앏은 패널 형태의 구조물은 그 형상의 특성상 좌굴이 발생하기 쉽다. 등방성 재료에 대한 좌굴의 해석은 그동안 많은 연구가 이루어졌다. 그러나 복합재의 경우는 좌굴 현상의 거동이 매우 복잡하고 난해하기 때문에 많은 연구가 이루어지지 않았다. 적층복합재의 좌굴거동을 수치적으로 해석하기 위하여 3D 쉘요소를 적용하여 해석을 수행하였다. 본 연구에서는 3가지 종류의 layup에 대하여 비선형 좌굴 현상을 계산하였고 좌굴거동의 하중-변위 특성 관계를 규명하였다. 적층복합재의 경우 좌굴 거동이 극심한 비선형 현상을 나타내며, 또한 수치적으로 수렴하기 어렵다. 3가지 layup 적층복합재의 좌굴 거동을 해석하기 위하여 arc-length 방법을 사용하였다. 비선형 좌굴 거동의 힘-변위 곡선을 계산 하였고 또한 Tsai-Wu 파괴이론에 의하여 좌굴거동이 발생하면서 복합재의 파괴를 계산하였다.

세계적으로 대공간 건축물의 수요가 점점 증가하고 있는 추세에 따라 단층 래티스 돔 구조 시스템은 단순한 외관과 간단한 그리드 패턴으로 인해 300m 공간 구조로 널리 채택 될 것입니다. 선행 연구에서 300m 길이의 단층 래티스 돔에 자중 및 적설 하중을 가했을 때 강재를 이용한 골조 시스템을 이용하여 단층 래티스 돔의 구조 안정성을 대략적으로 파악 하였다. 강성 연결로 되어있는 300m 단층 래티스 스팬의 스팬에 대한 안정성 연구는 이미 많이 수행되었지만 연결부의 강성에 따른 좌굴특성에 대한 연구는 많지 않습니다. 따라서 연구자들이 실제 설계에 적용 할 연구 데이터가 많지 않기 때문에이 구조의 다양한 연결 조건을 연구 할 필요가 있다. 본 연구의 목적은 연결 조건에 따라 300M 단층 래티스 스팬의 좌굴 특성을 분석하여 대공간 단층 래티스 돔의 설계자들에게 도움을 주고자 한다.

Beam bracing is applied to prevent the relative displacement of the top and bottom flanges or to effectively control the twisting of the section, and the lateral stability of the beams are provided by lateral bracing, torsional bracing or a combination of both. Modular steel I-girders are laterally interconnected by torsional bracings that are installed to increase the resistance to lateral torsional buckling. In this paper, numerical parametric study was carried out by varying the crossbeam web height to examine the effects of the web torsional stiffness. Three-dimensional finite-element analysis using the commercial finite element software ABAQUS was obtained for the parametric numerical analyses of a series of feasible two-girder models, and the failure mode, lateral-torsional buckling strength and the moment-displacement behavior of the main girders was determined.

A pultruded fiber reinforced polymer plastic (PFRP) structural is one of the most widely used composite member in construction. In generally, PFRP members is composed of plate elements so that it needs to evaluate stability problems when they are used by construction members. On the other hand, creep effect may be occurred in PFRP members under sustained load. Primary to experiment for PFRP creep, previous works are studied. In the previous work related to buckling of PFRP member, it can be calculated buckling strength of PFRP members when it is known that material property of longitudinal and transverse direction of PFRP members. The researches for creep behavior of PFRP has been conducted and time-dependent degradation elastic moduls can be predicted by the empirical equation. In this study, it will be conducted creep test for PFRP and time-dependent stress-strain relationship will be plotted. It is expected that long-term buckling behavior of PFRP is evaluated by theoretical and numerical method such as finite element method.

Using closed-section ribs as longitudinal stiffeners have been proven to be an effective system for axially compressed members, however, studies on the application of these on laminated composite shell are insufficient. Thus, this study aims to evaluate the buckling behavior of the laminated composite shell when closed-section ribs were applied as longitudinal stiffeners. The effect of the rotational stiffness of the closed-section ribs on the buckling modes and strengths will be determined in this paper. The three-dimensional finite element modeling were set up using ABAQUS and a series of eigenvalue analysis were conducted, applying eight layers of the layup [(0°)4]s, [(45°/-45°)2]s and [(0°/90°)2]s on the orthotropic plates. Through the parametric studies, the increasing effect on the elastic buckling strengths due to the rotational stiffness are numerically verified, and the buckling strength of a longitudinally stiffened shell with a laminated composite material were compared with that of the isotropic material.

곡률을 갖고 있는 쉘 부재들은 선박 및 육상구조 내에서 캠버와 선수, 선미, 파이프 및 저장용 탱크에 주로 사용되고 있다. 이러한 곡률 쉘 부재들은 기본적으로 원통형 실린더 부재의 일부라고 간주할 수 있다. 일반적으로 곡률의 존재는 압축하중 작용 시 좌굴강 도 및 최종강도를 증가시키는 것으로 알려져 있다. 본 논문에서는 이러한 영향을 확인하기 위하여 탄성대변형 시리즈해석을 수행하였으며, 매개변수의 영향을 분석하였다. 실린더의 최종강도 거동은 초기처짐과 해석모델링 방법에 큰 영향을 받는 것을 확인하였다.

본 연구에서는 쌍동형 카페리에 다수 존재하는 유공판의 좌굴강도 설계 수행 결과 및 개선사항을 논의하고 있다. 카페리와 같이 길이가 50미터 이상이고, 길이/폭의 비가 12보다 큰 중/소형 고속선박은 상대적으로 두께가 얇고 연강을 사용함으로서 좌굴강도가 취약해질 가능성이 농후하다. 특히, 작업자의 접근 및 통로로 활용되는 유공판에서 좌굴강도가 취약해질 가능성이 있다. 안전한 구조설계를 위해서는 유공주위의 면내 하중 재 분포에 의한 좌굴강도 및 최종강도에 대한 명확한 검토가 필요하다. 본 연구에서는 유공판의 좌굴 및 최종강도 특성에 영향을 미치는 매개변수의 영향을 종합적으로 고려하기 위하여 유한요소해석 프로그램인 ANSYS를 활용한 비선형시리즈 해석을 수행하였으며, 주요 변수(종횡비, 유공비, 유공형상)들에 대한 영향을 검토하였다. 이 결과를 바탕으로 하여, 유공판의 좌굴강도를 결정짓는 가장 큰 인자는 유공비였으며, 종횡비와 유공의 형상은 그 영향이 미비하였다.

본 논문에서는 국부좌굴 현상을 고려하여 강판 콘크리트 패널(SCP)의 유한요소 해석을 수행하고 설계지침과 비교하여 전 단 스터드의 효율적인 스터드 배치 간격을 연구하였다. 강판 콘크리트 구조의 설계 및 기술기준은 전단 균열의 전개와 국부 좌굴 현상을 방지하기 위하여 스터드의 최대 간격을 제한하고 있으나 이는 기존 강재-콘크리트 합성 구조의 설계기준을 토대로 산정되었다. 이에 유한요소 해석 프로그램을 이용한 강판 및 SCP의 국부좌굴 부재 해석을 통하여 스터드 최대 배치 간격을 구하고 설계지침에서 제시한 값과 비교하였다. 먼저, 단일 강판에 대하여 국부좌굴 해석을 수행하여 판좌굴 이론과 비교 검증하였고, 연속적인 스터드 배치에 따른 영향을 확인하기 위하여 다수의 강판이 연결된 경우에 대하여 해석을 수행하였다. 또한 강판 콘크리트 구조에서 콘크리트의 영향 및 합성 거동에 따른 영향을 확인하기 위하여 강판 콘크리트 구조를 모델링하고, 국부좌굴이 발생하지 않는 스터드 배치 최대 간격을 구하여 설계지침과 비교하였다.

As the national income grows, there is a growing demand for buildings that require long span structures such as exhibition facilities, sports facilities, special industrial facilities, and aerospace facilities. Single-layer latticed dome is one of representative llong span structures. But single layer latticed domes are apt to occur the unstable phenomena that are called “buckling” because of the lack of strength of members and instability of structures, etc. In the previous study, the structural stability of a single-layer lattice dome was roughly grasped by a frame structural system using a ready-made steel when a self-weight and a snow load were applied to a single-layer latticed dome having a span of 300 m and a height of 75 m. However, a systematic study of a 300m single layer lattice dome with various rise-span ratios was not performed. Therefore, it is necessary to study various conditions of this structure because the researchers do not have much research data to apply to actual design. Therefore, the purpose of this study is to verify the buckling characteristics of span 300M single-layer latticed dome with rise-span ratio

본 연구에서는 1차 전단변형이론을 고려한 비국소 자기-전기-탄성 나노 판의 2방향 좌굴해석에 관하여 연구하였다. 면내 전기-자기-탄성 나노 판에서 전기장과 자기장은 무시할 수 있다. 자기-전기 경계조건과 맥스웰 방정식에 따라 전기-자기-탄성 나노 판의 두께 방향에 따른 자위 및 전위의 변화가 결정된다. 자기-전기-탄성 나노 판의 탄성이론을 재 공식화하기 위하여 에링겐의 비국소 미분 구성 관계식을 사용하였다. 변분이론을 이용하여 비국소 탄성이론의 지배방정식을 연구하였 다. 비국소 이론과 국소 이론의 관계를 계산 결과를 통하여 분석하였다. 또한, 비국소 매개변수, 면내 하중 방향 그리고 형상 비에 따른 구조적 응답을 연구하였다. 계산 결과들은 전위 및 자위의 효과를 나타내었다. 이러한 계산 결과들은 자기-전기-탄성 재료로 구성된 신소재 구조물의 설계 및 해석에 사용될 수 있고 향후 연구의 비교자료가 될 수 있을 것으로 판단된다.

The pultruded fiber reinforced polymer plastic (PFRP) is one of the most actively studied composite materials for the structural member in construction industries. In domestic design process, the PFRP member is designed as an isotropic material having only longitudinal material properties for simplicity, because it is too complex to consider orthotrophy of PFRP perfectly. In this study, three cases of buckling analysis of PFRP plate is conducted theoretically and numerically. First, the PFRP plate is considered as an orthotropic material. Second, the PFRP plate is considered as an isotropic plate having only longitudinal material properties. Third, the PFRP plate is considered as an isotropic plate having geometric mean of longitudinal and transverse material properties. As a result of buckling analysis, a buckling strength of PFRP plate as an isotropic plate having only longitudinal material properties is about 2.21 times larger than that of PFRP plate analyzed as an orthotropic plate. On the other hand, a buckling strength of PFRP plate as an isotropic plate having geometric mean material properties is about 1.19 times larger than that of PFRP plate analyzed as an orthotropic plate. In conclusion, the safety factor of 3 used in domestic design process of PFRP member is no longer applicable due to overestimation of buckling strength of PFRP member which leads to nonconservative design.

Recent studies have revealed that plates stiffened by closed-section ribs can be designed to have greater strength. Thus, this study is about the increasing effect on local plate buckling strength of isotropic plates when longitudinally stiffened with closed-section ribs, which is mainly due to the rotational restraint of the closed-section ribs. The effects on buckling strengths of the stiffened plates are examined by numerical analyses. Three-dimensional finite element models were obtained using a general structural analysis program ABAQUS and a series of eigenvalue analyses were conducted. Through this study, the increasing effect on the local buckling strength due to the rotational stiffness is numerically verified. From the parametric studies, there is an obvious tendency that the local buckling strength of the stiffened plate would converge to the buckling strength of plate with fixed boundary condition. The findings of this study would contribute in improving the optimum design of longitudinally stiffened isotropic plates.

Since 1990’s, many researches about ultra high performance concrete have been conducted. Compare to conventional concrete, it shows significantly high compressive and tensile strength so that leads to reduce the self weight of structures. However, the use of slender member may meet the buckling failure that is not common phenomenon in concrete structures so far. Most design codes have not suggested any provisions for buckling limit states and very few of researches have been conducted for buckling of concrete girders. In this study, a number of finite element analysis were carried out to investigate the buckling behavior of UHPC I-shaped girders.

This study investigates characteristics on inelastic flange local buckling of ultra high performance concrete (UHPC) plate supported by one edge. The UHPC plate were modeled using 3D shell elements (S4R) and analyzed using by geometric and material nonlinear analysis. The plates for FE analysis were supported by pined and fixed boundary conditions to considering constrained effects of one web. The inelastic local buckling strength from the FE analysis were evaluated according to the flange slenderness ratios. The results shows that material non-linearities of tensile behavior of UHPC highly affects the inelastic local buckling of UHPC plate.

This study investigates elastic flange local buckling of ultra high performance concrete (UHPC) I-girders. The girders were modeled using 3D shell elements (S4R) and analyzed by eigenvalue analysis. Then, the flange local buckling strength from the FE analysis were evaluated according to the flange and web slenderness ratios and compared to the local buckling strength of steel girders. The results shows that the flange local buckling of UHPC I-girders are underestimated compared to the strength of steel girders which has same geometric cross sections and further studies needed related to this field.

All structures can not be perfect due to geometric or material initial imperfections. Initial imperfections are an important factor in determining the buckling mode and are known to be important factors in evaluating the actual buckling strength. The DNV-RP-C202 design standard limits the longitudinal stiffener spacing. However, the criteria for the stiffener spacing presented in DNV-RP-C202 is a guideline derived from the curved panel theory of perfect cross-sectional shape without initial imperfections. In this study, considering geometric initial imperfections, the transition point of stiffener spacing where longitudinal stiffeners affect the buckling strength of reinforced steel wind turbine tower is analyzed using finite element analysis program. The results of finite element analysis compared with theoretical results based on the perfect shape. As a result, a more reasonable stiffener spacing considering the initial imperfections was suggested.

A pultruded fiber reinforced polymer plastic (PFRP) structural member consisted of plate elements, which is commonly used as construction member, may be considered as an orthotropic material due to its unique manufacturing process. It has different mechanical properties with respect to the longitudinal and transverse directions. This orthotropic nature of PFRP material needs to be considered in the analysis of buckling behavior. In this paper, a simplified buckling analysis for PFRP plate using geometric mean of the longitudinal and transverse mechanical properties is performed. The comparison between exact buckling analysis and simplified buckling analysis is conducted. Each analysis is performed by the Levy method and the finite element method (FEM), respectively.

The single layer latticed domes have attracted many designers and researchers's attention all of the world, because these structures as spatial structure are of great advantage in not only mechanical rationality but also function, fabrication, construction and economic aspect. But single layer latticed domes are apt to occur the unstable phenomena that are called "buckling" because of the lack of strength of members, instability of structural shape, etc. In the case of latticed dome, there are several types of buckling mode such as overall buckling, local buckling, and member buckling according to the shape of dome, section type of member, the size of member, junction's condition of member and so on. There are many methods to increase the buckling strength of the single layer latticed dome, that is, with the change of geometrical shape of dome, the reinforcement of buckled member, etc. Therefore, the purpose of this study is to verify the reinforcement effect of buckled member when designers reinforce the buckled member to increase the buckling strength of single layer latticed dome with 3-way grid.

In this study, the buckling restoration at CFRP 3-Point bending specimen composed of 30°, 45°and 60° is investigated when the pressure at the lowest position on the compressed specimen is eliminated. The fracture configuration and stress contour of the specimen can be seen according to the laminate angle of fiber. The result of this study is thought to apply the data for the safe design of CFRP structure.

This study is about the basic design technology to radically increase the structural stability of structural shell or tube, which are utilized in a variety of large structures like aircrafts, plant, bridges and buildings. Recent studies have revealed that the plates stiffened by closed-sections ribs can be designed to have greater strength as well as the reduction of used number of stiffeners. Then, the analytical models were selected based on the huge steel tube design and the finite element modeling has been conducted using the ABAQUS. Through this study, the elastic buckling strengths are compared with the flat plate buckling stress and the improved effect in the local buckling strength due to the closed-section ribs are numerically verified.