• 동력기계공학회지
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• 제22권6호
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• pp.28-35
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• 2018

The large-eddy simulation (LES) was carried out to evaluate the instantaneous vector and vorticity profiles of a small-size axial fan (SSAF) at the operating point of full-flowrate. The downstream flow of the SSAF exhibits a shorter axial flow when not fully developed, especially the stronger vortex appears at the edge near the flow end. On the other hand, the downstream flow of the SSAF exhibits a longer axial flow, and the weaker vortex appears at the edge near the flow end when the flow is sufficiently developed. Moreover, in the downstream of the SSAF, a periodic and intermittent flow pattern appears at the edge showing the axial flow, and the instantaneous vorticity contour lines showing the form of a circle group are distributed at specific intervals from the downstream region of the blade tip, which is considered to be the result of the intermittency phenomenon influenced by the number of blades and the number of revolutions.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.2890-2895
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• 2007

Heat transfer on two identical nearby circular cylinders immersed in the uniform cross flow at Re = 100 and Pr = 7.0 was numerically studied. We consider all possible arrangements of the two circular cylinders in terms of the distance between the two cylinders and the inclination angle with respect to the direction of the main flow. It turns out that significant changes in the characteristics of heat transfer are noticed depending on how the two circular cylinders are positioned, resulting in quantitative changes of heat transfer coefficients on both cylinders. Collecting all the numerical results obtained, we propose a contour diagram for averaged Nusselt number for each of the two cylinders. The perfect geometrical symmetry implied in the flow configuration allows one to use those diagrams to estimate heat transfer rates on two identical circular cylinders arbitrarily positioned in physical space with respect to the main flow direction.

• 한국전산유체공학회지
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• 제13권2호
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• pp.42-47
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• 2008

Heat transfer on two identical nearby circular cylinders immersed in the uniform cross flow at Re=120 and Pr=0.7 was numerically studied. We consider all possible types of arrangements of the two circular cylinders in terms of the distance between the two cylinders and the inclination angle with respect to the direction of the main flow. It turns out that significant changes in the characteristics of heat transfer are noticed depending on how the two circular cylinders are positioned, resulting in quantitative changes of heat transfer coefficients on both cylinders. Collecting all the numerical results obtained, we propose a contour diagram for averaged Nusselt number for each of the two cylinders. The perfect geometrical symmetry implied in the flow configuration allows one to use those diagrams to estimate heat transfer rates on two identical circular cylinders arbitrarily positioned in physical space with respect to the main flow direction.

• International Journal of Aeronautical and Space Sciences
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• 제3권2호
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• pp.67-75
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• 2002

In the course of missile system design, jet plume impingement is encountered in designing airframe as well as launchers, requiring careful investigation of its effect on the system. In the present paper, recent works on such topic are presented to demonstrate usefulness of CFD results in helping design the hardware. The jet impinging flow structure exhibits such complex nature as shock shell, plate shock and Mach disk depending on the flow parameters. The main parameters are the ratio of the jet pressure to the ambient pressure and the distance between the nozzle and the wall. In the current application, the nozzle contour and the pressure ratio are held fixed, but the jet impinging distance is varied to illuminate the characteristics of the jet plume with the distance. The same methodology is then applied to a complex vertical launcher system (VLS), capturing its flow structure and major design parameter. These applications involving jets are thus hoped to demonstrate the usefulness and value of CFD in designing a complex structure in the real engineering environment.

• 한국항해항만학회지
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• 제29권6호
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• pp.523-528
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• 2005

장애물이 있는 배관속의 점성유동을 다양한 난류모형을 적용하여 해석하였다. 적용한 난류모형은 k-$\epsilon$, k-$\omega$, Spalart-Allmaras, Reynolds stress 이고, 배관내의 격자는 구조격자(structured grid) 이다. 속도벡터, 압력분포 반복계산(iteration)에 의한 잔류치(residual), 양정(dynamic head) 등을 모사하였다. 4개의 난류모형을 배관유동에 적용하였고 상용 프로그램을 사용하여 해석을 수행하였다.

• Spatial Information Research
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• 제8권1호
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• pp.131-140
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• 2000

하천의 흐름해석 분야에서는 모형이 요구하는 입·출력 자료의 구성이 복잡할 뿐만 아니라 흐름의 공간적 분포특성 도시가 매우 중요하지만 지금까지 체계적인 자료관리가 이루어지지 않은 실정이다. 본 연구에서는 등고, 하천, 표고, 경계 및 하도단면 등으로 구성된 국가지리정보시스템과 연계된 데이터베이스를 구축하는 방법과 등간격 하도단면 자료를 구축하는 방법을 제안하였다. 연구대상지역은 팔당댐 하류에서 인도교 지점에 이르는 한강구간을 선택하였다. 구축된 데이터베이스는 연구대상지역의 과학적인 하천유량 관리에 유용하게 이용될 것이다.

• Nuclear Engineering and Technology
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• 제30권6호
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• pp.485-495
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• 1998

Migration characteristics of tracers in a rock fracture in a case of line-source and line-collection was studied. The fracture plane was discretized into a square mesh to which variable apertures were assigned. The spatially varying apertures of a fracture were generated using a geostatistical method, based on a given aperture probability density distribution and a specified spatial correlation length. The flow potential and pressure at each node were computed. Calculations showed that fluid flow occurs predominantly through a few preferred paths. Hence, the large range of apertures in the fracture gives rise to flow channeling. The solute transport was calculated using a particle tracking method. The migration plumes of tracer between injection line and withdrawal line are displayed in contour plots. The elution curves are shown to be controlled by the aperture density distribution and to be insensitive to statistical realization and spatial correlation length.

• 디지털융복합연구
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• 제10권6호
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• pp.289-296
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• 2012

우리나라는 지형적, 기후적 특성으로 인해 매년 여름 산사태의 가능성이 크며, 최근 난개발로 인해 이의 발생과 피해가 더욱 커지고 있다. 천안지역은 상대적으로 안전한 지역으로 인식되어 왔으나 산사태의 위험요인이 증가하고 있어 체계적 분석이 필요하다. 본 논문에서는 천안 성거산 주변을 중심으로 등고선 지도를 이용하여 지형의 특징을 추출하고, 이를 이용하여 호우 시 수로와 유역의 면적을 계산하였다. 분석결과 성거산 주변 지역은 수로의 길이와 호우 유입량 관점에서 산사태에 비교적 안정적인 것으로 분석되었으나 일부 국소지역은 계속적 관찰이 필요하다. 한편 등고선 지도는 다른 수치지도 보다 비용 면에서 경제적이므로 1차적 산사태 위험도 분석에 적합하다.

• 한국융합학회논문지
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• 제5권4호
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• pp.75-79
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• 2014

본 연구에서는 자동차 냉각팬에 대해서 유동해석을 수행하였다. 냉각팬의 형상에 대하여 유동 조건은 같게 하여 Canival, Teracan 및 basic 3가지의 모델을 CATIA프로그램으로 설계하여 본 해석을 실시하였다. 날개의 모양에 따라 유체의 속도의 등고선이 변화하는 것을 볼 수 있으며, 날개의 모양 또는 넓이에 따라 각기 다른 압력분포를 볼 수 있었다. 세 가지 모델 중, Teracan 모델인 냉각팬이 공기의 유동이 많아 라디에이터의 열을 식히는데 가장 효율적이 된다고 사료된다. 그리고 디자인 면에서의 융합 기술로의 접목도 가능하여 미적인 감각을 나타낼 수 있다.

• 한국지열·수열에너지학회논문집
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• 제1권1호
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• pp.1-8
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• 2005

Aquifer Thermal Energy Storage (ATES) can be a cost-effective and renewable geothermal energy source, depending on site-specific and thermohydraulic conditions. To design an effective ATES system having the effect of groundwater movement, understanding of thermohydraulic processes is necessary. The heat transfer phenomena for an aquifer heat storage are simulated by using FEFLOW with the scenario of heat pump operation with pumping and waste water reinjection in a two layered confined aquifer model. Temperature distribution of the aquifer model is generated, and hydraulic heads and temperature variations are monitored at the both wells during 365 days. The average groundwater velocities are determined with two hydraulic gradient sets according to boundary conditions, and the effect of groundwater flow are shown at the generated thermal distributions of three different depth slices. The generated temperature contour lines at the hydraulic gradient of 0.001 are shaped circular, and the center is moved less than 5 m to the direction of groundwater flow in 365 days simulation period. However at the hydraulic gradient of 0.01, the contour center of the temperature are moved to the end of east boundary at each slice and the largest movement is at bottom slice. By the analysis of thermal interference data between two wells the efficiency of the heat pump system model is validated, and the variation of heads is monitored at injection, pumping and no operation mode.