• Proceedings of KOSOMES biannual meeting
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• 2005.05a
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• pp.147-154
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• 2005

The ship plating is generally subjected to combined in-plane load and lateral pressure loads. In-plane loads include axial load and edge shear, which are mainly induced by overall hull girder bending and torsion of the vessel. Lateral pressure is due to water pressure and cargo. These load components are not always applied simultaneously, but more than one can normally exist and interact Hence, for more rational and safe design of ship structures, it is of crucial importance to better understand the interaction relationship of the buckling and ultimate strength for ship plating under combined loads. Actual ship plates are subjected to relatively small water pressure except for the impact load due to slamming and panting etc. The present paper describes an accurate and fast procedure for analyzing the elastic-plastic large deflection behavior up to the ultimate limit state of ship plates under combined loads. In this paper, the ultimate strength characteristics of plates under axial compressive loads and lateral pressure loads are investigated through ANSYS elastic-plastic large deflection finite element analysis with varying lateral pressure load level.

• Journal of the Korean Society of Marine Environment & Safety
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• v.12 no.1 s.24
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• pp.67-74
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• 2006

The ship plating is generally subjected to combined in-plane load and lateral pressure loads. In-plane loads include axial load and edge shear, which are mainly induced by overall hull girder bending and torsion rf the vessel. Lateral pressure is due to water pressure and cargo. These load components are not always applied simultaneously, but more than one can normally exist and interact. Hence, for more rational and safe design rf ship structures, it is of crucial importance to better understand the interaction relationship of the buckling and ultimate strength for ship plating under combined loads. Actual ship plates are subjected to relatively small water pressure except for the impact load due to slamming and panting etc. The present paper describes an accurate and fast procedure for analyzing the elastic-plastic large deflection behavior up to the ultimate limit state of ship plates under combined loads. In this paper, the ultimate strength characteristics of plates under axial compressive loads and lateral pressure loads are investigated secondary buckling behavior through ANSYS elastic-plastic large deflection finite element analysis with varying lateral pressure load level.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2017.04a
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• pp.56-56
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• 2017

점적 호스 중 PC 드립은 경질 호스의 내부에 Micro-path가 부착된 유로장치와 압력을 보상하는 연질의 실리콘으로 구성되어 있다. 이때 일정압력에서 적정 길이까지 동시에 내부 압력을 유지하며 균등하게 유출구를 통하여 유량을 공급하는 압력보상 기능이 매우 중요하다. 그러나 이 부분에 대한 기술은 선진국에 비해 아직 부족하여 수입에 의존하는 경향이 매우 높다. 뿐만 아니라 선진국 제품에 비해 유로장치 및 연질 실리콘의 탄성이 균일하지 못해 압력에 따른 유량의 편차가 큰 편이다. 본 연구에서는 우리나라 제품의 PC 드립 압력 균등성 기술을 향상시키기 위해 PC 드립의 핵심기술인 연질 실리콘의 성능에 대한 평가와 유량의 편차를 분석하여 문제점을 통한 개선방안을 제시하고자 하였다. 연질 실리콘의 규격은 $17{\times}8{\times}0.85mm$ (가로${\times}$세로${\times}$두께)로서 Water line의 내부에 결합되어 구성된다. PC 드립용 실리콘은 국내 A사 제품을 중심으로 하여 성능을 측정하였다. 측정을 정밀하게 하기 위해 Microtester를 사용하여 일정하게 하중이 부과되도록 하였다. 연질의 실리콘의 경도는 압력 보상에 중요한 기능을 하고 있으며 또한 PC 드립의 경질 미로와 같이 압력을 제어하는 역할을 하고 있다. 국내 A사의 실리콘 경도는 이상적인 실리콘 경도에 비하면 매우 불균일하였다. 세부적으로는 40 이하의 낮은 경도에서는 비교적 일치하였으나 경도 45 이상에서는 큰 차이를 보여주고 있었다. 국내 A사의 실리콘 경도에 따른 공급유량의 특성에서는 실리콘의 경도가 낮을수록 실리콘은 무르며 탄성이 줄어든다. 반면에 경도가 높을수록 탄성이 커지고 딱딱한 특성을 가진다. 동일한 PC 드립에 실리콘의 경도별 특성은 경도에 따른 유량이 반드시 일정하지 않으며 대체로 경도가 높을수록 동일 압력에 대해 유량이 많아지는 것을 알 수 있었다. 압력의 변화에 대해 유량이 일정하게 유지하는 특성을 가질수록 사용범위가 넓어지고 안정성이 높은 것으로 판단되며 실리콘 경도 35~55 범위에서 1~2bar의 공급압력에서 사용하는 것이 적합할 것으로 보여진다. 경도 45의 실리콘을 사용하여 수입 드립, 국내 A사의 드립 및 수입과 국내 혼용시 압력에 따른 공급유량의 특성을 분석하였다. 최대 유량과 최소 유량에서 발생되는 오차는 수입 실리콘이 비교적 작았으나 3.6 bar 이상에서는 유량이 급격히 떨어지는 양상을 보였다. 국내 A사의 제품은 0.8~2.0 bar 까지 성능이 비슷했으나 0.8 bar 이하에서는 오차가 있었으나 높은 압력에서는 오히려 성능이 우수하였다. 수입 드립과 다소 유사한 성능을 나타낸 것이 A사 드립과 수입 실리콘을 혼용하여 사용한 것은 전체적으로 비슷한 양상을 나타내었다. 따라서 실리콘 경도 오차를 고려하면 압력별 유량의 변화는 실리콘의 경도와 밀접한 관계가 있는 것으로 판단되었다.

• Journal of the Korean Vacuum Society
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• v.16 no.4
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• pp.244-249
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• 2007

Deadweight piston gauge have been widely used as a fundamental instrument of precise pressure measurement because they are robust, accurate, potable, convenient to use and are able to realize the definition of pressure as farce per unit area. Basically, a deadweight piston gauge consists of a piston mounted vertically in a close-fitting cylinder filled with a gas and weights of known mass values. The pressure to be measured is applied to the base of the piston generating an upward vertical force, and is balanced by the downward gravitational force generated by weights. These instruments can be used to measure pressures above 10 kPa because of tare weights including piston. However, using a variable bell-jar pressure method and a newly developed weight loading device we can extend the application range of deadweight piston gauge to lower pressures. In this paper, we present the practical calibration results for two CDGs(Capacitance diaphragm gauge, MKS) with full-scale ranges of 1.33 kPa and 13.3 kPa, respectively.

• Journal of Korean Society of Coastal and Ocean Engineers
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• v.23 no.1
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• pp.63-69
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• 2011

In this paper, the wave forces on a cylindrical aquaculture fish cage, which consists of the porous mesh with the uniform porosity, are analyzed using matched eigenfunction expansion method. The boundary condition on the porous net is derived based on the Darcy's law, which implies that the velocity of the fluid passing through the net is linearly proportional to the pressure difference between two sides of the net. The wave forces and wave responses are investigated by changing the porous parameter of porous net as well as the submerged position (floating type, bottom-mounted type) of an aquaculture fish cage. It is found that the wave forces on a bottom-mounted type are largely decreased compared with that on a floating type. Also, the porosity of the netting structure plays an important role in reducing the wave forces and the wave elevation in the vicinity of an aquaculture fish cage.

• Journal of Energy Engineering
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• v.17 no.4
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• pp.204-211
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• 2008

Polyethylene(PE) pipes have been widely used as they are easy to construct and suitable for economical efficient when they are compared with metal pipelines. This paper studied the effect of various external loadings on stress and deflection of the buried PE pipes using Finite Element Method(FEM). For this purpose, stresses of buried PE pipes were calculated according to the loading condition such as pipe types(pipe diameter $50{\sim}400mm$), burial depths($0.6{\sim}1.2m$) and internal pressures($0.4{\sim}4bar$). As a result, it was founded the effect and relation with each of loading conditions under the buried condition.

• Journal of the Korean Society of Hazard Mitigation
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• v.8 no.1
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• pp.39-45
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• 2008

The most important elements in flexible pavement design criteria are stress and strain distributions. To obtain reasonable stress and strain distributions in pavements, moving wheel loads must be applied to analyze the pavement responses. In this study, finite element analysis was used to identify the three-dimensional states using the vehicle load into a constant-position / time-variable load (25, 50 and 80km/hr). In an elastic system, the strain is the same in both longitudinal and transverse directions under a single wheel. However, the same is not necessary in a viscoelastic system. Test results showed that the maximum values between transverse and longitudinal strains the bottom of asphalt concrete base layers under 25km/hr were were about 40 percent.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.5
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• pp.262-267
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• 2017

The number of shops needed for the fabrication of a sphere type cargo tank for an LNG carrier is proportional to the size of the tank to be constructed. Due to the limitations of facility investment, it is difficult to fabricate various size tanks with a perfectly spherical shape in the (factory). An efficient method of increasing the capacity of the cargo tank is to extend the conventional sphere type LNG tank vertically by inserting a cylindrical shell structure. In this study, equations for the dynamic pressure distribution due to horizontal acceleration are derived for a sphere type LNG tank with central extension. The derived equations can be easily applied to the design and structural assessment of a sphere type LNG tank with central extension. Furthermore, the results of this study can be combined with the static design loads previously reported by Shin & Ko [9], in order to establish a simplified analysis method which enables a precise initial estimate to be obtained, thereby obviating the need for a time consuming finite element analysis.

• Composites Research
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• v.20 no.4
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• pp.31-41
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• 2007

Dome shape design methods of Filament Winding (FW) composite pressure vessel, which can suggest various dome contour according to the external loading conditions, were investigated analytically and numerically. The performance indices(PV/W) of the pressure vessels with same cylinder radius and boss opening but different dome shape were evaluated by finite element analysis under the internal pressure loading condition. The analysis results showed that as the dome shape becomes flat, the performance index decreases significantly due to the reduced burst pressure. Especially, for the case of the high value of the parameter ro, the ratio between the radii of the cylinder part and the boss opening, the flat dome is disadvantageous in the aspect of the weight reduction, and additional reinforcing dome design technique should be required to increase the burst pressure. For example, above ro=0.54 condition, the dome shape change according to the loading condition could cause the low burst pressure and increase of composite weight in dome region and is not recommendable except for the special case that maximum inner volume or sufficient space between skirt and dome is the primary design objective. However, at ro=0.35, the dome shape change brings not so significant differences in the performance of FW vessel.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.9
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• pp.653-661
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• 2020

This study derives numerically the shell Knockdown factors for the isogrid-stiffened cylinders of space launch vehicles when the axially compressive force and internal pressure are applied simultaneously. A commercial nonlinear finite element analysis software, ABAQUS, is used for the present work. Nonlinear postbuckling analyses are conducted to calculate the global buckling loads of a cylinder without and with the internal pressure. The shell Knockdown factor is numerically derived using the predicted global buckling loads without and with the geometrically initial imperfection of a cylinder. When the internal pressure of 500 kPa and compressive force are applied to the cylinder, the global buckling load and Knockdown factor increases by 304% and 53%, respectively, as compared to the results without the internal pressure.