structural engineering and mechanics : An international journal
2004 .01
-
A refined finite element for first-order plate and shell analysis
Structural engineering and mechanics : An international journal
2011 .01
-
Buckling Analysis of Composite Plates and Shells using Finite Element Method
한국강구조학회지
1994 .06
-
Nonlinear Analysis of RC Structures using Assumed Strain RM Shell Element
ARCHITECTURAL RESEARCH
2014 .03
-
An extended finite element method for modeling elastoplastic FGM plate-shell type structures
Structural engineering and mechanics : An international journal
2018 .01
-
Defect-free 4-node flat shell element: NMS-4F element
Structural engineering and mechanics : An international journal
1999 .01
-
Elasto-plastic analysis using shell element considering geometric and material nonlinearities
Structural engineering and mechanics : An international journal
1998 .01
-
가정된 변형률장에 의한 쉘 구조물의 유한요소 해석에 관한 연구 ( A Study on the Finite Element Analysis of Shell Structures by the Assumed Strain Fields )
대한건축학회 학술발표대회 논문집 - 구조계
1995 .10
-
Geometrically Nonlinear Analysis of Hinged Cylindrical Laminated Composite Shells
복합신소재구조학회논문집
2012 .01
-
An accurate and efficient shell element with improved reduced integration rules
Structural engineering and mechanics : An international journal
1999 .01
-
The use of the strain approach to develop a new consistent triangular thin flat shell finite element with drilling rotation
Structural engineering and mechanics : An international journal
2018 .01
-
개구부가 있는 부재의 변위변환행렬을 이용한 비선형 해석
대한건축학회 논문집 - 구조계
2006 .12
-
Assumed strain quadrilateral C laminated plate element based on third-order shear deformation theory
Structural engineering and mechanics : An international journal
1999 .01
-
저차고체요소를 이용한 쉘 구조물의 자유진동해석에 대한 비교연구
대한건축학회 논문집 - 구조계
2005 .04
-
Stresses analyses of shell structure with large holes
Structural engineering and mechanics : An international journal
1998 .01
-
선형 Solid-shell 을 이용한 용접해석
대한기계학회 춘추학술대회
2004 .04
-
곡선쉘 유한요소를 이용한 보강된 적층판 및 쉘구조의 탄·소성 좌굴해석
한국강구조학회지
1996 .03
이 논문의 저자 정보
최근 본 자료
댓글(0)
0