• 한국해양공학회지
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• 제31권6호
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• pp.379-387
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• 2017

In this study, a pile-guide mooring system (PGMS) was designed for an offshore liquefied natural gas bunkering terminal (LNG-BT), which is an essential infrastructure for large LNG-fuelled ships. The PGMS consisted of guide piles to restrict five motions of the floater, except for heave, as well as a seabed truss structure to support the guide piles and foundation piles to fix the system to the seabed. Singapore port was considered for a case study because it is a highly probable ports for LNG bunkering projects. The wave height, current speed, and wind speed in Singapore port were investigated to calculate the environmental loads acting on the hull and PGMS. A load and resistance factor approach was used for the structural design, and a finite element analysis was performed for design verification. The steel usage of the PGMS was analyzed and compared with the material usage of a gravity-based structure under similar LNG capacity and water depth criteria. This paper also describes the water depth limit and wave conditions of the PGMS based on estimation of the initial investment and the present value profit difference. It suggests a suitable LNG-BT support system for various design conditions.

• 한국지반공학회논문집
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• 제31권10호
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• pp.5-16
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• 2015

본 연구에서는 국가건설기준이 한계상태설계법으로 전환됨에 따라 현재 연구기반이 미약한 쏘일네일링의 LRFD 설계법 개발의 일환으로 인발저항에 대한 저항편향계수를 분석하였다. 쏘일네일링의 설계 및 시공 기술수준 등 지역적 특성을 반영하기 위하여 국내 비탈면과 굴착공사에서 수행된 인발시험 자료를 수집하고, 지반특성, 쏘일네일의 제원, 인발시험 결과 등으로 구성된 데이터베이스를 구축하였다. 쏘일네일링의 인발저항에 대한 저항계수를 보정하기 위하여 국내에서 가장 많이 이용되며 비교적 자료수가 충분한 중력식과 가압식 그라우팅공법의 인발저항에 대한 저항편향계수를 산정하였다. 저항편향계수는 1.144~1.325으로 실제 극한인발저항력을 비교적 보수적으로 예측하고 있으며 미국의 연구사례(NCHRP Report)보다 안전측으로 설계가 이루어지고 있으나, 인발저항력에 대한 불확실성은 $COV_R$=0.27~0.43으로 비교적 큰 것으로 나타났다. 또한 가압식 그라우팅공법은 중력식 그라우팅공법에 비해 내재된 안전여유가 많으며, 실제 발휘되는 극한인발저항력의 불확실성이 낮은 것으로 분석되었다.

• 한국철도학회논문집
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• 제12권4호
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• pp.518-525
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• 2009

논문은 샌드위치 복합재가 적용된 바이모달 트램의 설계검증을 위한 구조 성능 시험과 유한요소 해석에 대해 기술하였다. 차체 구조물에 적용된 샌드위치 복합재는 알루미늄 하니컴 심재와 WR580/NF4000 유리섬유/애폭시 면재로 구성되었다. 이때, 차체 구조물의 구조 시험은 JIS E 7105 규정에 따라 수직하중, 압축하중, 비틀림 및 고유진동수 시험이 각각 수행되었다. 그리고 다이얼게이지, 스트레인게이지, 가속도 센서를 통해 얻어진 처짐, 응력, 고유전동수 결과에 따른 구조 안전성을 평가하였다. 그리고 Ansys v11.0을 이용하여 유한요소해석을 수행하였고, 구조 시험 결과와 비교하였다. 구조 시험 결과는 제안된 유한요소 모델을 사용한 구조 해석 결과와 처침, 응력, 고유진동수가 비교적 잘 일치함을 확인하였다.

• 한국전산구조공학회논문집
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• 제30권5호
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• pp.397-404
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• 2017

본 연구의 목적은 트러스의 형태를 바꿔가며 엇갈린 트러스(STF) 시스템의 내진성능을 평가하는 것이다. 예제 구조물은 10층의 철골조 사무실 건물이며, 시스템별로 각각 프랫트러스, 하우트러스, 와렌트러스, 케이트러스와 비렌딜트러스를 적용하였다. 중력하중, 풍하중, 지진하중을 고려한 구조해석을 실시하여 부재에 높은 DCR을 만족하는 단면을 산정한 후 고유주기, 밑면전단력과 층간변위를 산출하였다. 그 후, 역량스펙트럼법을 통해 1.2배의 설계지진(DE)과 최대고려지진(MCE)에 대한 성능점을 산정하고, STF 시스템의 항복여부 및 소성힌지의 분포를 파악하여 구조기준에서 제시한 목표성능수준을 만족하는지 살펴보았다. 평가 결과, 모든 시스템이 해당 목표성능수준을 만족하였으며, 시스템의 경제성 및 효율성을 따져보았을 때, PR10이나 VR10이 가장 적합한 것으로 나타났다.

• 콘크리트학회논문집
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• 제15권3호
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• pp.470-481
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• 2003

플랫 플레이트 구조의 외부접합부는 편심전단에 대해 비대칭형의 위험단면을 가지고 있으며, 위험단면의 길이가 내부접합부 보다 작고 중력하중과 횡하중 모두에 의해 편심전단응력이 발생하게 되므로 뚫림전단파괴에 대해 대단히 취약하다. 외부접합부의 거동은 대단히 복잡하며 또한 구조해석에서 사용하고 있는 강도모델이 부적합하기 때문에, 현 설계기준은 실험결과를 정확히 설명하고 있지 못하다. 본 연구에서는 이러한 현 설계기준의 미비점을 보완하기 위하여 슬래브-기둥 외부접합부에 대해 비선형유한요소해석을 수행하였다. 외부접합부에서는 횡하중의 재하방향에 따라 거동 및 최대강도가 상이하며, 해석결과에 근거하여 하중재하방향 별로 외부접합부에 대한 강도모델을 제안하였다. 제안된 강도모델은 실험결과와의 비교를 통해 검증되었다.

• Steel and Composite Structures
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• 제31권4호
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• pp.373-385
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• 2019

This paper presents a useful in-plane structural analysis of low-rise blind-bolted composite frames with semi-rigid joints. Analytical models were used to predict the moment-rotation relationship of the composite beam-to-column flush endplate joints that produced accurate and reliable results. The comparisons of the analytical model with test results in terms of the moment-rotation response verified the robustness and reliability of the model. Abaqus software was adopted to conduct frame analysis considering the material and geometrical non-linearities. The flexural behaviour of the composite frames was studied by applying the lateral loads incorporating wind and earthquake actions according to the Australian standards. A wide variety of frames with a varied number of bays and storeys was analysed to determine the bending moment envelopes under different load combinations. The design models were finalized that met the strength and serviceability limit state criteria. The results from the frame analysis suggest that among lateral loads, wind loads are more critical in Australia as compared to the earthquake loads. However, gravity loads alone govern the design as maximum sagging and hogging moments in the frames are produced as a result of the load combination with dead and live loads alone. This study provides a preliminary analysis and general understanding of the behaviour of low rise, semi-continuous frames subjected to lateral load characteristics of wind and earthquake conditions in Australia that can be applied in engineering practice.

• Steel and Composite Structures
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• 제15권4호
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• pp.379-397
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• 2013

Conoidal shells are doubly curved stiff surfaces which are easy to cast and fabricate due to their singly ruled property. Application of laminated composites in fabrication of conoidal shells reduces gravity forces and mass induced forces compared to the isotropic constructions due to the high strength to weight ratio of the material. These light weight shells are preferred in the industry to cover large column free open spaces. To ensure design reliability under service conditions, detailed knowledge about different behavioral aspects of conoidal shell is necessary. Hence, in this paper, static bending, free and forced vibration responses of composite conoidal shells are studied. Lagrange's equation of motion is used in conjunction with Hamilton's principle to derive governing equations of the shell. A finite element code using eight noded curved quadratic isoparametric elements is developed to get the solutions. Uniformly distributed load for static bending analysis and three different load time histories for solution of forced vibration problems are considered. Eight different stacking sequences of graphite-epoxy composite and two different boundary conditions are taken up in the present study. The study shows that relative performances of different shell combinations in terms of static behaviour cannot provide an idea about how they will relatively behave under dynamic loads and also the fact that the points of occurrence of maximum static and dynamic displacement may not be same on a shell surface.

• 소성∙가공
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• 제27권3호
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• pp.139-144
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• 2018

Many studies have been conducted on the process of forming magnesium alloy sheets to reduce the body weights of vehicles. Magnesium has a lower specific gravity than steel and also has a higher specific strength. Mg alloy sheets have low formability and a lot of springback due to their limited ductility and low young's modulus. As the temperature increases, the yield strength of the material decreases. Warm forming increases the formability and minimizes the springback of a material by heating it and the die to reduce the required load at forming. In this study, the temperature of the AZ31B sheet was controlled in order to reduce springback and increase formability. However, as the temperature increased, the deformation characteristics of the material changed and the radius of curvature of the material increased. The load and springback amount required for forming were analyzed according to the temperature and the bottoming force in the bending deformation.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2001년도 제16회 학술발표회 논문초록집
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• pp.91-94
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• 2001

A structural test of the wind turbine rotor blade must be required to evaluate the uncertainty in design assessment due to use of material, design concepts, production processes and so on, and the possible impact on the structural integrity. In the full-scale static strength test, the measuring parameters are strain, displacements, loads, weight and the center of gravity. There are test equipments, measuring sensors, a test rig and fixtures to obtain measuring parameters. In order to simulate the aerodynamics load, the three-point loading method instead of the one-point loading method is applied. There is slightly some difference between the measured results and the predicted results with the reference fiber volume fraction of 60%. However, the agreement between the measured results and the predicted results with the actual fiber volume fraction of 52.5% is good. Even though a slightly non-linearity from 80% loading to 100% loading, a linear static solution is sufficient for the design purpose as the amount of the non-linearity is relatively small. Comparison between measured and predicted strain results at the maximum thickness positions of the blade profile for 0.236R(5.56m), 0.493R(11.59m) and 0.574R(13.43m), under 20%, 40%, 60%, 80% and 100% loadings for the upper part of the blade. The predicted values are in good agreement with the measured values.

• 한국추진공학회지
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• 제5권1호
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• pp.76-81
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• 2001

A structural test of the wind turbine rotor blade is to evaluate the uncertainty of design due to selection of material, design concepts, production processes and so on, and their possible impacts on the structural integrity. In the full-scale static strength test, the measuring parameters are strain and displacements vs. loads, weight and the center of gravity. In order to simulate the aerodynamics load, the three-point loading method is applied. There is slight difference between the measured results and the predicted results for the reference fiber volume fraction of 60% . However, the agreement between the measured results and the predicted results with the actual fiber volume fraction of 52.5% is good. Even though a slightly non-linearity from 80% loading to 100% loading exists, a linear static solution is sufficient for the design purpose due to te small amount of non-linearity. Comparison between measured and predicted strain results at the maximum thickness positions of the blade profile for 0.236R(5.56m), 0.493R(11.59m) and 0.574R(13.43m), under 20%, 40%, 60%, 80% and 100% loadings for the upper part of the blade. The predicted values are in good agreement with the measured values.