• 해양환경안전학회:학술대회논문집
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• 해양환경안전학회 2005년도 추계학술대회지
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• pp.159-163
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• 2005

채널 내부의 비정상 흐름을 규명하기 위하여 실제 사용 중인 판형 열교환기 모델을 대상으로 가시화 실험과 입자영상유속계(PIV)를 사용한 계측을 수행하였다. 실험은 기복을 가지고 있는 채널의 높이와 내부유동의 부분 평균속도벡터에 따른 7가지 종류의 레이놀즈수를 적용하였고, 순간속도벡터분포와 유동특성을 고찰하였다. 실험에서 삼각형상 그루브 채널은 하부 채널과 채널 흐름에 의해서 받고 있는 전단응력의 그루브 흐름과의 관계에서 복합적인 흐름의 형태로 나타났다. 삼각형상 그루브와 채널 사이의 경계인 전단혼합층은 채널에서 난류강도가 상승하는 주흐름에 영향을 미쳤다.

• 해양환경안전학회:학술대회논문집
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• 해양환경안전학회 2005년도 추계학술대회지
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• pp.153-158
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• 2005

표면에 부착된 수직벽 후방의 난류전단흐름을 입자영상유속계를 이용하여 조사하였다. 하부 틈새를 갖는 수직벽 후류영역에서는 박리 후 비정상적인(unsteady) 재순환 영역이 형성되었으며, 약 x=3H위치에서 전단층의 재부착 및 난류경계층으로의 재발달 과정이 나타났다. 수직벽 직전의 오목한(concave) 유선곡률과 수직벽 후방의 볼록한(convex)유선곡률의 영향은 수직벽 주위에서 가장 크게 나타나고, 하류로 나아감에 따라 전단층 주위 유체의 유입 등으로 그 영향이 박리 전단층 내에서 커다란 와구조가 연속적으로 발생하였다.

• Ocean and Polar Research
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• 제26권2호
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• pp.145-154
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• 2004

Surface energy and $CO_2$ fluxes have been measured over an ocean at Ieodo Ocean Research Station of KORDI since May 2003. Eddy covariance technique, which is a direct flux measurement, is used to quantitatively understand the interaction between the ocean surface and the atmospheric boundary layer. Although fluxes were continuously measured during the period from May 2003 to February 2004, the quality control of these data yielded <20% of data retrieval. The atmospheric stability did not show any distinct dirunal patterns and remained near-neutral to stable from May to June but mostly unstable during fall and winter in 2003. Sensible heat flux showed a good correlation with the difference between the sea water temperature and the air temperature. The maximum fluxes of sensible heat and latent heat were $120Wm^{-2}$ and $350Wm^{-2}$ respectively, with an averaged Bowen ratio of 0.2. The ocean around the tower absorbed $CO_2$ from the atmosphere and the uptake rates showed seasonal variations. Based our preliminary results, the daytime $CO_2$ flux was steady with an average of $-0.1 mgCO_2m^{-2}s^{-1}$ in summer and increased in winter. The nighttime $CO_2$ uptake was greater and fluctuating, reaching up to $-0.1 mgCO_2m^{-2}s^{-1}$ but these data require further examination due to weak turbulent mixing at nighttime. The magnitude of $CO_2$ flux was positively correlated with the half hourly changes in horizontal mean wind speed. Due to the paucity of quality data, further data collection is needed for more detailed analyses and interpretation.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.397-400
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• 2006

In this study, we experimentally investigate the possibility of skin-friction drag reduction by series of transverse cavities in a turbulent boundary layer flow. The effects of cavity depth (d), cavity length (l) and cavity spacing (s) on the skin friction drag are examined in the range of $Re_{\theta}\;=\;4030\;{\sim}\;7360$, $d/{\theta}_0\;=\;0.13\;{\sim}1.03$, l/d = 1 ~ 4 and s/d = 5 ~ 20. We perform experiments for twenty different cavity geometries and directly measure total drag force using in-house force measurement system. In most cases, the skin friction drag is increased. At several cases, however, small drag reduction is obtained. The variation of the skin ftiction drag is more sensitive to the cavity length than to the cavity depth or cavity spacing, and drag is reduced at $s/l\;{\geq}\;10$ and $l/{\theta}_0\;{\leq}\;0.26$ irrespective of the cavity depth. At $l/\bar{\theta}_0\;=\;0.13$ and s/l = 10, maximum 2% drag reduction is achieved. When the skin friction drag is reduced, there is little interaction between the flows inside and outside cavity, and the flow changed by the cavity is rapidly recovered at the following crest. A stable vortex is formed inside a cavity in the case of drag reduction. This vortex generates negative skin friction drag at the cavity bottom wall. Although there is form drag due to the cavity itself, total drag is reduced due to the negative skin friction drag.

• 한국공간구조학회논문집
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• 제13권3호
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• pp.83-90
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• 2013

A series of wind tunnel tests were conducted on 7 super-tall buildings with various polygon cross-sections, including triangle, square, pentagon, hexagon, octagon, dodecagon, and circular. The primary purpose of the present study is to investigate the effect of increasing number of sides on aerodynamic characteristics for super-tall buildings. Wind tunnel tests were conducted under the turbulent boundary layers whose power-law exponent is 0.27. Fluctuating wind pressures from more than 200 pressure taps were recorded simultaneously, and time series of overturning moments were calculated considering tributary area of each pressure tap. The results show that the overturning moment coefficients and the spectral values decrease with increasing number of sides, and the largest mean and fluctuating overturning moments were found for the triangular super-tall building, and the largest spectral values were found for the square super-tall building. The analysis should be conducted more in detail, but currently it can be roughly said that there seems to be a little differences in the aerodynamic characteristics for the super-tall buildings whose number of sides is larger than 5 or 6.

• 한국전산유체공학회지
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• 제18권3호
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• pp.8-13
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• 2013

Drag reduction of a running vehicle is very important issue for the energy savings and emission reduction of its power train. Especially for a solar powered electric vehicle, the drag reduction and weight lightening are two serious problems to be solved to extend its driving distance under the given energy condition. In this study, the ground effect of an airfoil shaped road vehicle was studied for an optimum body design of an ultra-light solar powered electric vehicle. Clark-Y airfoil type was adopted to the body shape of the model vehicle to reduce aerodynamic drag. From the study, it was found that the drag of the model vehicle was reduced as the height(h) between ground and the lower surface of the model vehicle was decreased. It is due to the reduction of the down-wash decreasing the induced drag of the vehicle. The lift was also decreased as the height decreased. It is due to the turbulent boundary layer developed beneath the vehicle body. The drag is classified into two types; the form and friction drag. The fraction of form drag to friction one is 76 to 24 on the model vehicle. As the height(h) of the model vehicle from the ground surface increases the form drag also increases but the friction drag is in reverse.

• 한국주조공학회지
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• 제12권3호
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• pp.220-229
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• 1992

The degree of purification and the macrostructure of high purity aluminium were studied through the alternate stirring method in order to improve the nonuniformity of solute concentration in the unidirectional stirring method. The $2^3$ factorial design was done to examine the effects of experimental factors more qualitatively. In the relatively low stirring speed of 1500 rpm with alternate stirring mode, the uniform solute profile and refined grain structure were obtained due to strong washing effect and turbulent fluid flow. It was induced by the transition of the momentum boundary layer by alternation of the stirrer. It was concluded from this study that the alternate stirring mode was more effective to obtain the uniformity of solute even in the stirring speed of 1500 rpm. But the degree of purification decreased below the critical alternating period. When 2N(99.8wt.%) aluminium was used as the starting material the morphology of solid-liquid showed the cellular shape and the columnar grains were inclined to the direction of rotation. This inclined grain growth resulted from the difference of relative velocities of solid and liquid. The inclined angle was increased as the stirring speed increased and solidification proceeded. In the case of 4N aluminium, there was no inclined grain growth and it was confirmed from the macrostructure and SEM work that the morphology of solid-liquid interface was planar. From the factorial design, it was found that the alternate stirring mode showed poorer purification effect than that of unidirectional stirring mode at low speed(500 rpm). In addition, the factor that had the most significant effect on the degree of purification was the stirring speed.

• Journal of Advanced Marine Engineering and Technology
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• 제38권6호
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• pp.615-624
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• 2014

핀-튜브 열교환기는 산업용 보일러, 라디에이터, 냉동기 등에 많이 사용되고 있어 열교환기의 성능향상을 위한 다양한 연구가 진행되고 있다. 본 연구에서는 Plain형 핀-튜브 열교환기에 대해 가로피치, 와류발생기위치, 튜브표면의 돌기형상 및 돌기개수 등의 변화에 따른 열전달 및 압력강하 특성을 이론적으로 해석하였다. CFD 해석시 경계조건으로는 SST 난류모델을 적용하였으며, 튜브표면의 온도는 333 K이고, 입구측 공기의 온도와 속도는 423~438 K, 1.5~2.1 m/s로 가정하였다. 해석결과로는 열전달계수는 가로피치에 대한 영향은 큰 차이가 없으며, 열전달특성은 와류발생기 설치가 튜브 전방부에 위치할수록 양호한 것으로 나타났다. 또한 튜브표면의 돌기형상은 열전달 및 압력강하 특성에서 원형이 톱니형과 삼각형보다 적절하였으며, 16개 원형 돌기형상이 가장 양호하였다.

• 대한토목학회논문집
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• 제13권3호
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• pp.193-206
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• 1993

쇄파대(碎波帶)에서 undertow에 관한 해석적(解釋的) 모형(模型)을 제시(提示)하였다. 유도(誘導)된 기초방정식(基礎方程式)의 각 항(項)은 크기 비교(比較)로 평가(評價)되었으며, 이에 따라 난류법선응력(亂流法線應力)와 streaming velocity 항(項)이 무시(無視)될 수 있었다. undertow의 기동력(起動力)이 되는 파종성분(波動成分)의 각 항(項)은 Chebyshev 4차(次) 다항식(多項式)으로 근사(近似)한 파형(波形)으로 산정(算定)하였다. 그리고 과동점성계수(過動點性係數)의 연직분포(鉛直分布)를 3가지 형태(形熊)의 함수(凾數)로 가정(假定)하였으며, 과동점성계수(過動點性係數)의 상수(常數)는 새로운 경계조건(境界條件)을 도입(導入)하여 결정(決定)하였다. 그 결과(結果), undertow의 해(解)를 구하는데 필요한 인력(入力) 매개변수(媒介變數)가 간단화(簡單化) 되었다. 여러가지 수리실험자료(水理實驗資料)와 본(本) 모형(模型)의 해(解)를 비교(比較)한 결과(結果), 저면경사(底面傾斜)가 완만(緩慢)할수록 그리고 과동점성계수(過動點性係數)의 연직분포(鉛直分布)를 선형함수(線形凾數)로 가정(假定)하였을 때 좋은 결과(結果)를 나타내었다.

• 한국강구조학회 논문집
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• 제21권3호
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• pp.245-255
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• 2009

산업용 건축물은 일반적으로 박공지붕형 저층의 형태로 많이 건설된다. 본 연구는 박공지붕형 저층건물의 풍압분포와 특성을 알아보기 위하여 풍동실험을 수행하였다. 풍동실험은 경사각 변화에 따른 외장재용 피크외압계수 분포양상을 알아보기 위하여 동일한 폭과 높이, 길이를 가지지만 지붕 경사각이 서로 다른 7가지의 모형을 제작하여 실험하였다. 실험결과 지붕과 벽면의 모서리 부분에서 최대 피크외압계수가 나타났으며, 이를 KBC-2005 및 각국의 기준과 비교하여 보았다. 실험에 의한 피크외압계수는 AIJ-2004와 매우 유사하게 나타났지만 KBC -2005보다는 다소 크게 나타났다.