• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1995년도 봄 학술발표회 논문집
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• pp.62-69
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• 1995

The differential equations governing both the free vibrations and buckling loads of the beam-columns with constant volumes are derived and solved numerically. The axial load effects are included in the differential equations. The Runge-Kutta method and Regula-Falsi method are used to compute the eigenvalues corresponding to the natural frequencies. and buckling loads. In numerical examples, the simple end constraint is considered.

• 한국강구조학회 논문집
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• 제26권6호
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• pp.523-535
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• 2014

현 내진기준의 근간인 역량설계법(capacity design)에 의할 때, 중심가새골조의 내진설계는 기둥 및 보부재는 탄성부재로, 가새부재는 반복적인 인장과 압축을 통해 지진에너지를 소산하는 비탄성 부재로 설계되어야 한다. 가새부재는 에너지를 소산하는 과정에서 기둥부재에 추가적인 축력을 유입시키므로, 이 추가 축력을 고려하여 기둥부재를 탄성설계해야 한다. 현행 기준은 중심가새골조의 기둥부재 설계시 전층의 가새가 동시에 인장항복 및 좌굴하는 가장 보수적인 상황을 가정하여 기둥의 축력을 산정하거나 특별지진하중에 대해 기둥을 설계하는 방법을 제안하고 있다. 그러나 전층의 가새가 동시에 좌굴할 가능성은 희박하며, 특별지진하중에는 시스템 초과강도라는 경험적이고 우회적인 요소가 도입되었다는 한계가 있다. 이와 같은 문제점을 극복하기 위한 몇몇 선행 관련 연구들 역시 가새의 좌굴을 명시적으로 고려하지 못하였을 뿐더러 역학적 근거도 희박하다. 최근에 행해진 연구 중에서 역 V형 중심 가새골조를 대상으로, 기존의 기둥축력 산정법이 가지는 한계를 극복할 수 있는 새로운 기둥축력 산정법이 제안된 바가 있다. 하지만 역 V형 중심 가새골조와 X형 중심 가새골조의 하중전달 메커니즘은 상이하기 때문에 이 축력산정법을 X형 가새골조에 그대로 적용할 수는 없다. 따라서 본 연구에서는 X형 중심가새골조만의 역학적 특성을 고려한 네 가지의 기둥축력 산정법을 제안하였다. 특히 모달질량을 가중치로 고려하여 고차모드의 영향을 반영할 수 있는 새로운 방안을 제시하였다. 방대한 지진데이터를 입력으로 한 비선형 동적해석을 수행하여 제시된 방안의 타당성을 평가하였다.

• 대한토목학회논문집
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• 제30권2A호
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• pp.81-92
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• 2010

강프레임 부재의 설계에서 탄성 시스템좌굴해석은 프레임의 실제 거동을 예측하기 어려운 반면, 비탄성 시스템좌굴해석은 압축부재의 세장비에 따른 비탄성 거동이 고려됨으로써 보다 현실적인 부재의 좌굴거동을 예측할 수 있다. 그러나 시스템좌굴해석 수행후 오일러좌굴식을 이용한 방법은 압축력이 비교적 작게 발생하는 부재에서 과도한 유효좌굴길이를 산정한다는 문제점을 내포하고 있다. 본 연구에서는 강프레임 구조의 모든 부재의 탄성 및 비탄성 유효좌굴길이계수를 산정할 수 있는 새로운 해석방법을 제안하였다. 제안된 방법은 가상축력계수 개념을 기반으로 비탄성 강도감소계수를 도입하고 반복고유치해석을 수행하여 각 부재의 유효좌굴길이계수를 산정한다. 제안된 방법의 타당성을 검증하기 위하여 예제 강프레임 구조물을 제안된 방법에 의거한 유효좌굴길이와 기존 방법에 의거한 결과를 비교하였다. 검증 결과, 제안된 방법은 강프레임의 모든 부재의 탄성 및 비탄성 유효좌굴길이계수를 합리적으로 산정할 수 있었다. 부가적으로 재료의 비탄성 거동이 부재의 유효좌굴길이에 미치는 영향도 논의되었다.

• Interaction and multiscale mechanics
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• 제4권4호
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• pp.313-320
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• 2011

This paper proposes an approximate formulation to estimate the bifurcation buckling loads of cylindrical shells with soft elastic cores under the conditions of axial compression. In general, thin-walled, axially compressed cylindrical shells buckle into a diamond pattern in the elastic range. However, buckling symmetrical with respect to the axis of the cylinder may occur when the cylindrical shell is supported by an elastic medium. By considering this characteristic, we introduce the simplified approximate formulation that can give sufficiently accurate results for the bifurcation buckling loads of cylindrical shells. Moreover the results are compared with the exact buckling loads in order to confirm the accuracy of the proposed approximate formulation.

• 대한조선학회지
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• 제24권1호
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• pp.42-50
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• 1987

The energy expressions are formulated for the axially stiffened shell treating the stiffeners as discrete elements. The principle of minimum potential energy is employed to formulate the buckling equations for a simply supported, axially stiffened shell under uniform axial compression. The displacement functions are expended into double trigonometric series. The mode assuming method employed in this paper makes it possible to reduce the matrix size of the eigenvalue problem considerably. Effects are made to investigate the transition from overall buckling to local buckling and to verify the existence of the minimum stiffness ratio of stiffener as in the case of stiffened plate. The results of the calculation show that the critical stiffener size increase linearly as the length of the shell increases. The results also show that the overall buckling load decreases and the local buckling load has a nearly constant value as the length of the shell increases. The results show very good agreements with other computational available.

• Structural Engineering and Mechanics
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• 제13권5호
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• pp.543-556
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• 2002

A dynamic elastic local buckling analysis is presented for a pile subjected to an axial impact load. The pile is assumed to be geometrically perfect. The interactions between the pile and the surrounding soil are taken into account. The interactions include the normal pressure and skin friction on the surface of the pile due to the resistance of the soil. The analysis also includes the influence of the propagation of stress waves through the length of the pile to the distance at which buckling is initiated and the mass of the pile. A perturbation technique is used to determine the critical buckling length and the associated critical time. As a special case, the explicit expression for the buckling length of a pile is obtained without considering soil resistance and compared with the one obtained for a column by means of an alternative method. Numerical results obtained show good agreement with the experimental results. The effects of the normal pressure and the skin friction due to the surrounding soil, self-weight, stiffness and geometric dimension of the cross section on the critical buckling length are discussed. The sudden change of buckling modes is further considered to show the 'snap-through' phenomenon occurring as a result of stress wave propagation.

• 해양환경안전학회지
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• 제23권3호
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• pp.313-319
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• 2017

Cylindrical shells are often used in ship structures at deck plating with a camber, side shell plating at fore and aft parts, and bilge structure part. It has been believed that such curved shells can be modelled fundamentally by a part of a cylinder under axial compression. From the estimations with the usage of cylinder models, it is known that, in general, curvature increases the buckling strength of a curved shell subjected to axial compression, and that curvature is also expected to increase the ultimate strength. We conduct series of elasto-plastic large deflection analyses in order to clarify the fundamentals in buckling and plastic collapse behaviour of cylindrical shells under axial compression. From the numerical results, we derive design formula for predicting the ultimate strength of cylindrical shell, based on a series of the nonlinear finite element calculations for all edges, simply supporting plating, varying the slenderness ratio, curvature and aspect ratio, as well as the following design formulae for predicting the ultimate strength of cylindrical shell. From a number of analysis results, fitting curve can be developed to use parameter of slenderness ratio with implementation of the method of least squares. The accuracy of design formulae for evaluating ultimate strength has been confirmed by comparing the calculated results with the FE-analysis results and it has a good agreement to predict their ultimate strength.

• Steel and Composite Structures
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• 제30권2호
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• pp.81-96
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• 2019

The behavior of a new Three-Tube Buckling-Restrained Brace (TTBRB) with circumference pre-stress (${\sigma}_{{\theta},pre}$) in core tube are investigated through a verified finite element model. The TTBRB is composed of one core tube and two restraining tubes. The core tube is in the middle to provide the axial stiffness, to carry the axial load and to dissipate the earthquake energy. The two restraining tubes are at inside and outside of the core tube, respectively, to restrain the global and local buckling of the core tube. Based on the yield criteria of fringe fiber, a design method for restraining tubes is proposed. The applicability of the proposed design equations are verified by TTBRBs with different radius-thickness ratios, with different gap widths between core tube and restraining tubs, and with different levels of ${\sigma}_{{\theta},pre}$. The outer and inner tubes will restrain the deformation of the core tube in radius direction, which causes circumference stress (${\sigma}_{\theta}$) in the core tube. Together with the ${\sigma}_{{\theta},pre}$ in the core tube that is applied through interference fit of the three tubes, the yield strength of the core tube in the axial direction is improved from 160 MPa to 235 MPa. Effects of gap width between the core tube and restraining tubes, and ${\sigma}_{{\theta},pre}$ on hysteretic behavior of TTBRBs are presented. Analysis results showed that the gap width and the ${\sigma}_{{\theta},pre}$ can significantly affect the hysteretic behavior of a TTBRB.

• Steel and Composite Structures
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• 제33권4호
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• pp.595-614
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• 2019

In cold-formed steel (CFS) structures, such as trusses, transmission towers and portal frames, the use of back-to-back built-up CFS unequal angle sections are becoming increasingly popular. In such an arrangement, intermediate welds or screw fasteners are required at discrete points along the length, preventing the angle sections from buckling independently. Limited research is available in the literature on axial strength of back-to-back built-up CFS unequal angle sections. The issue is addressed herein. This paper presents an experimental investigation on both the welded and screw fastened back-to-back built-up CFS unequal angle sections under axial compression. The load-axial shortening and the load verses lateral displacement behaviour along with the deformed shapes at failure are reported. A nonlinear finite element (FE) model was then developed, which includes material non-linearity, geometric imperfections and modelling of intermediate fasteners. The FE model was validated against the experimental test results, which showed good agreement, both in terms of failure loads and deformed shapes at failure. The validated FE model was then used for the purpose of a parametric study to investigate the effect of different thicknesses, lengths and, yield stresses of steel on axial strength of back-to-back built-up CFS unequal angle sections. Five different thicknesses and seven different lengths (stub to slender columns) with two different yield stresses were investigated in the parametric study. Axial strengths obtained from the experimental tests and FE analyses were used to assess the performance of the current design guidelines as per the Direct Strength Method (DSM); obtained comparisons show that the current DSM is conservative by only 7% on average, while predicting the axial strengths of back-to-back built-up CFS unequal angle sections.

• Structural Engineering and Mechanics
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• 제70권4호
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• pp.499-511
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• 2019

In this study, the axial compressive behavior of novel quadruple C-channel built-up cold-formed steel columns with different slenderness ratio was investigated, using the experimental and numerical analysis. The axial compressive capacity and failure modes of the columns were obtained and analyzed. The finite element models considering the geometry, material and contact nonlinearity were developed to simulate and analyze the structural behavior of the columns further. There was a great correlation between the numerical analyses and test results, which indicated that the finite element model was reasonable and accurate. Then influence of, slenderness ratio, flange width-to-thickness ratio and screw spacing on the mechanical behavior of the columns were studied, respectively. The tests and numerical results show that due to small slenderness ratio, the failure modes of the specimens are generally local buckling and distortional buckling. The axial compressive strength and stiffness of the quadruple C-channel built-up cold-formed steel columns decrease with the increase of maximum slenderness ratio. When the screw spacing is ranging from 150mm to 450mm, the axial compressive strength and stiffness of the quadruple C-channel built-up cold-formed steel columns change little. The axial compressive capacity of quadruple C-channel built-up cold-formed steel columns increases with the decrease of flange width-thickness ratio. A modified effective length factor is proposed to quantify the axial compressive capacity of the quadruple C-channel built-up cold-formed steel columns with U-shaped track in the ends.