• 한국방재학회 논문집
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• 제9권2호
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• pp.53-57
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• 2009

개수로에서 발생하게 되는 분류흐름에는 많은 특성들이 나타나게 된다. 특히, 지류부의 내측 벽면을 따라서 이차류 흐름이 나타나 토사나 오염물 등의 퇴적물 침전을 일으키는 분리구역이 발생하게 된다. 분류흐름에서 발생하는 분리구역의 특성을 연구하기 위해 상류흐름에서의 자유수면 및 유속을 계산할 수 있는 이차원 천수방정식 수치모델인 RMA2를 이용하였다. 수치모의 결과는 Hsu 등(2002)의 실험결과와 비교하여 잘 일치함을 알 수 있었다. 수치모의를 통해 유량비에 대한 분리구역의 크기 관계를 제시할 수 있었다. 그리고 분리구역의 크기를 줄이기 위해 본류와 지류가 만나는 모서리 지점을 곡선과 대각선으로 연결하여 유수흐름을 완만하게 만든 지형들을 제안하였다.

• Wind and Structures
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• 제5권1호
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• pp.25-48
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• 2002

Wind flow and pressure on the roof of the Texas Tech Experimental Building are studied along with the incident wind in an effort to understand the wind-structure interaction and the mechanisms of roof pressure generation. Two distinct flow phenomena, cornering vortices and separation bubble, are investigated. It is found for the cornering vortices that the incident wind angle that favors formation of strong vortices is bounded in a range of approximately 50 degrees symmetrical about the roof-corner bisector. Peak pressures on the roof corner are produced by wind gusts approaching at wind angles conducive to strong vortex formation. A simple analytical model is established to predict fluctuating pressure coefficients on the leading roof corner from the knowledge of the mean pressure coefficients and the incident wind. For the separation bubble situation, the mean structure of the separation bubble is established. The role of incident wind turbulence in pressure-generation mechanisms for the two flow phenomena is better understood.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 춘계학술대회 논문집
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• pp.315-319
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• 2009

Investigation of the lateral force fluctuations in an axisymmetric overexpanded compressed truncated perfect (CTP) nozzle for the shutdown transient is presented. These nozzles experience side-loads during start-up and shut-down operations, because of the flow separation at nozzle walls. Two types of flow separations such as free shock separation (FSS) and restricted shock separation (RSS) shock structure occur. A two-dimensional unsteady numerical simulation has been carried out over an axisymmetric CTP nozzle to simulate the lateral force fluctuations in nozzle during shutdown process. Reynolds Averaged Navier-Stokes equations are numerically solved using a fully implicit finite volume scheme. Governing equations are solved by coupled implicit scheme. Two equation k-$\omega$ SST turbulence model is selected. Unsteady pressure is measured at four locations along the nozzle wall. Present pressure variation compared well with the experimental data. During shutdown transient, separation pattern varies from FSS to RSS and finally returns to FSS. Several pressure peaks are observed during the RSS separation pattern. These pressure peaks generate lateral force or side loads in rocket nozzle.

• 대한화학회지
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• 제38권9호
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• pp.660-666
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• 1994

이웃하는 란탄족 원소의 분리에서 온도와 흐름속도의 영향을 치환크로마토그래피로 연구하였다. 일렬로 연결된 두 컬럼에 Amberlite 120 양이온 교환수지를 채워서 충전용과 분리용으로 나누어 사용하였다. 보유이온은 $H^+$을, 흐름용액은 0.012M과 0.015M의 EDTA 용액을 사용하였다. 실험중에는 관의 온도를 90$^{\circ}C$로 유지하였으며 이온교환수지 관 속에 생기는 기포를 줄이기 위해 일정한 압력을 걸었다. 용출액은 ICP-AES로 직접 분석하였다. 이 실험에서 란탄족 원소쌍 La: Ce, Ce :Pr, Pr: Nd에 대한 분리인자는 각각 4.6, 2.8, 1.9이었으며 이것은 25$^{\circ}C$에서 이론적으로 얻은 것보다 큰 값이다. 흐름속도를 2.5 ml/min에서 1.5 ml/min로 줄이면 이론단해당높이(HETP)도 1.60 cm에서 0.88 cm로 줄었다. 따라서 용리액의 흐름속도를 줄이고 온도를 높이므로써 분리효율을 증가시킬 수 있었다. 이 실험에서 99.9% 이상의 순수 란탄족 원소에 대한 회수율은 49∼77%이었다.

• 한국추진공학회지
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• 제17권1호
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• pp.61-69
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• 2013

핀틀 움직임에 의해 발생되는 큰 유동박리에 대해 적합한 2-방정식 난류모델의 압축성계수 보정모델을 판단하기 위하여 수치적 연구를 수행하였다. 난류모델은 저 레이놀즈수 k-${\varepsilon}$ 모델과 k-${\omega}$ SST 모델에 압축성 보정 모델(Wilcox와 Sarkar 모델)을 적용하여, 핀틀 노즐의 세부유동장을 관찰하고 노즐 벽면에서의 압력을 실험데이터와 비교 분석하였다. 마하디스크(Mach disk)의 위치와 박리영역에서의 압력 회복 형태는 난류모델에 따라 다르게 나타났으며, 각 난류모델에 압축성 보정을 적용하여 유동 박리 포획의 정확도를 개선하였다. 압축성이 보정된 k-${\varepsilon}$ 모델이 실험결과와 매우 잘 일치하였다.

• 한국자동차공학회논문집
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• 제16권5호
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• pp.22-28
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• 2008

A closed type crankcase ventilation system has been adopted to engines to prevent emission of blow-by gas to atmosphere. In the early closed type crankcase ventilation system, blow-by gas which contains engine lubricating oil is re-circulated into the intake system. The blow-by gas containing oil mist leads to increased harmful emissions and engine problems. To reduce loss of the engine oil, a highly-efficient oil separation device is required. Principle of a cyclone oil separator is to utilize centrifugal force in the separator and, therefore, oil separator designs depend on rotational flow which causes the centrifugal force. In this paper, flow characteristics and oil separation performances for cyclone type designs are calculated with CFD methodology. In the CFD model, oil particle was injected on a inlet surface with Rosin-Rammler distribution and uniform distribution. The major design parameters considered in the analysis model are inlet area, cone length and outlet depth of the oil separator. As results, reducing inlet area and increasing cone length increase oil separation performance. Changes in outlet depth could avoid interference between rotational flow and outlet flow in the cyclone oil separator.

• 대한조선학회논문집
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• 제49권6호
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• pp.512-520
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• 2012

In this study, the numerical analysis for the flows around an axial cylinder is carried out in order to investigate the basic characteristics of drag of blunt body. A variation of drag and flow separation for the axial cylinder is investigated according to the length-diameter ratio. Also, the flow separation around the head is removed by rounding-off the front edge of the body to analyze the effect of drag reduction. Most of the drag turns out to be a pressure drag component and the variation of drag is caused by the change of pressure and velocity which is affected strongly by the flow separation at the edges of the axial cylinder. Especially, it is found that the pressure drag component acting on the back of axial cylinder, as known as the base drag, mainly changes the drag. As the length-diameter ratio of axial cylinder increases, the drag sharply decreases and the minimum is shown when the length-diameter ratio is about 2.4. Also, as the length-diameter ratio increases further above 2.4, the drag increases at a slower rate. The pressure drag is almost constant when the length-diameter ratio is greater than 8, but the increase of friction drag component is the reason for the increase of the drag. When flow separation is removed completely at the front edge of the axial cylinder, the pressure drag component is reduced to 12~17%, but the total drag is reduced to only 17%~32% due to the friction drag component that increases linearly proportional to the length-diameter ratio.

• JSTS:Journal of Semiconductor Technology and Science
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• 제7권3호
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• pp.140-150
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• 2007

A simple, label-free microfluidic cell purification method is presented for separation of cancer cells by exploiting difference in cell adhesion. To maximize the adhesion difference, three types of polymeric nanostructures (50nm pillars, 50nm perpendicular and 50nm parallel lines with respect to the direction of flow) were fabricated using UV-assisted capillary moulding and included inside a polydimethylsiloxane (PDMS) microfluidic channel bonded onto glass substrate. The adhesion force of human breast epithelial cells (MCF10A) and human breast carcinoma (MCF7) was measured independently by injecting each cell line into the microfluidic device followed by culture for a period of time (e.g., one, two, and three hours). Then, the cells bound to the floor of a microfluidic channel were detached by increasing the flow rate of medium in a stepwise fashion. It was found that the adhesion force of MCF10A was always higher than that of MCF cells regardless of culture time and surface nanotopography at all flow rates, resulting in a label-free detection and separation of cancer cells. For the cell types used in our study, the optimum separation was found for 2 hours culture on 50nm parallel line pattern followed by flow-induced detachment at a flow rate of $300{\mu}l/min$.

• Bulletin of the Korean Chemical Society
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• 제32권4호
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• pp.1315-1320
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• 2011

Whey protein (WP) is a mixture of proteins, and is of high nutritional values. WP has become an important source of functional ingredients in various health-promoting foods. In this study, size-exclusion chromatography (SEC) and asymmetrical flow field-flow fractionation (AsFlFFF) were used for separation and analysis of whey proteins. It was found that a lab-prepared WP from raw milk is mostly of ${\beta}$-lactoglobulin with small amount of higher molecular weight components, while a commercial whey protein isolate (WPI) powder contains relatively larger amount of components other than ${\beta}$-lactoglobulin, including IgG and protein aggregates. Results suggest that AsFlFFF provides higher resolution for the major whey proteins than SEC in their normal operation conditions. AsFlFFF could differentiate the BSA and Albumin, despite a small difference in their molecular weights, and also was able to separate much smaller amount of aggregates from monomers. It is noted that SEC was able to show the presence of low molecular weight components other than the major whey proteins in the WP samples, which AsFlFFF could not show, probably due to the partial loss of those low molecular weight species through the membrane.

• Advances in aircraft and spacecraft science
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• 제9권2호
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• pp.131-148
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• 2022

The paper presents the surface-modified NACA 2412 airfoil performance with variable cavity characteristics such as size, shape and orientation, by numerically investigated with the pre-validation study. The study attempts to improve the airfoil aerodynamic performance at 30 m/s with a variable angle of attack (AOA) ranging from 0° to 20° under Reynolds number (R_e) 4.4×10⁵. Through passive surface control techniques, a boundary layer control strategy has been enhanced to improve flow performance. An intense background survey has been carried out over the modifier orientation, shape, and numbers to differentiate the sub-critical and post-critical flow regimes. The wall-bounded flows along with its governing equations are investigated using Reynolds Average Navier Strokes (RANS) solver coupled with one-equational transport Spalart Allmaras model. It was observed that the aerodynamic efficiency of cavity airfoil had been improved by enhancing maximum lift to drag ratio ((l/d) max) with delayed flow separation by keeping the flow attached beyond 0.25C even at a higher angle of attack. Detailed investigation on the cavity distribution pattern reveals that cavity depth and width are essential in degrading the early flow separation characteristics. In this study, overall general performance comparison, all the cavity airfoil models have delayed stalling compared to the original airfoil.