• Journal of Advanced Marine Engineering and Technology
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• 제33권6호
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• pp.912-917
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• 2009

An experimental flow visualization study of the entrance section of channels formed with wavy plates was made. The experiments were conducted in a water channel and a laser illuminated particle tracking was used as the technique of flow visualization. The flow region that were found in the experiments are steady, unsteady and significantly-mixed flows. Instabilities of the flow first appear near the exit of the channel. As the Reynolds number increases, the flows are characterized by the appearance of flow separation and the growth of recirculation region.

• Journal of Astronomy and Space Sciences
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• 제36권1호
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• pp.1-9
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• 2019

In this paper we present analysis of current density when the Cluster spacecraft pass the nightside auroral region at about $4-5R_E$ from the center of Earth. The analysis is made when the inter-spacecraft separation is within 200 km, which allows all four spacecraft to be situated inside the same current sheet. On 22 February 2002, two field-aligned current (FAC) events were observed in both the southern and the northern hemispheres. The FACs were calculated with magnetic field data obtained by the four spacecraft using the Curlometer method. The scales of the FACs along the spacecraft trajectory and the magnitudes were hundreds of kilometers and tens of $nA/m^2$, respectively, and both events were mapped to the auroral region in the ionosphere. We also examined reliability of the results with some parameters, and found that our results are adequately comparable with other studies. Nevertheless, some limitations that decrease the accuracy of current estimation exist.

• 한국유체기계학회 논문집
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• 제17권5호
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• pp.27-36
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• 2014

This paper presents a numerical investigation of the effect of the rotation speed on the performance in a transonic axial compressor with the dihedral stator. Four stator geometries with different stacking line variables were tested in the flow simulations over the whole operating range. It was found that a large shroud loss at the rotor outlet and the subsequent shroud corner separation in the stator passage occurred at low mass flow rate with the 100 % design speed. The hub dihedral stator could suppress the shroud loss region and consequently improve the stall margin. In case of the 70 % design speed condition as the mass flow rate decreased, it was seen that the high loss region was placed at the midspan of the rotor passage. The dihedral stator slightly affected the local diffusion factor, but the performance of the compressor was not changed.

• 한국철도학회논문집
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• 제9권6호
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• pp.772-777
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• 2006

Three-dimensional numerical study is performed for the flow analysis around the rolling stock with square cross section (Mugungwha train model). The height (H) of rolling stock is considered as the characteristic length and the total length of rolling stock is 40 which correspond to 1/2 unit of rolling stock. The gap between the surface and rolling stock is 0.17H which is average value. The relative velocity between the surface and rolling stock is assumed to be zero and Re=10,000 based on the characteristic length. Low Re ${\kappa}-{\epsilon}$[15] is employed for the calculation of turbulence which resolve all the way to the solid surface (laminar sub-layer). Large flow separation occurred at the front head of train and a pair of vortex is generated on both top and side of rolling stock. The behavior of vortices on the top of the rolling stock is believed to affect the performance of the pantograph which should be intensively investigated. The difference between the high pressure in the front stagnation region of train and the low pressure in the rear separated region causes a large pressure drag. A large pair or vortex are generated in the rear of train and the size of vortex is increased more than the size of cross section of train.

• 한국가시화정보학회지
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• 제13권3호
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• pp.29-34
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• 2015

The interaction between a normal shock wave and a boundary layer along a wall surface in internal compressible flows causes a very complicated flow. This interaction region containing shock train and mixing region is called as pseudo-shock waves. Pseudo-shock waves in the divergent part of a rectangular nozzle have been investigated by using large-eddy simulation (LES). LES studies have been done for the complex flow phenomena of three-dimensional pseudo-shock waves. The LES results have been validated against experimental wall-pressure measurements. The LES results are in good agreement with experimental results. Pseudo-shock length and corner separation have been studied in three-dimensional LES model. Comparison of centerline pressure measurement and 3D visualization measurement has been discussed for the corner separation position. It has been concluded that the pseudo-shock length should be measured by using 3D visualization measurement.

• Journal of Power Electronics
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• 제8권4호
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• pp.301-308
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• 2008

This paper proposes a method of improving the stability in sensor-less control of permanent magnet synchronous motors. The control method for low-speed region is divided into two: One is a high frequency method, which involves a problem of reverse rotation once misdetection of the permanent magnet polarity should occur, and another one is a current drive method, which has a problem that phase and speed oscillations are caused by quick speed changes. Hence, authors propose adoption of the current drive method for the basic control system with added compensation of stabilization by means of the high frequency method. This combination secures stable control with no risk of reversal and less vibration. In addition, authors have also considered a frequency separation filter of a shorter delay time so that current control performance will not lower even when high frequencies are introduced. This filter has achieved simplified compensation using repetitive characteristic through the utilization of the periodicity of high frequency current. Simulation and experiment have been conducted to verify that the stable performance of this system is improved.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 춘계학술대회논문집
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• pp.140-146
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• 2002

The fluid induced vibration (FIV) phenomena of a 2-D.O.F airfoil system have been investigated in low Reynolds number incompressible flow region. Unsteady flows with viscosity are computed using two-dimensional incompressible Navier-stokes code. To validate developed Navier-Stokes code, steady and unsteady flow fields around airfoil are analyzed. The present fluid/structure interaction analysis is based on the most accurate computational approach with computational fluid dynamics (CSD) and computational structural dynamics (CSD) techniques. The highly nonlinear fluid/structure interaction phenomena due to severe flow separations have been analyzed fur the low Reynolds region (R$_{N}$ =500~5000) that has a dominancy of flow viscosity. The effect of R$_{N}$ on the fluid/structure coupled vibration instability of 2-DOF airfoil system is presented and the effect of initial angle of attack on the dynamic instability are also shown.own.

• 반도체디스플레이기술학회지
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• 제5권3호
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• pp.29-32
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• 2006

Because of new requirements related to the employment of SMT(Surface Mounting Technology) manufacturing and the diversity of components on high density PCB(Printed Circuit Boards), Thermal control of the reflow process is required in order to achieve acceptable yields and reliability of SMT assemblies. Accurate control of the temperature distribution during the reflow process is one of the major requirements, especially in lead-free assembly. This study has been performed for reflow process using the commercial CFD(Computational Fluid Dynamics) tool for predicting flow and temperature distributions. Porous plate was installed to prevent leakage flow which was one of the major problem of temperature uniformity in the reflow process. There is a separation region where the flow is turned. Outside wall made of porous plate is to prevent and minimize separation region for acquiring uniform temperature during operation. This paper provided design concept from CFD results of the steady state temperature distribution and flow field inside a reflow oven.

• 대한전자공학회논문지SP
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• 제42권4호
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• pp.49-59
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• 2005

본 논문에서는 측색적인 오차와 낟알 무의 현상을 동시에 감소시키기 위해 추가적인 잉크와 정량적인 낟알 무의 측정자를 이용한 6색 분리 방법을 제안한다. 기존의 6색 분리 방법에서는 3색이나 4색 프린터에서 나타나는 도트의 가시성을 줄이기 위해 밝은 영역에서 사용되는 묽은 잉크(light magenta와 light cyan)를 진한 잉크(magenta와 cym)로 대체한다. 그러나 묽은 잉크와 진한 잉크의 색상의 차이로 인해서 밝은 영역에서 정확한 측색적인 색 재현이 어렵게 되었다. 이러한 측색적인 오차를 줄이기 위해 추가적인 잉크(additional colorants)인 yellow와 light magenta 잉크를 밝은 영역에서 사용한다. 따라서 밝은 영역에서 magenta 잉크는 light magenta와 yellow로 대체되고 cyan은 light cyan과 light magenta로 대체된다. 이러한 추가적인 잉크의 사용은 진한 잉크의 색상과 유사한 색을 만들 수 있기 때문에 측색적인 오차를 줄일 수 있게 된다. 또한 추가적인 잉크는 작은 도트의 가시성을 갖고 있기 때문에 부드러운 영상도 재현될 수 있다. 한편 중간 영역에서도 부드러운 영상을 획득하기 위해 magenta는 light magenta와 magenta로 대체되고 cyan은 light cyan과 cyan으로 대체된다 그러나 농도가 다른 두 잉크의 사용은 거친 도트 패턴을 생성하게 된다. 이러한 현상을 반영하기 위해 정량적인 낟알 무의 측정자가 사용된다. 어두운 영역에서는 묽은 잉크를 사용해도 더 이상 낟알 무늬가 감소되지 않기 때문에 magenta와 cyan 잉크만 사용한다.

• 한국터널지하공간학회 논문집
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• 제11권2호
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• pp.175-188
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• 2009

도심지 등 지역적인 여전에 의하여 기존의 지하 공동 또는 터널에 근접하여 발파를 이용한 새로운 터널을 굴착할 경우, 새로운 터널의 굴착으로 인하여 지반이 이완되고 따라서 기존 지하 공동의 안정성에 문제가 발생할 수 있다. 이러한 가존 지하 공동의 안정성에 문제를 발생시킬 수 있는 가장 큰 요소로는 기존 지하 공동과 신설 터널의 이격거리가 될 수 또한 신설 터널 굴착으로 인한 소성영역의 발생에 따른 지반 이완을 문제 심을 수 있다. 따라서 본 연구에서는 기존 광역 상수관과 신설 터널의 이격거리에 따른 기존 광역 상수관의 안정성을 평가하기 위하여 이격거라가 다른 여섯 가지 모델에 대해 석고를 이용힌 2차원 축소 모형실험을 실시하였다. 실험 결과는 터널 굴착과정과 파괴 단계에서 발생된 변위 벡터와 균열양상으로 표현하였다. 터널 굴착과정 중 발생하는 변위를 분석하면, 터널과 광역 상수관의 간격이 상수관 직경의 2.5배 (2.5D)까지는 이격거리가 증가함에 따라 감소하는 경향을 보인다. 그러나 중심 간격이 2.5D를 넘으면 추가변위는 발생하지 않았다.