돔형 스페이스 프레임의 부재강성변화에 따른 임계좌굴하중과 유효좌굴길이계수

서지정보

ㆍ발행기관 : 한국공간구조학회 ㆍ수록지정보 : 한국공간구조학회지 / 13권 / 1호
ㆍ저자명 : 손수덕, 이승재

목차

Abstract
1. 서 론
2. 접선강성행렬과 임계점
3. 불안정 현상과 좌굴하중의 특성
3.1 육각뿔 모델의 임계하중과 좌굴길이
3.1 스타돔의 경계조건과 유효좌굴길이
4. 결 론
감사의 글
참고문헌

영어 초록

This study investigated characteristics of buckling load and effective buckling length by member rigidity of dome-typed space frame which was sensitive to initial conditions. A critical point and a buckling load were computed by analyzing the eigenvalues and determinants of the tangential stiffness matrix. The hexagonal pyramid model and star dome were selected for the case study in order to examine the nodal buckling and member buckling in accordance with member rigidity. From the numerical results, an effective buckling length factor of adopted models was bigger than that of Euler buckling for the case of fixed boundary. These numerical models indicated that the influence of nodal buckling was greater than that of member buckling as member rigidity was higher. Besides, there was a tendency that the bifurcation appeared on the equilibrium path before limit point in the member buckling model.

참고 자료

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