• Proceedings of the Korean Vacuum Society Conference
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• 2012.02a
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• pp.498-498
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• 2012

직류 아크 토치를 이용하여 열플라즈마를 발생시키는 방법은 전극의 구성에 따라 크게 비이송식(non-transferred)과 이송식(transferred)의 2가지 형태로 나눌 수 있다. 1950년대 H. Maecker 등에 의해 이론적 기초가 형성되기 시작한 이송식 아크 플라즈마 발생장치는 처리 대상물질을 전극으로 사용하여 양극에서의 에너지 전달을 직접 이용할 수 있으므로 열효율이 매우 높기 때문에 이를 이용한 고출력 토치에 관한 활발한 연구가 지속되고 있다. 본 연구에서는 대기압 아르곤 자유연소아크 방전에 의해 발생되는 열플라즈마의 열유동 특성을 수치적으로 해석하기 위하여 아크 기둥의 온도, 압력 및 속도 특성을 Navier-Stokes 방정식과 Maxwell 방정식을 연계 계산하였다. 또한 아크-전극 상호작용(arc-electrode interaction) 모델링을 통한 양극(anode)인 처리 대상물질로의 에너지 플럭스 유입을 고려하여 전극 내부의 온도분포를 계산하였다. 해석결과를 검증하기 위하여 음극과 양극 사이 플라즈마 기둥(column)의 중심축 온도는 Haddad & Farmer(1984)의 실험데이터와 비교하였고, 양극으로의 에너지 플럭스 및 온도분포 데이터는 Bini 등(2006)의 실험 및 해석데이터와 비교하여 만족스런 일치를 확인하였다.

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.5 no.3
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• pp.92-98
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• 2006

In this study, the behavior characteristics of a hydrostatic thrust bearing used in hydraulic equipment was analyzed using a commercial finite element program, ADINA. The solid domain was modeled with the fluid domain simultaneously to solve the fully coupled problem, because this is a problem where a fully coupled analysis is needed in order to model the fluid-structure interaction(FSI). The results such as bearing deformation, stress, film thickness and lifting bearing force were obtained through FSI analysis, and then they were compared with the results calculated from the classical method, a single step sequential analysis. It was found that the result difference between two analyses was increased according to the injection pressure. Therefore, in case of high pressure loading, it is desirable to conduct the FSI analysis to examine the deformation characteristics of a hydrostatic slipper bearing.

• 유체기계공업학회:학술대회논문집
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• 1999.12a
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• pp.163-169
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• 1999

The numerical procedure has been developed for simulating incompressible viscous flow around a turbine stage with rotor-stator interaction. This study solves 2-D unsteady incompressible Navier-Stokes equations on a non-orthogonal curvilinear coordinate system. The Marker-and-Cell concept is applied to efficiently solve continuity equation. To impose an accurate boundary condition, O-H multiblocked grid system is generated. O-type grid and H-type grid is generated near and outer rotor-stator The cubic-spline interpolation is applied to handle a relative motion of a rotor to the stator. Turbulent flows have been modeled by the Baldwin- Lomax turbulent model. To validate present procedure, the time averaged pressure coefficients around the rotor and stator are compared with experiment and a good agreement obtained.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05c
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• pp.176-181
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• 1996

중수로 원자로에서 핵심 구조물인 압력관은 합금이 사용되고 있는데, 고온, 고압의 방사선 분위기에서 사용되기 때문에 가동중 변형을 받는다. 따라서 본 연구에서는 압력관의 건전성 평가기술을 확보하기 위하여 Zr-2.5wt.% Nb 압력관의 집합조직과 온도 변화에 따른 강도 특성을 조사하였다. 집합조직의 변화는 시편의 채취방향을 달리하여 네 가지의 집합조직 변화를 주었으며, 이들 시편에 대해 상온에서 부터 45$0^{\circ}C$까지 온도를 변화시가면서 인장시험을 실시하였다. 온도가 증가함에 따라 시편의 집합조직과 관계없이 네 종류의 시편 모두가 30$0^{\circ}C$까지는 강도가 직선적으로 감소하는 현상을 보이며, 30$0^{\circ}C$에서 37$0^{\circ}C$ 사이의 온도에서 강도가 약간 증가하는 현상을 보였다. 또한 37$0^{\circ}C$이상의 온도에서는 강도가 다시 직선적으로 감소하는 경향을 나타냈다. 이 같은 현상은 30$0^{\circ}C$ 까지는 프리즘 슬림(-slip)으로 전위가 움직이다가 30$0^{\circ}C$ 이상의 온도에서부터 37$0^{\circ}C$까지는 피라미드 슬림(-slip)계의 경쟁 상호작용에 의한 추가적인 응력이 필요하여 나타난 현상이라 사료된다. 온도의 변화에 따른 강도와 연신율의 curve에서 30$0^{\circ}C$와 37$0^{\circ}C$의 범위에서 plateaus region과 연신율이 최소값을 갖는 것은 동적변형시효(dynamic strain ageing)현상과 관련이 있는 것으로 생각되나 추가적인 연구가 필요하다. 집합도가 변함에 따라 인장강도는 T(transverse)>L(longitudinal)> 30。> 45 。순으로 나타났으며 이는 slip과 twin의 복합적인 작용에 의한 것으로 해석된다.

• Journal of the Korean Chemical Society
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• v.26 no.5
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• pp.296-303
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• 1982

The solubilities of 1-phenyl-2-acetamido-3-butanone were measured in $H_2O$ at 20, 30 and 40$^{\circ}$C at pressure from 1 to 4500 kg/$cm^2$. Pressure going up to 4500 kg/$cm^2$, the solubility in $H_2O$decreases consistantly as that of diketopiperazine does. As diketopiperazine is a model compound of peptide bond and 1-phenyl-2-acetamido-3-butanone has only one peptide bond and a pretty large hydrophobic group, the solubility behavior is quite surprising. Volume change and heat capacity change data are reasonable.

• Journal of the Korean Society of Propulsion Engineers
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• v.6 no.1
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• pp.71-82
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• 2002

A time-iterative compressible Navier-Stokes code is developed to analyze the flowfield of a two-dimensional ejector nozzle system. A parametric study has been made for two controlling parameters, duct to nozzle area ratio and nozzle pressure ratio. Results show that there is an optimum area ratio for an efficient pumping of secondary flow. At high area ratios, a freestream flow directly passes through the mixing duct without giving adequate pumping. While at low area ratios, jet boundary is acting as a blockage to incoming flow. The nozzle pressure ratio variation shows that the pumping rate increases as the pressure ratio increases provided there is no interaction between the shroud wall and the shock cell structure.

• Journal of the Korea Computer Graphics Society
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• v.20 no.4
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• pp.9-16
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• 2014

This paper proposes a novel method that couples fluid and deformation/fracture. Our method considers two interaction types: fluid-object interaction and fluid-fluid interaction. In fluid-fluid interaction, we simulate water and smoke separately and blend their velocities in the intersecting region depend on their densities. Our method separates projection process into two steps for each of water and smoke. This reduces the number of grid cells required for projection in order to optimize the number of iterations for convergence and improve stability of the simulation. In water projection step, smoke region regarded as the cells with Dirichlet boundary condition. The smoke projection step solves water region with Neumann boundary condition. To take care of fluid-object interaction, we make use of the fluid pressure to update velocities of the each of the mass points so that the object can deform or fracture. Although our method doesn't provide physically accurate results, the various examples show that our method generate appealing visuals with good performance.

• Applied Chemistry for Engineering
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• v.10 no.3
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• pp.456-460
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• 1999

The YHB radial distribution functions of a linear gas molecule CO were calculated by a computer within the Stockmayer molecular potential molel, which assumed thc CO molecule as a simple dipolar molecule. To examine the validity of the obtained YHB radial distribution of CO gas molecule, the density dependent pressures of CO at several temperatures were also calculated. The calculated pressures showed a good agreement with literially known experimental CO pressure data. The temperatures examined were 273, 298, and 373 K and the densities were up to $0.013/{\AA}^3$ (maximum pressure = 1000 atm). Since the calculated pressures showed a good agreement with the experimental values, the obtained YHB radial distribution functions of CO molecule seemed good enough to obtain and predict various equilibrium physical and chemical quantities of CO molecule sensitive to density such as pressure. It was also found that in CO gas system the dipole-dipole interaction is effective up to approximately 2.5 molecular diameter.

• Journal of the Korea Society of Computer and Information
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• v.25 no.3
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• pp.155-162
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• 2020

Among the fourth industrial revolution technologies, products related to healthcare using IoT and sensors are currently being developed. We design and develop an interaction system based on user standing posture recognition using multi-channel large area pressure sensors in this paper. To this end, first of all we investigate major sensor markets of the sensor industry and review technology trends and the current and future of smart healthcare. Based on this survey, we examine and compare cases developed at home and abroad for multi-channel large-area pressure sensors, which are key components of the system that we want to develop. We recognize the standing posture status of the user through the developed system and experiment with how effective it is actually in user posture calibration and apply the research results to various healthcare devices' medical fields based on this.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.3
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• pp.37-45
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• 2002

The vortex flow and aerodynamic load characteristics of a $65^{\circ}$ sweep delta wing with the leading edge extension in sideslip condition is investigated experimentally. The freestream velocity is 40 m/sec, which corresponds to a Reynolds number per meter of $1.76{\times}10^6$ based on the wing root chord. The angles of attack range from $12^{\circ}$ to $28^{\circ}$, and the sideslip angles treated are $0^{\circ}$ , $-10^{\circ}$, $-20^{\circ}$. The LEX vortex of the leeward side. The LEX and wing vortics coalesce to to become a concentrated strong vortex or to break down at down at downstream position. Due to the interation of the LEX and wing vortices, a high suction pressure is maintained on the windward wing surface, and a low suction pressure is formed on the leeward wing surface