• 한국강구조학회 논문집
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• 제22권6호
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• pp.609-616
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• 2010

이 논문은 600MPa급 고강도강이 원형강관 건축구조용으로 이용될 때 중심압축재의 좌굴강도에 관하여 수치해석적으로 조사한 것이다. 600MPa급 고강도강의 소재인장시험 결과로부터 중심압축재의 좌굴강도를 산정하였으며, 좌굴강도 산정에는 Beam-Column이론에 근거한 방법과 Tangent Modulus 이론에 의한 양자의 방법을 이용하였다. 그리고 소성흐름이 없는 인장시험의 응력-변형도 관계를 비례한도의 크기와 비례한도에서 항복점에 이르는 접선계수의 기울기로 근사시키고 좌굴강도 미치는 영향인자를 조사하였다. 600MPa급 고강도강에 적용되는 현재의 건축기준은 압축재의 경우 항복강도 Fy값을 480Mpa 까지 상향조정하여도 무리가 없다고 사료된다.

• Structural Engineering and Mechanics
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• 제40권4호
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• pp.563-581
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• 2011

Many novel materials, developed in recent years, have obvious properties with different modulus of elasticity in tension and compression. The ratio of their tensile modulus to compressive modulus is as high as five times. Nowadays, it has become a new trend to study the mechanical properties of these bimodular materials. At the present stage, there are extensive studies related to the strength analysis of bimodular structures, but the investigation of the buckling stability problem of bimodular rods seems to cover new ground. In this article, a semi-analytical method is proposed to acquire the buckling critical load of bimodular slender rod. By introducing non-dimensional parameters, the position of neutral axis of the bimodular rod in the critical state can be determined. Then by combining the phased integration method, the deflection differential equation of bimodular pin-ended slender rod is deduced. In addition, the buckling critical load is obtained by solving this equation. An example, which is conducted by comparing the calculation results between the three of the methods including the laboratory tests, numerical simulation method and the method we developed here, shows that the method proposed in the present work is reliable to use. Furthermore, the influence of bimodular characteristics on the stability is discussed and analyzed.

• Steel and Composite Structures
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• 제2권3호
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• pp.209-222
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• 2002

This paper describes the buckling phenomenon of a tubular truss with unsupported length through a full-scale test and presents a practical computational method for the design of the trusses allowing for the contribution of torsional stiffness against buckling, of which the effect has never been considered previously by others. The current practice for the design of a planar truss has largely been based on the linear elastic approach which cannot allow for the contribution of torsional stiffness and tension members in a structural system against buckling. The over-simplified analytical technique is unable to provide a realistic and an economical design to a structure. In this paper the stability theory is applied to the second-order analysis and design of the structural form, with detailed allowance for the instability and second-order effects in compliance with design code requirements. Finally, the paper demonstrates the application of the proposed method to the stability design of a commonly adopted truss system used in support of glass panels in which lateral bracing members are highly undesirable for economical and aesthetic reasons.

• Advances in nano research
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• 제4권3호
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• pp.229-249
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• 2016

In this paper, buckling characteristics of nonhomogeneous functionally graded (FG) nanobeams embedded on elastic foundations are investigated based on third order shear deformation (Reddy) without using shear correction factors. Third-order shear deformation beam theory accounts for shear deformation effects by a parabolic variation of all displacements through the thickness, and verifies the stress-free boundary conditions on the top and bottom surfaces of the FG nanobeam. A two parameters elastic foundation including the linear Winkler springs along with the Pasternak shear layer is in contact with beam in deformation, which acts in tension as well as in compression. The material properties of FG nanobeam are supposed to vary gradually along the thickness and are estimated through the power-law and Mori-Tanaka models. The small scale effect is taken into consideration based on nonlocal elasticity theory of Eringen. Nonlocal equations of motion are derived through Hamilton's principle and they are solved applying analytical solution. Comparison between results of the present work and those available in literature shows the accuracy of this method. The obtained results are presented for the buckling analysis of the FG nanobeams such as the effects of foundation parameters, gradient index, nonlocal parameter and slenderness ratio in detail.

• 한국강구조학회 논문집
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• 제18권1호
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• pp.71-80
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• 2006

강판 전단패널의 거동이 일반연강 (S400) 을 이용한 실험 및 해석으로 고찰되었다. 강판 전단패널은 작은 하중에서 좌굴을 하지만, 패널의 전단극한강도는 인장력 작용에 의한 강판 전단패널의 좌굴후 강도에 의해 좌우된다. 그러나, 설계상에서 강판 전단패널의 성능은 강판 전단패널의 탄성좌굴강도에 국한된다. 캐나다 극한강도 설계 규준 (CAN/CSA-S16.1-94)은 스트립 모델을 이용한 박강판 전단패널의 해석을 위한 절차를 규정하고 있다. 본 논문에서는 실험결과와 스트립모델 해석 결과를 이용하여 강판 전단패널의 구조성능을 평가하였다.

• Composites Research
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• 제12권6호
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• pp.31-42
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• 1999

항공우주산업에서 무게를 증가시키지 않고 비행구조물의 구조적 성능을 증가시키는 것은 굉장한 잇점을 갖는다. 본 연구에서는 복합재료 평판의 무게를 증가시키지 않고 좌굴하중과 인장 파단하중을 동시에 증가시키는 혁신적인 설계 방법에 대해서 연구하였다. 원공이 있는 복합재료 적층판에서 곡선 섬유층과 직선 섬유층을 조합하여 적층판을 구성할 때 좌굴하중과 인장파단 하중이 동시에 증가되는 현상에 대하여 유한요소 해석을 사용하여 알아보았다. 원공의 크기와 적층 순서를 달리하면서 곡선섬유를 이용한 효과가 얼마나 되는지 알아보았다. 또한, 각각의 경우에 대해서 파단이 어떻게 일어나는가도 관찰하였다. 곡선섬유 평판을 제작하기 위해서는 연속적이고 부드럽게 변하는 fiber path가 필요하다. 여기서는 유한요소로 구한 섬유 방향을 사용하여 제작이 가능한 부드럽게 이어지는 fiber path를 구하는 간단한 방안을 제시하였다.

• 대한기계학회논문집A
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• 제21권12호
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• pp.2090-2095
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• 1997

The plane stress fracture toughness for thin aluminum alloy(2024-T3 and 7075-T6) specimens are characterized by using compact-tension (CT) specimens. Anti-buckling plates were fabricated on both sides of the thin CT specimens to prevent the buckling phenomena which caused by the 45.deg. C plastic yielding at the crack tip under the plane stress condition. The plane stress fracture toughnesses determined by three different procedures are compared with each others. The plane stress fracture toughnesses are also compared with a few published values which were determined by using center-cracked panel specimens.

• 대한조선학회논문집
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• 제44권5호
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• pp.504-508
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• 2007

In the case of thin plate blocks, buckling deformation due to longitudinal shrinkage is the most important weld-induced deformation. This paper is concerned with developing the formula to predict the longitudinal shrinkage due to welding, in which mechanical tension effect in welding direction is accounted for. For this purpose, bead on plate welding test has been carried out for the 27 thin plate specimens with varying welding conditions and magnitude of tensile load. Empirical formula of predicting the longitudinal shrinkage has been derived based on the results of welding test, in which effect of mechanical tension is included. The derived formula can be usefully used in predicting the level of tensile load to reduce the longitudinal shrinkage.

• Steel and Composite Structures
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• 제36권2호
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• pp.163-177
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• 2020

Concentrically Braced Frames (CBFs) are commonly used in the construction of steel structures because of their ease of implementation, rigidity, low lateral displacement, and cost-effectiveness. However, the principal disadvantage of this kind of braced frame is the inability to provide deformation capacity (ductility) and buckling of bracing elements before yielding. This paper aims to present a novel Composite Buckling Restrained Fuse (CBRF) to be utilized as a bracing segment in concentrically braced frames that allows higher ductility and removes premature buckling. The proposed CBRF with relatively small dimensions is an enhancement on the Reduced Length Buckling Restrained Braces (RL-BRBs), consists of steel core and additional tensile elements embedded in a concrete encasement. Employing tensile elements in this composite fuse with a new configuration enhances the energy dissipation efficiency and removes the tensile strength limitations that exist in bracing elements that contain RL-BRBs. Here, the optimal length of the CBRF is computed by considering the anticipated strain demand and the low-cyclic fatigue life of the core under standard loading protocol. An experimental program is conducted to explore the seismic behavior of the suggested CBRF compare with an RL-BRB specimen under gradually increased cyclic loading. Moreover, Hysteretic responses of the specimens are evaluated to calculate the design parameters such as energy dissipation potential, strength adjustment factors, and equivalent viscous damping. The findings show that the suggested fuse possess a ductile behavior with high energy absorption and sufficient resistance and a reasonably stable hysteresis response under compression and tension.

• 대한조선학회논문집
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• 제34권3호
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• pp.53-60
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• 1997

일반적으로 선박 판부재의 좌굴강도에 대한 안전성 평가는 선체구조 설계단계에서 반드시 거쳐야 할 단계로 한 척의 배는 수많은 판부재로 구성되어 선박구조 전체에 대한 이론적이며 체계적인 시스템을 이용한 좌골강도평가의 정확도 및 효율성이 강조되고 있다. 그러나 현재의 판부재 좌굴강도를 평가하는 각 선급의 규정치가 많은 영향인자를 고려치 않고 있거나 함축척으로 고려하고 있기 때문에 경우에 따라서는 좌굴강도가 상당한 안전측의 값을 제시하는 등 실제 선급규정치의 사용에 제약을 주기도 한다. 따라서 본 연구에서는 면내인장력의 영향등 선급들의 좌굴 규정치뿐만이 아니라 면내인장력의 효과, 경계조건, 횡하중 및 잔류응력등을 고려하면서 손쉽게 좌굴평가를 수행할 수 있는 선진 좌굴평가시스템을 개발하였다. 이들 선진 좌굴평가시스템을 이용하면 선박판부재의 보다 정도 높고 효율적인 평가가 가능하리라 생각되며 앞으로 대중적인 사용을 위해 워크스테이션 외에도 개인용 컴퓨터에서의 시스템 구축을 계획하고 있다.