• Steel and Composite Structures
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• 제45권1호
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• pp.51-66
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• 2022

This paper presents the axial compression behavior of partially encased composite (PEC) columns using H-shaped structural steel. In the experimental program, a total of eight PEC columns with H-shaped steel sections of different flange and web slenderness ratios were tested to investigate the interactive mechanism between steel and concrete. The test results showed that the PEC columns could sustain the load well beyond the peak load provided that the flange slenderness ratio was not greater than five. In addition, the previous analytical model was extended to predict the axial load-strain relationships of the PEC columns with H-shaped steel sections. A good agreement between the predicted load-strain relationships and test data was observed. Using the analytical model, the effects of compressive strength of concrete (21 to 69 MPa), yield strength of steel (245 to 525 MPa), slenderness ratio of flange (4 to 10), and slenderness ratio of web (10 to 25) on the interactive mechanism (K_h = confinement factor for highly confined concrete and K_w = reduction factor for steel web) and ductility index (DI = ratio between strain at peak load and strain at proportional load) were assessed. The numerical results showed that the slenderness of steel flange and yield strength of steel significantly influenced the compression behavior of the PEC columns.

• 한국강구조학회 논문집
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• 제29권1호
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• pp.81-88
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• 2017

확장단부판 접합부는 강구조물의 보-기둥 접합부 혹은 변단면 부재로 구성된 PEB 구조시스템에 적용되는 접합부의 한 형태이다. 확장단부판 접합부는 접합부를 구성하는 단부판의 두께, 고장력볼트의 게이지 거리, 고장력볼트 축부의 직경, 고장력볼트의 개수 등의 영향으로 상이한 거동특성을 나타낸다. 확장단부판 접합부는 미국 및 유럽 등지에서는 다양한 형태로 강구조물의 기둥-보 접합부에 적용되고 있으나 우리나라에서는 널리 적용되고 있지 않다. 이러한 이유로는 확장단부판 접합부에 대한 설계강도식 제안, 접합부상세 제안, 내진성능 평가, 제작 및 시공지침서 개발 등이 적절히 이루어지지 못하고 있기 때문이다. 따라서 이 연구는 비보강 확장단부판 접합부의 국내 적용을 위한 기초자료를 제공하기 위하여 진행하였다. 이를 위하여 두께 12mm의 비보강 확장단부판에 대한 비선형 유한요소해석 및 실험을 수행하였다.

• 대한두개안면성형외과학회지
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• 제12권1호
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• pp.12-16
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• 2011

Purpose: This study examined the biomechanical stability of four different plating techniques in the experimental model of mandibular subcondyle fracture. Methods: Twenty standardized bovine tibia bone samples ($7{\times}1.5{\times}1.0cm$) were used for this study. Each of the four sets of tibia bone was cut to mimic a perpendicular subcondyle fracture in the center area. The osteotomized tibia bone was fixed using one of four different fixation groups (A,B,C,D). The fixation systems included single 2.0 mm 4 hole mini adaption plate (A), single 2.0 mm 4 hole dynamic compression miniplate (B), double fixation with 2.0 mm 4 hole mini adaption plate (C), double fixation with a 2.0 mm 4 hole mini adaption plate and 2.0 mm 4 hole dynamic compression miniplate (D). A bending force was applied to the experimental model using a pressure machine (858 table top system, $MTS^{(R)}$) until failure occurred. The load for permanent deformation, maximum load of failure were measured in the load displacement curve with the chart recorder. Results: Double fixation with a 2.0 mm 4 hole mini adaption plate and a 2.0 mm 4 hole dynamic compression miniplate (D) applied to the anterior and posterior regions of the subcondyle experimental model showed the highest load to failure. Conclusion: From this study, double fixation with an adaption plate and dynamic compression miniplate fixation technique produced the greatest biomechanical stability. This technique may be considered a useful means of fixation to reduce the postoperative internal maxillary fixation period and achieve early mobility of the jaw.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2004년도 추계학술대회 논문집
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• pp.1172-1175
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• 2004

At present, CHS(Compression Hip Screw) is one of the best prosthesis for the intertrochanteric fracture. There is nothing to evaluate the CHS itself with the finite element analysis and mechanical tests. They have same ways of the experimental test of the ASTM standards. The purpose of this study is to evaluate the existing CHS and the new CHS which have transformational design factors with finite element analysis and mechanical tests. The mechanical tests are divided into compression tests and fatigue test for evaluating the failure load, strength and fatigue life. This finite element method is same as the experimental test of the ASTM standards. Under 300N of compression load at the lag screw head. There are less differences between Group (5H, basic type) and Group which has 8 screw holes. However, there are lots of big differences between Group and Group which is reinforced about thickness of the neck range. Moreover, the comparison of Group and Group shows similar tendency of the comparison of Group and Group . The Group is reinforced the neck range from Group. After the experimental tests and the finite element analysis, the most effective design factor of the compression hip screws is the reinforcement of the thickness, even though, there are lots of design factors. Moreover, to unite the lag screw with the plate and to analyze by static analysis, the result of this method can be used with experimental test or instead of it.

• 한국분무공학회지
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• 제24권1호
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• pp.35-42
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• 2019

Syngas is widely produced by incomplete combustion of coal, water vapor, and air (oxygen) in a high-temperature/high-pressure gasifier through a coal-gasification process for power generation. In this study, a simulation syngas which was mainly composed of $H_2$, CO, $CO_2$, and $N_2$ was fueled with diesel. A modified single cylinder compression ignition (CI) engine is equipped with intake port syngas supply system and mechanical diesel direct injection system for dual fuel combustion. Combustion and emission characteristics of the engine were investigated by applying various syngas composition ratios and compression ratios. Diesel fuel injection timing was optimized to increase indicated thermal efficiency (ITE) at the engine speed 1,800 rpm and part load net indicated mean effective pressure ($IMEP_{net}$) 2 to 5 bar. ITE of the engine increased with the $H_2$ concentration, compression ratio and engine load. With 45% of $H_2$ concentration, compression ratio 17.1 and $IMEP_{net}$ 5 bar, ITE of 41.5% was achieved, which is equivalent to that of only diesel fuel operation.

• 한국지반공학회지:지반
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• 제14권6호
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• pp.5-16
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• 1998

모래지반에서 모형강널말뚝의 수직하중에 대한 거동을 알아보기 위하여 말뚝단면적이 동일하고 플랜지의 개구정도가 각기 다른 5개의 모형말뚝을 제작하였으며, 각 말뚝에 대해 상대밀도, 하중작용방향(압축, 인발)을 달리하여 토조내에서 실내 모형말뚝시험을 수행하였다. 동일한 말뚝에 대해 인발하중을 받는 경우보다 압축하중을 받는 경우가 극한지지력에 있어 100%가량 크며, 상대밀도가 조밀할수록 그 차이는 더욱 증가하였다. 인발재하시험에서 극한지지력과 극한상태의 침하량은 상대밀도가 증가함에 따라 증가하였으며, 동일한 지반조건하에서 개구정도의 변화에 따른 극한지지력과 침하량은 일정한 범위내에 존재하였다. 압축하중조건하에서 극한지지력은 개구정도가 30$^{\circ}$이내에 있을 경우 가장 크게 나타났으며, 상대밀도가 커질수록 이러한 경향이 뚜렷하게 나타났다. 단면의 변화에 따른 극한하중 변화는 하중분포의 해석결과 부분폐색효과에 기인된 것으로 생각된다.

• 한국지반공학회논문집
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• 제19권6호
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• pp.227-243
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• 2003

강관말뚝의 속채움 콘크리트 B방법에서 미끌림방지턱의 구조적인 특성을 알아보기 위하여, 강관말뚝머리의 내부에 미끌림방지턱을 설치하지 않은 시험체와 2단의 곡률 강편 미끌림방지턱을 강관말뚝내부에 용접한 시험체(시방서 방법), 그리고 미끌림방지턱을 다수의 곡률 강편과 고장력볼트로 체결한 시험체(개발형 방법)에 대하여 실물크기 인발 및 압발 실험을 수행하였다. 그 결과, 미끌림방지턱이 없는 시험체는 최대인발하중 15.6tonf에서, 최대압발하중 27.57tonf에서 콘크리트의 화학적 부착파괴가 발생하였다. 그리고 미끌림방지턱이 있는 시방서 방법과 개발형 방법의 시험체는 없는 시험체보다 최대인발하중의 약 8.9배와 최대압발하중의 6.2배 크게 나타났다. 또한 시방서 방법과 개발형 방법의 하단 미끌림방지턱에 대한 하중분담비율은 거의 동일한 거동을 보인 반면에, 상단 미끌림방지턱은 시방서방법보다 개발형 방법의 하중분담비율이 크게 기여하였다. 그리고 시방서 방법과 개발형 방법의 미끌림방지턱 형상에 의한 합성작용과 구조성능은 거의 동일하였다.

• 소성∙가공
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• 제4권1호
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• pp.39-47
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• 1995

The compression molding of SMC (sheet molding compund) at room temperature was analyzed based on rigid-viscoplastic approach by three dimensional finite element program. The developed program was tested by solving the three dimensional compression of wedge type specimens of aluminum alloys at various processing conditions. The simulation results were compared well to the experimental results available in the literature. based on this comparison the program was proved to be valid and was further applied in solving compression molding of SMC, which is a thermosetting material reinforced with chopped fiber glass. To investigate the effects of friction conditions and mold closing speeds for compression molding of SMC charge at room temperature, compressions of the cylindrical and rectangular shaped SMC were analyzed for various friction conditions and mold closing speeds. The calculated load values were compared to the experimental results for the compression molding of cylindrical specimen.

• Structural Engineering and Mechanics
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• 제51권6호
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• pp.955-971
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• 2014

Large post-buckling behavior of Timoshenko beams subjected to non-follower axial compression loads are studied in this paper by using the total Lagrangian Timoshenko beam element approximation. Two types of support conditions for the beams are considered. In the case of beams subjected to compression loads, load rise causes compressible forces end therefore buckling and post-buckling phenomena occurs. It is known that post-buckling problems are geometrically nonlinear problems. The considered highly non-linear problem is solved considering full geometric non-linearity by using incremental displacement-based finite element method in conjunction with Newton-Raphson iteration method. There is no restriction on the magnitudes of deflections and rotations in contradistinction to von-Karman strain displacement relations of the beam. The beams considered in numerical examples are made of lower-Carbon Steel. In the study, the relationships between deflections, rotational angles, critical buckling loads, post-buckling configuration, Cauchy stress of the beams and load rising are illustrated in detail in post-buckling case.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1999년도 봄 학술발표회 논문집
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• pp.252-259
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• 1999

One of the most important factors for a proper design of a slender compression member may be the exact determination of the elastic critical load of that member. In the cases of non-prismatic compression member, however, there are times when the exact critical load becomes impossible to determinate if one relies on the neutral equilibrium method or energy principle. Here in this paper, the approximate critical loads of symmetrically or non-symmetrically tapered members are computed by finite element method. The two parameters considered in this numerical analysis are the taper parameter, $\alpha$ and the sectional property parameters, m. The computed results for each sectional property parameter, m are presented in an algebraic equation which agrees with those by F.E.M The algebraic equation can be easily used by structural engineers, who are engaged in structural analysis and design of non-prismatic compression member.