• 해양환경안전학회지
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• 제10권2호
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• pp.41-47
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• 2004

선체구조 부재에는 이중저의 거더 및 늑판등에서 유공을 가진 판이 많이 사용되고 있는데, 이는 중량 경감, 사람 및 화물의 이동, 배관 등의 목적이다. 보통은 강도상 큰 문제가 없는 부위에 위치하지만, 매로는 불가피하게 높은 응력이 작용하는 부위에 설치해야 할 경우가 있다. 이러한 판에 유공의 존재는 면내 하중에 의한 탄성좌굴강도 및 최종강도에 큰 영향을 주게 된다. 따라서, 유공판의 탄성좌굴강도 및 최종강도 평가는 선박의 초기 구조설계단계에서 구조부재 치수를 결정할 매, 검토해야 할 중요한 설계기준 중의 한가지가 된다. 그러므로, 유공판에 대한 합리적이고 신뢰적인 탄성좌굴강도 및 최종강도 설계식이 필요하게 되었다. 본 연구에서는 다양한 종횡비와 유공의 치수비 그리고 세장비의 영향을 고려하여 탄소성대변형 유한요소법을 근간으로 한 해석코드인 ANSYS(7.1)를 사용하여 시리즈해석을 수행하였다.

• 대한기계학회논문집
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• 제8권6호
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• pp.604-609
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• 1984

본 연구에서는 동력이 작용하는 원환의 동력학적 진동해석으로부터 임계 좌굴 하중을 유도하 였다. 또한 진동 해석에서는 병진 관성 이외에 회전 관성과 전단 변형 효과를 개별적으로 고려 함으로서 두 개의 고유진동수에 관한 공식을 유도하였고 이로부터 좌굴하중을 산출하였다. 그 결과는 Timoshenko가 재료역학적 이론을 배경으로 산출한 좌굴하중과도 잘 일치함을 확인할 수 있었다.

• Advances in nano research
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• 제9권3호
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• pp.147-156
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• 2020

This research is related to nonlinear stability analysis of advanced microbeams reinforced by Graphene Platelets (GPLs) considering generic geometrical imperfections and thermal loading effect. Uniform, linear and nonlinear distributions of GPLs in transverse direction have been considered. Imperfection sensitivity of post-bucking behaviors of the microbeam to different kinds of geometric imperfections have been examined. Geometric imperfection is first considered to be identical as the first buckling mode, then a generic function is employed to consider sine-type, local-type and global-type imperfectness. Modified couple stress theory is adopted to incorporate size-dependent behaviors of the beam at micro scale. The post-buckling problem is solved analytically to derive load-amplitude curves. It is shown that post-buckling behavior of microbeam is dependent on the type geometric imperfection and its magnitude. Also, post-buckling load can be enhanced by adding more GPLs or selecting a suitable distribution for GPLs.

• Structural Engineering and Mechanics
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• 제73권2호
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• pp.181-190
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• 2020

In this paper, non-linear dynamic buckling behaviour of laminated composite curved panels subjected to dynamic in-plane axial compressive loads is studied using finite element methods. The work is carried out using the finite element software ABAQUS. The curved panels are modelled with S4R element and the nonlinear dynamic equilibrium equations are solved using the ABAQUS/Explicit algorithm. The effect of aspect ratio, radius of curvature and thickness are studied. The importance of orientation of plies in the direction of loading is also reiterated in this study. Vol'mir's criterion is used to calculate the dynamic buckling loads. The panels are subjected to rectangular pulse load of various amplitude and durations and the responses are observed. For particular loading amplitude, a critical value of loading duration is observed beyond which the variation of dynamic buckling load is insignificant. It is also observed that, the value of dynamic bucking load reduces as the loading duration is increased though the reduction is not much after a particular loading duration.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회A
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• pp.711-716
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• 2008

A circular tube undergoes bucking behavior when it is subjected to axial loading. An upper bound analysis can be an attractive approach to predict the buckling load and energy absorption efficiently. The upper bound analysis obtains the load or energy absorption by means of assumption of the kinematically admissible velocity fields. In order to obtain an accurate solution, kinematically admissible velocity fields should be defined by considering many factors such as geometrical parameters, dynamic effect, etc. In this study, experiments and finite element analyses are carried out for circular tubes with various dimensions and loading conditions. As a result, the kinematically admissible velocity field is newly proposed in order to consider various dimensions and the strain rate effect of material. The upper bound analysis with the suggested velocity field accurately estimates the mean load and energy absorption obtained from results of experiment and finite element analysis.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2009년도 춘계 학술발표회
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• pp.482-489
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• 2009

Various model piles with different sections such as reinforced concrete, steel, steel-concrete composite without rebar and steel-concrete composite with rebar were made, and vertical load test was conducted using a large scaled UTM(Universal Test Machine) to evaluate Young's modulus and ultimate load of the model piles. Based on the tests, ultimate load of steel-concrete composite pile is 31% greater than the sum of it of reinforced concrete pile and it of steel pile. This is caused that ultimate load and Young's modulus of inner concrete increase due to confining effect by outer steel casing. Variation of ultimate load is also insignificant depending on the ratio of length to diameter(L/D), therefore bucking has not an effect on change of ultimate load in case of the L/D below 10.

• 한국공간구조학회논문집
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• 제6권1호
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• pp.75-82
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• 2006

단층 래티스 돔은 작은 단면의 선 부재 조합으로 전체구조물이 구성되는 특성상 구성부재의 세장비, 부재 반개각 하중조건, 접합부 특성 등에 매우 큰 영향을 받으므로, 비선형 좌굴해석에 의한 좌굴하중을 사용해야 하지만 여러 가지 현실적 제약이나 문제점 등에 의해 이러한 것이 제대로 반영되지 않은 설계가 이루어지고 있다. 이러한 이유로 돔 구조물의 설계 시 부재의 과다 설계, 자유로운 형상 설계의 제약 등의 문제점들이 나타나는 것이 지금의 현실이다. 따라서 이 논문의 목적은 위에서 언급된 문제점을 해결하기 위하여 고유치 해석을 통한 선형 좌굴해석에 기초한 비선형 좌굴하중을 예측하고 이를 이용함으로서 보다 효과적인 설계를 가능케 하는 설계식을 제안하는 데 있다.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1999년도 가을 학술발표회 논문집
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• pp.87-94
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• 1999

The structural behavior of welded steel box columns subjected to axial compression and combined load of axial and horizontal load is described. The nonlinear stress-strain relation of the material and residual stress resulted from welds were included in the analysis. Inelastic buckling analysis of hollow rectangular sections of various width-thickness and slenderness ratios was carried out using the semi-analytical and spline finite strip method to investigate the local and global bucking stress and mode interaction. The buckling stress was compared with test results and design curves. Post-buckling behavior was traced by the finite element program(ADINA) and compared with experimental results. The comparison showed that the ultimate stress can be used for the design purpose.

• Steel and Composite Structures
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• 제13권6호
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• pp.539-560
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• 2012

This study uses an explicit numerical algorithm to evaluate the ultimate load capacity analysis of a unit Strarch frame, accounting for the initial imperfection effects of the stress-erection process. Displacement-based filament beam element and an explicit dynamic relaxation method with kinetic damping are used to achieve the analysis. The section is composed of the finite number of filaments that can be conveniently modeled by various material models. Ramberg-Osgood and bilinear kinematic elastic plastic material models are formulated to analyze the nonlinear material behaviors of filaments. The numerical results obtained in the present study are compared with the results of experiment for stress-erection and buckling of unit Strarch frames.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2003년도 봄 학술발표회 논문집
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• pp.403-408
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• 2003

The objective of this study is to understand the variables affected the confinement for the transverse reinforcement of the reinforced concrete structural walls with the T-shaped cross section subjected to cyclic lateral loads. The structural performance of T-shaped walls was advanced by the transverse reinforcement which restrained the concrete subjected to compressive stress. If the arrangement of transverse reinforcement was not suitable for the confinement, T-shaped walls happened the brittle failure by web crushing or bucking of vertical reinforcement at the compression zone. It is necessary to confine transverse reinforcement in order to prevent the these failure. But the location of neutral axis and the magnitude of ultimate strain vary according to the section shape, a ratio of axial load, a ratio of wall cross sectional area to the floor-plan area, an aspect ratio and the reinforcement ratio. Therefore, the objective of this research is to grasp the location of neutral axis and the range which needs for the confinement of transverse reinforcement through the results of the sectional analysis which varies the ratio of axial load and the ratio of vertical reinforcement.