• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2005년도 추계 학술발표회 제17권2호
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• pp.25-28
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• 2005

The elastic buckling load or strength of a concentrically loaded slender metal column may be increased many times by reinforcing it with an assemblage of pretensioned stays and rigidity connected crossarm members. The complete system is herein referred to as a 'stayed column'. The purpose of the pretensioned stays and crossarm members is to introduce, at several points along the length of the column, restraint against translation and rotation and thereby decrease the effective unsupported buckling length of the column. This paper verifies that pretensioned cable of stayed column is effective for cyclic load and increases strength of shear wall against earthquake by reinforcing side of wall. Design process of stayed column which satisfies demanded capacity and ductility of wall is presented by analyzing result of experiment.

• Composites Research
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• 제25권1호
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• pp.19-25
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• 2012

본 연구에서는 압축하중을 받는 원공을 가진 샌드위치 복합재 기둥의 좌굴 거동을 조사하였다. 샌드위치 복합재 기둥은 유리섬유직물/에폭시 면재와 우레탄 폼 심재로 구성되어 있다. 이때 면재 두께는 1.7mm, 심재 두께는 23mm, 37mm, 48mm, 61mm, 그리고 원공 직경은 25mm와 38mm를 고려하였다. 원공 위치가 샌드위치 복합재 기둥의 좌굴 거동에 미치는 영향을 조사하기 위해 직경 25mm인 원공이 시편중앙부에 있는 경우, 시편중앙부를 기준으로 중앙부와 끝단 사이의 1/4 지점에 있는 경우, 시편중앙부를 기준으로 중앙부와 끝단 사이의 1/2 지점에 있는 경우를 고려하였다. 시편중앙부에 직경 25mm인 원공이 있는 경우의 좌굴하중과 최대하중은 원공이 없는 경우보다 10% 정도 낮게 나타나며, 시편중앙부에 직경 38mm인 원공이 있는 경우의 좌굴하중과 최대하중은 원공이 없는 경우보다 30% 정도 낮게 나타났다. 그러나 원공 위치가 좌굴하중과 최대하중에 미치는 영향은 크지 않았다. 주요 파괴 모드는 심재 두께가 23mm와 37mm와 같이 얇은 경우는 심재 전단파괴가 지배적이고 심재 두께가 48mm와 61mm와 같이 두꺼운 경우는 면재-심재 분리가 지배적으로 관찰되었다.

• Structural Engineering and Mechanics
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• 제10권1호
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• pp.27-36
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• 2000

The Oktalok nodal connection system is an aesthetic and efficient system. It has been widely used throughout Australia. The paper will briefly introduce the concept and application of the Oktalok nodal system. The existing design method is based on the assumption that the joints are pin-ended, i.e., the rotational stiffness of the joints is zero. However the ultimate capacity of the frame may increase significantly depending on the rotational stiffness of the joints. Stiffness tests and finite element simulations were carried out to determine the rotational stiffness of the Oktalok joints. Column buckling tests and non-linear finite element analyses were performed to determine the member capacity of columns with semi-rigid end conditions. A simple formulae for the effective length factor of column buckling is derived based on the above experimental and theoretical investigations.

• Steel and Composite Structures
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• 제3권5호
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• pp.307-320
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• 2003

This paper presents an efficient approach to the determination of the buckling loads of down-aisle, spliced, unbraced, pallet rack structures subjected to vertical and horizontal loads. A pallet rack structures is analysed by considering the stability equations of an equivalent free-sway column. The effects of semi-rigid beam-to-upright, splice-to-upright and base-plate-to-upright connections are fully incorporated into the analysis. Each section of upright between successive beam levels in the pallet rack is considered to be a single column element with two rotational degrees of freedom. A computer algebra package was used to determine modified stability equations for column elements containing splices. The influence of the position of splices in a pallet rack is clearly demonstrated.

• 한국농공학회지
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• 제41권5호
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• pp.112-122
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• 1999

이 논문은 일정체적을 갖는 양단고정 변단면 기둥의 좌굴하중 및 후좌굴 거동에 관한 연구이다. 기둥의 변단면으로는 직선형, 포물선형, 정현의 선형을 갖는세 가지 변단면을 채택하였다. Bernoulli-Euler 보 이론을 이용하여 압축하중이 작용하여 좌굴된 기둥이 정확탄성곡선을 지배하는 미분방정식을 유도하였다. 유도된 미분방정식을 Runge-Kutta 법과 REgula-Falsi법을 이용하여 수치해석하였다. 수치해석의 결과로 좌굴하중, 좌굴기둥의 평형경로 및 정확탄성곡선을 산출하였다. 또한 좌굴하중-단면비 곡선으로부터 최강기둥의 좌굴하중과 단면비를 산출하였다.

• International Journal of Aeronautical and Space Sciences
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• 제15권1호
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• pp.20-31
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• 2014

This paper deals with the development of a realistic shape optimization of damaged columns that are subjected to conservative and non-conservative forces, using the Genetic Algorithm (GA). The analysis is based on the design of the most optimized shape of the column under the constraint of constant weight, considering the Static, Vibrational, and Flutter characteristics. Under the action of conservative and non-conservative longitudinal forces, an elastic column loses its stability. A numerical analysis based on FEM has been performed on a uniform damaged column, to compute the fundamental buckling load, vibration frequency, and flutter load, under various end restraints. An optimization search based on the Genetic Algorithm is then executed, to find the optimal shape design of the column. The optimized column references the one having the highest buckling load, highest vibration frequency, and highest flutter load, among all the possible shapes of the column, for a given volume. A comparison is then made between the values obtained for the optimized damaged column, and those obtained for the optimized undamaged column. The comparison reveals that the incorporation of damage in the column alters its optimal shape to only a certain extent. Also, the critical load and frequency values for the optimized damaged column are comparatively low, compared with those obtained for the optimized undamaged column. However, these results hold true only for moderate-intensity damage cases. For high intensity damage, the optimal shape may not remain the same, and may vary, according to the severity of damage.

• 한국강구조학회 논문집
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• 제27권4호
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• pp.377-386
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• 2015

본 연구에서는 공칭인장강도 800MPa급 고강도강재(HSA800)로 제작된 중간주의 중심압축실험을 통해 좌굴강도를 평가하여 현행 구조설계기준(KBC2009, 2010 AISC-LRFD) 기둥곡선의 비탄성영역 적용성 여부를 검토하였다. 강도로 무차원화한 판폭두께비와 판단부 지지조건 및 기둥 세장비를 변수로 하였으며, 고강도강재와 일반강재의 좌굴거동 차이 여부를 확인하기 위해 일반강재(SM490)로 제작된 비교실험체를 포함시켰다. 실험결과 중심압축을 받는 모든 HSA800 중간주 실험체는 현행 강구조기준의 설계좌굴강도를 충분히 발휘하였으나 일부 SM490 실험체는 설계강도를 하회하였다. 이는 고강도강재의 잔류응력에 의한 강도저하가 일반강재에 비해 작기 때문으로 판단된다.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1996년도 가을 학술발표회 논문집
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• pp.3-10
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• 1996

Numerical methods are developed for solving the buckling loads and the elastica of clamped- free columns of circular cross-section with constant volume. The column model is based rut the Timoshenko beam theory. The Runge-Kutta and Regula-Falsi methods, respectively, are used to solve the governing differential equations and to compute the eigenvalues. Extensive numerical results, including buckling loads, elastica of buckled shapes and effects of shear de-formation, are presented in non-dimensional form for elastic columns whose radius of circular cross-section varies both linearly and parabolically with column length.

• 한국소음진동공학회논문집
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• 제16권10호
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• pp.1074-1081
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• 2006

This paper deals with the dynamic stability analysis of clamped-hinged columns with constant volume. Numerical methods are developed for solving natural frequencies and buckling loads of such columns, subjected to an axial compressive load. The parabolic taper with the regular polygon cross-section is considered, whose material volume and column length are always held constant. Differential equations governing both free vibrations and buckled shapes of such columns are derived. The Runge-Kutta method is used to integrate the differential equations, and the Regula-Falsi method is used to determine natural frequencies and buckling loads, respectively. The numerical methods developed herein for computing natural frequencies and buckling loads are found to be efficient and robust. From the numerical results, dynamic stability regions, dynamic optimal shapes and configurations of strongest columns are reported in figures and tables.

• Earthquakes and Structures
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• 제9권6호
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• pp.1181-1192
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• 2015

In this paper, an analytical method is proposed to study the effect of crack and axial load on vibration behavior and stability of the cracked columns. Using the local flexibility model, the crack has been simulated by a torsional spring with connecting two segments of column in crack location. By solving governing eigenvalue equation, the effects of crack parameters and axial load on the natural frequencies and buckling load as well as buckling load are investigated. The results show that the presents of crack cause to reduction in natural frequencies and buckling load whereas this reduction is affected by the location and depth of the crack. Furthermore, the tensile and compressive axial load increase and decrease the natural frequencies, respectively. In addition, as the compression load approaches to certain value, the fundamental natural frequency reaches zero and instability occurs. The accuracy of the model is validated through the experimental data reported in the literature.