• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 추계학술발표대회 논문집
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• pp.121-124
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• 2004

The purpose of this study is to define the optimized layer pattern of composite wind turbine blade by using a commercial FEM program and to perform the fatigue test of T-Bolt. FEM analysis is done by using a PATRAN and ABAQUS to get a information about stress distribution ,critical deformation shape and get a critical load factor in local buckling analysis. As a result of the linear and nonlinear structural analysis, layer pattern of blade was optimized. T-Bolt is a connecting part of wind turbine blade and rotor hub, therefore T-bolt is cirtical part of wind turbine blade. T-bolt fatigue test is conducted to get a information of life cycle of T-bolt. The test is done by using a hydraulic actuator system

• 한국공간구조학회논문집
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• 제10권4호
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• pp.67-74
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• 2010

대공간 구조형식을 갖는 단층 래티스 돔은 역학성, 가능성, 심미성 등을 갖는 구조물로서 그 용도가 점점 확대되고 있다. 단층 래티스 돔의 골조 격자 패턴은 무수히 존재하며, 그 대표적인 패턴에는 삼각형, 사각형, 육각형, 라멜라형, 리브형 등이 있다. 대공간 구조물의 경우, 일반구조물과 달리 재래적인 공법으로 지붕 골조를 시공할 경우 많은 가설재가 소요됨으로 시공비 증가가 예상된다. 따라서 대공간 구조물의 지붕 골조 설치는 특수 Erection 공법에 의하는 것이 일반적이며, 그 중 지상에서 지붕골조를 설치 후 jack-up 서포트에 의해 골조를 인양하는 Step-Up 공법을 적용할 경우 공기와 공비의 대폭적인 절감이 예상된다. 따라서 본 논문의 목적은 Step-Up 공법에 의해 단층라멜라 돔의 지붕골조를 시공할 경우, 인양 중 가설 서포트 개수와 위치에 따른 좌굴특성을 검토하는 것이다. 연구 결과 서포트 개수 및 위치에 따른 단층라멜라 돔의 다양한 좌굴 특성에 관한 실무자를 위한 기초적인 자료를 얻을 수 있었다.

• 대한조선학회 특별논문집
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• 대한조선학회 2006년도 특별논문집
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• pp.89-96
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• 2006

The objective of this paper is to find out a reasonable method for docking analysis of ships. The characteristics of reaction force distribution under docking condition are investigated by carrying out parametric study. To assess the allowable reaction force on keel block from structural strength point of view, two kinds of structural assessment methods are proposed in accordance with expected collapse pattern. In order to verify the proposed method, linear buckling and elasto-plastic large deflection analyses of typical double bottom structure are carried out and the results are compared.

• Computers and Concrete
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• 제29권4호
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• pp.219-235
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• 2022

Strengthening slender reinforced concrete (RC) columns is a challenge. They are susceptible to overall buckling that induces bending moment and axial compression. This study presents the precise three-dimensional finite element modeling of slender RC columns strengthened with fiber-reinforced polymer (FRP) composites sheets with various patterns under concentric or eccentric compression. The slenderness ratio λ (height/width ratio) of the studied columns ranged from 15 to 35. First, to determine the optimal modeling procedure, nine alternative nonlinear finite element models were presented to simulate the experimental behavior of seven FRP-strengthened slender RC columns under eccentric compression. The models simulated concrete behavior under compression and tension, FRP laminate sheets with different fiber orientations, crack propagation, FRP-concrete interface, and eccentric compression. Then, the validated modeling procedure was applied to simulate 58 FRP-strengthened slender RC columns under compression with minor eccentricity to represent the inevitable geometric imperfections. The simulated columns showed two cross sections (square and rectangular), variable λ values (15, 22, and 35), and four strengthening patterns for FRP sheet layers (hoop H, longitudinal L, partial longitudinal L_w, and longitudinal coupled with hoop LH). For λ=15-22, pattern L showed the highest strengthening effectiveness, pattern L_w showed brittle failure, steel reinforcement bars exhibited compressive yielding, ties exhibited tensile yielding, and concrete failed under compression. For λ>22, pattern L_w outperformed pattern L in terms of the strengthening effectiveness relative to equivalent weight of FRP layers, steel reinforcement bars exhibited crossover tensile strain, and concrete failed under tension. Patterns H and LH (compared with pattern L) showed minor strengthening effectiveness.

• 한국항해항만학회지
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• 제31권3호
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• pp.271-279
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• 2007

선체구조는 기본적으로 판부재의 조합으로 이루어져 있으며, 이러한 판부재의 하중분담 능력 혹은 최종강도 평가는 선체구조의 합리적인 설계 및 구조의 안정성 평가에 있어서는 아주 중요하다. 또한, 선체구조를 구성하고 있는 구조요소들은 작용외력에 대하여 개별적으로 작용하지 않으며 전체적으로 연속거동을 하게 된다. 실제 선박에서의 붕괴형태 중 한가지는 종방향 굽휨에 의해서 갑판 혹은 선저부에 좌굴 및 소성붕괴이다. 그래서, 합리적인 설계에서는 이러한 급작스런 붕괴형태를 방지하기 위하여 좌굴 및 소성붕괴 거동을 파악하는 것이 아주 중요하며, 실제 선박에서는 갑판부와 선저부에서는 하중분담 능력을 증가시키기 위하여 여러개의 종보강재를 가진 보강판 구조의 설계를 하게 된다. 본 연구에서는 선체 판넬구조의 모델링 방법에 따른 최종강도 거동의 차이를 분석하여, 합리적인 모델링영역을 규명하고자 한다. 사용된 해석 모델은 실제 상선의 이중저구조에서 사용되는 판넬에서 채택하였으며 유한요소해석 모델링 시 3가지 단면형상에 대해 각각 6가지 서로 다른 해석모델을 적용하였으며, 이때 보강재의 단면형상을 변화하였다. 본 연구의 목적은 압축하중이 작용하는 선체 보강판구조에서 해석영역에 대한 좌굴 및 최종강도 거동의 특성을 분석하였다.

• 한국지진공학회:학술대회논문집
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• 한국지진공학회 2000년도 추계 학술발표회 논문집 Proceedings of EESK Conference-Fall 2000
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• pp.184-191
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• 2000

In this research, a numerical model is developed for analysis of buried pipelines considering longitudinal permanent ground deformation(PGD) due to liquefaction induced lateral spreading. Buried pipelines and surrounding soil are medeled as continuous pipelines using the beam elements and a series of elasto-plastic springs uniformly distributed along the pipelines, respectively. Idealized various PGD patte군 based on the observation of PGD are used as a loading configuration and the length of the lateral spread zone is considered as a loading parameter. Numerical results are verified with other research results and efficient applicability of developed procedure is shown. Analyses are performed by varying different parameters such as PGD pattern, pipe diameter and pipe thickness. Results show that response of buried pipelines are more affected by pipe thickness than pipe diameter. Finally, the critical length of the lateral spread zone and the critical magnitude of PGD which cause yielding, local buckling or tension failure are proposed for the steel pipe which are normally used in Korea.

• 한국강구조학회 논문집
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• 제23권2호
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• pp.229-236
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• 2011

본 연구는 폭두께비(W/T)에 따른 중심압축하중을 받는 SC(Steel Plate-Concrete)구조의 압축거동 특성을 파악하는 것이 주목적이다. SC구조는 전단 연결재를 갖는 샌드위치 강판 사이에 콘크리트를 타설하여 시공하는 구조이다. SC구조의 실험체는 폭두께비(W/T)가 1.60와 3.56인 실험체로 구분하였다. 실험을 통하여 다음과 같은 결과를 얻었다. SC구조 실험체의 파괴양상은 최대압축강도에 도달하기 전에 스터드와 스터드 사이 강판이 국부좌굴하고 콘크리트는 일부 균열 및 박리현상이 나타났다. 또한 SC구조 실험체의 최대압축강도는 기존 설계기준식(AISC 2005, ACI318-05 및 KBC 2005)에 의한 압축강도보다 거의 크게 나타났다. SC구조 실험체의 폭두께비(W/T)가 증가할수록 강판에 의한 SC구조 실험체의 콘크리트 구속효과는 감소하는 것으로 나타났다.

• 국제강구조저널
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• 제18권4호
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• pp.1210-1218
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• 2018

A new type of earthquake-resisting element that consists of a steel plate shear wall with slits is introduced. The infill steel plate is divided into a series of vertical flexural links with vertical links. The steel plate shear walls absorb energy by means of in-plane bending deformation of the flexural links and the energy dissipation capacity of the plastic hinges formed at both ends of the flexural links when under lateral loads. In this paper, finite element analysis and experimental studies at low cyclic loadings were conducted on specimens with steel plate shear walls with multilayer slits. The effects caused by varied slit pattern in terms of slit design parameters on lateral stiffness, ultimate bearing capacity and hysteretic behavior of the shear walls were analyzed. Results showed that the failure mode of steel plate shear walls with a single-layer slit was more likely to be out-of-plane buckling of the flexural links. As a result, the lateral stiffness and the ultimate bearing capacity were relatively lower when the precondition of the total height of the vertical slits remained the same. Differently, the failure mode of steel plate shear walls with multilayer slits was prone to global buckling of the infill steel plates; more obvious tensile fields provided evidence to the fact of higher lateral stiffness and excellent ultimate bearing capacity. It was also concluded that multilayer specimens exhibited better energy dissipation capacity compared with single-layer plate shear walls.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2005년도 춘계학술대회 논문집
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• pp.458-462
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• 2005

This paper deal with the optimal lamination condition of cylindrical shell applied new composite URN300 for a study of composite empirical formula. Finite element analyses for isotropic materials considered element numbers and boundary conditions are compared with existing empirical formulas to apply FE analysis for composite. And composite tensile test is done to know the composite material applied FE analysis for composite. The results of FE analyses for isotropic materials have indicated that Optimal element number and boundary condition were 1600 and both simple support. These conditions were applied in composite FE analyses. Ply orientations and lamination patterns in FE analyses for composite were considered. Ply orientations are $0^{\circ},\;15^{\circ},\;30^{\circ},\;45^{\circ},\;60^{\circ},\;75^{\circ},\;and\;90^{\circ}$. Lamination patterns are $[\pm\theta/0/90]_{14s]$ and $[\pm\theta_{14}/0_{14}/90_{14}]_s$ in FE analysis. Lamination pattern $[\pm\theta_{14}/0_{14}/90_{14}]_s$ is the equivalent model of $[\pm\theta/0/90]_{14s}$. At the result of this study, the FE analyses for composite have indicated that the optimized ply orientation $75^{\circ}$ is and real model must use in FE analysis for accurate results.

• Steel and Composite Structures
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• 제29권3호
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• pp.319-332
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• 2018

This paper investigates the free vibration of geometrically imperfect functionally graded car-bon nanotube-reinforced composite (FG-CNTRC) beams that are integrated with two sur-face-bonded piezoelectric layers and subjected to a combined action of a uniform temperature rise, a constant actuator voltage and an in-plane force. The material properties of FG-CNTRCs are assumed to be temperature-dependent and vary continuously across the thick-ness. A generic imperfection function is employed to simulate various possible imperfections with different shapes and locations in the beam. The governing equations that account for the influence of initial geometric imperfection are derived based on the first-order shear deformation theory. The postbuckling configurations of FG-CNTRC hybrid beams are determined by the differential quadrature method combined with the modified Newton-Raphson technique, after which the fundamental frequencies of hybrid beams in the postbuckled state are obtained by a standard eigenvalue algorithm. The effects of CNT distribution pattern and volume fraction, geometric imperfection, thermo-electro-mechanical load, as well as boundary condition are examined in detail through parametric studies. The results show that the fundamental frequency of an imperfect beam is higher than that of its perfect counterpart. The influence of geometric imperfection tends to be much more pronounced around the critical buckling temperature.