• Transactions of the Korean Society of Automotive Engineers
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• v.2 no.1
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• pp.38-50
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• 1994

To improve the efficiency of internal combustion engines, it is necessary to understand mixed air-fuel in-cylinder flow processes accurately at intake and compression strokes. There is experimental and numerical methods to analyse in-cylinder flow process. In numerical method, standard $k-{\varepsilon}$ model with wall function was mostly adopted in in-cylinder flow process. But this type model was not efficiently predicted in the near wall region. Therefore in the present study, low Reynolds number $k-{\varepsilon}$ model was adopted near the cylinder wall and standard $k-{\varepsilon}$ model in other region. Also QUICK scheme was used for convective difference scheme. This study takes axisymmetric reciprocating model engine motored at 200rpm with a centrally located valve, incorporated 60 degree seat angie, and flat piston surface excluding inlet port. Because in-cylinder flow processes are undergoing unsteady and compressible, averaged cylinder pressure and inlet velocity at arbitrary crank angle are determined from thermodynamic analytic method and incylinder states at that crank angle are iteratively determined from the numerical analytic method.

• Journal of the Korean Society of Marine Environment & Safety
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• v.15 no.2
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• pp.151-156
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• 2009

This experimental study investigated in to the flow characteristics around staggered cooling tube arrays of fan coil unit for ship. A particle image velocimetry technique was employed to obtain detailed measurements at inlet-velocity-based Reynolds numbers of $Re=1.5{\times}10^3{\sim}Re=2.5{\times}10^3$. As for the results, the flow evolves rapidly and becomes spatially periodic in the streamwise direction after a relatively short distance. The flow exhibits strong Reynolds number dependence in developing region but no significant Reynolds number effects are observed in spatially periodic region.

• Proceedings of the Korea Water Resources Association Conference
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• 2004.05b
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• pp.404-408
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• 2004

인공순환수로 실험구간에 반구구조물을 설치하지 않은 경우와 설치할 경우의 흐름특성을 분석하기 위하여 수치모의를 수행하였다. 수치모의는 FLUNET가 제공하는 RNG $k-\varepsilon$ 모형과 Reynolds Stress 모형을 사용하였으며 음파유속계(ADV)를 이용하여 측정한 결과와 비교분석 하였다. 수치모의와 실험결과의 상관성을 분석한 길과, RNG $k-\varepsilon$과 Reynolds Stress 모형의 계산결과와 실측값의 상관계수는 반구구조물을 설치하지 않은 경우 0.60 - 0.63, 반구구조물을 설치한 경우 0.75 - 0.78로 큰 차이가 없었다. 그러나 계산반복회수의 경우 RNG $k-\varepsilon$ 모형이 Reynolds Stress 모형에 비하여 2 - 5배 정도 빠르다. 두 모형의 걸과가 크게 차이가 나지 않으므로 순환수로 내의 흐름특성을 분석하기 위한 모형으로 수렴속도가 빠른 RNG $k-\varepsilon$ 모형을 선정하였다. 수치모의 결과와 "흐름 메카니즘에 의한 깔따구의 분포(I)- 실험"의 깔따구 분포경향을 비교한 결과 깔따구는 전반적으로 유속과 난류강도가 작은 곳에 분포하였으며 실험구간에 반구구조물이 있는 경우에는 구조물의 상${\cdot}$하류에 깔따구가 분포하였다. 이차류 또한 깔따구의 분포에 영향을 미친다. 향후 흐름특성에 따른 저서생물의 분포경향을 분석을 위하여 전산유체역학의 기법들을 적용하면 깔따구 등의 저서성 대형무척추 동물의 분포와 흐름특성의 관계를 저렴한 비용으로 분석할 수 있을 것이다.

• Journal of Advanced Marine Engineering and Technology
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• v.33 no.8
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• pp.1180-1186
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• 2009

This experimental study is about the flow characteristics according to existence and nonexistence of the control rod and location in the flow field where it has the Inclined rear walls in the open cavity. By using the visualization of flow and particle image velocimetry (PIV), we performed about a change and speed of the Reynolds number. Our objective was what part of the control rod gives less effects to the characteristics of flow and how the shear mixing layer moves at what critical point of the Reynolds number. As a result, we differed the location of control rod. So finally, L/H=0.2 was discovered to give less effects to the cavity. The flow of backside of vortex faces the upper side. And we found that this phenomenon shows up more clear when the number of Reynolds increases. This is because of the flow of vortex causes by the condition of y/H=1.0. This phenomenon gets more clear with increasing of number of Reynolds, and critical point of the Reynolds number was $Re=1.0{\times}10^4$ around. If control rod is L/H=0.1, depending on the number of Reynolds ($Re=6.0{\times}10^3$, $Re=8.0{\times}10^3$, $Re=1.0{\times}10^4$, $Re=1.2{\times}10^4$), doubled vortex shows up. As the shear mixing layer of the upper side of cavity increases, the speed of the lower side was very stable.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.26 no.5B
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• pp.469-479
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• 2006

In order to investigate characteristics of the primary flow and the secondary currents in meandering channels, the laboratory experiments were conducted in S-curved channels with angle of bend, $150^{\circ}$, and sinuosity of 1.52. The experimental conditions was decided varying average depth and velocity. Under these experimental conditions, spatial variations of the secondary currents in multiple bends were observed. The experimental results revealed that the distribution of primary flow in straight section is symmetric without respect to the experimental condition and the maximum velocity line of the primary flow occurs along the shortest path in experimental channel, supporting the result of previous works. The secondary currents in second bend became more developed than those in first bend. Particularly, the outer bank cell developed distinctively and the secondary current intensity was low at the straight section and high at the bends, periodically. Also, the secondary current intensity at the bends was as twice to three times as that at the straight section, and has its maximum value at the second bend. The turbulent flow characteristics of meandering channel was investigated with turbulent intensity of the primary flow and Reynolds shear stress. It was observed that the turbulent intensity is increasing when the velocity deviation of the primary flow is large whereas Reynolds shear stress increases when both the velocity deviation of the primary flow and the secondary current are large.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.40 no.7
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• pp.435-440
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• 2016

Effects of the increase rate of Reynold number on near-wall turbulent structures are investigated by performing direct numerical simulations of transient turbulent channel flows. The simulations were started with the fully-developed turbulent channel flow at $Re_{\tau}=180$, then temporal accelerations were applied. During the acceleration, the Reynolds number, based on the channel width and the bulk mean velocity, increased almost linearly from 5600 to 13600. To elucidate the effects of flow acceleration rates on near-wall turbulence, a wide range of durations for acceleration were selected. Various turbulent statistics and instantaneous flow fields revealed that the rapid increase of flow rate invoked bypass-transition like phenomena in the transient flow. By contrast, the flow evolved progressively and the bypass transition did not clearly occur during mild flow acceleration. The present study suggests that the transition to the new turbulent regime in transient channel flow is mainly affected by the flow acceleration rate, not by the ratio of the final and initial Reynolds numbers.

• Journal of Power System Engineering
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• v.13 no.4
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• pp.24-30
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• 2009

본 연구에서는 기존에 널리 사용되어져 온 Wavier-Stokes 방정식을 풀이하는 전통적인 CFD 해석에서 벗어나 최근에 그 응용 분야를 넓혀가고 있는 LBM의 해석코드를 개발하고, 이를 이용하여 이차원 채널속에 놓여진 쇄기형 물체 주위의 유동특성을 조사하였다. D2Q9 격자계 및 Bhatnagar-Gross-Krook (LBGK) 모델을 채택하였으며, 수치해석 결과는 기존의 실험결과의 잘 일치하였다. 쇄기형 물체에서 와의 형성 및 방출 Reynolds 수 범위는 $32{\leq}Re{\leq}620$ 이며, 원형실린더에서 알려진 Karman 와열을 형성하는 주기적인 와방출은 대칭적인 와가 형성된 후 $Re{\geq}85$부터 시작되며 Reynolds 수의 증가에 따라 와 방출 주파수는 증가되었다.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.3 no.5
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• pp.395-403
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• 1991

The purpose of this investigation was to characterize nucleate boiling and burn-out heat flux for rectangular free jet with saturated water impinging perpendicularly and upward against a flat uniform heat flux surface. Heat flux measured for Reynolds number based on rectangular nozzle width and for aspect ratio. The result of nucleate boiling heat transfer was presented nondimensional experimental equation including Nusselt, Boiling, Subcooling, Reynolds and Weber number. The effect of aspect ratio of heated surface in the burn-out heat flux had not appeared distinctly. But for the same aspect ratio, burn-out heat flux increased linearly with increment of nozzle exit velocity.

• Transactions of the Korean Society of Mechanical Engineers
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• v.15 no.5
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• pp.1717-1726
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• 1991

본 연구에서는 낮은 레이놀즈수 영역에도 적용될 수 있는 레이놀즈응력모델의 개발을 위해, 우선 벽근처 영역에서 사용되는 실험식(벽법칙)을 Hassid와 Poreh에 의 해 개발된 1-방정식모델로 대체하고 이를 레이놀즈응력모델과 접속시키는 방식을 사용 하였다. Hassid-Poreh의 1-방정식모델은 이미 Gibson등에 의해 그 성능이 평가되어 압력구배가 크지 않은 경계층유동의 낮은 레이놀즈수 영역에서 매우 좋은 결과를 보여 줌이 밝혀졌다. 본 연구에서는 곡면위의 난류경계층에 대해 위에서 설명한 바 있는 난류모델을 적용함에 있어 Gillis등과 Gibson등에 의해 실험된, 각각 곡률이 큰 경우 와 작은 경우의 대표적인 유동을 선택하여 모델의 성능을 시험하였다. 1-방정식모델 내에 포함된 길이차원(length scale)에 대해서는 곡률을 고려한 수정이 이루어졌다.

• Proceedings of the Korea Water Resources Association Conference
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• 2019.05a
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• pp.93-93
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• 2019

식생이 있는 개수로 흐름의 분석이 중요한 이유는 식생이 흐름 특성과 유사이송 및 하상변동에 영향을 주어 복잡한 흐름 현상을 만들어 내기 때문이다. 식생 밀도, 식생 길이, 식생이 식재된 형태에 따라 흐름의 현상이 달라지며, 흐름 특성의 변화로 인해 하상 및 주변 하천구조물에 영향을 줄 수 있다. 하천의 식생은 대부분 폭과 길이가 제한된 모습으로 존재하는 경우가 많으며, 식생이 존재하는 영역에서는 식생항력에 의해 유속이 감소하고 식생이 없는 영역에서 유속이 증가한다. 식생항력에 의해 변화된 흐름 특성은 일정 거리를 지나면 평형상태에 도달하게 되며, 식생의 경계면에서는 전단층이 발달하여 모멘텀의 교환이 활발하게 발생하는 현상을 보인다. 식생 흐름의 특성을 분석하기 위해 수치모형으로는 식생 흐름의 강한 비등방성을 모의할 수 있는 비등방성 수치모형이 적합하다. 본 연구에서는 부분 식생이 식재된 개수로에서 RSM (Reynolds stress model)을 이용하여 식생과 식생 주변의 흐름 특성 및 난류량을 분석하였다. 흐름의 변화에 따라 크게 3 구간으로 나누어 흐름 특성을 파악할 수 있으며, 식생의 밀도와 식생 영역의 폭의 길이에 따라 각 구간의 길이가 달라지는 것을 확인하였다.