• 대한기계학회논문집B
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• 제38권7호
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• pp.607-618
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• 2014

초임계 $CO_2$의 수직상향유동에서의 난류열전달에 관한 실험적연구가 내경 4.5 mm의 원형관에서 수행되었다. 실험범위는 유체평균온도 $29-115^{\circ}C$, 압력 74.6 - 102.6 bar, 국부 벽면 열유속 $38-234kW/m^2$ 그리고 질량유속 $208-874kg/m^2s$였다. 중간정도의 벽면 열유속 및 낮은 질량유속에서 벽면온도는 확연한 최대점을 나타냈다. 열전달에 대한 부력 및 유동가속의 영향을 살펴보기 위하여 실험 및 참조상관식(Kranoshchekov and Protopopov)에서 획득된 Nusselt 수의 비를 부력 및 유동가속을 나타내는 변수인 $Bo^*$ 및 $q^+$를 이용하여 분석하였다. 이 분석을 통해 유동가속 변수인 $q^+$는 실험에서의 열전달 현상을 적절히 표현할 수 있는 변수라는 것을 확인할 수 있었다. 마지막으로 초임계 유체의 수직상향 유동에서의 새로운 열전달 상관식이 개발되었으며, 이 상관식은 ${\pm}30%$의 오차범위에서 실험데이터를 잘 예측하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.789-794
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• 2000

The Paper studies the flow and heat transfer characteristics to a jet impinging at different oblique angles, to a plane surface by numerical methods. The flowfield and heat transfer rate associated with the oblique Impingement of an axisymmetric jet are of interest as a result of its presence in numerous technological Problems. For the computation of heat transfer rate, the standard ${\kappa}-{\varepsilon}$ and ${\kappa}-{\varepsilon}-\bar {{\upsilon}'^ 2}$ turbulent model were adapted. The accuracy of the numerical calculations was compared with various experimental data reported in the literature. ${\kappa}-{\varepsilon}-\bar {{\upsilon}'^ 2}$ model showed better agreement with experimental data than standard ${\kappa}-{\varepsilon}$ model in prediction of the turbulent intensity and the heat transfer rate. In the case of computation of flowfield, the study carries on the ${\alpha}=45$ deg, h/D=4.95. The jet Reynolds number based on the nozzle diameter(D), was 48,000. For the computation of heat transfer rate, the Re=20,000, the jet orifice-to-plate spacings(L/D) are 4, 6 and 10, and the angle between the axis of the jet orifice and the plate surface is set at 30, 45, 60, or 90 deg. For the smaller spacings, the near-peak Nusselt numbers are not significantly effected by the initial decreases in the Jet angle. The overall shape of the local Nusselt number x-axis profile is influenced by both the jet orifice-to-plate spacing and the jet angle.

• 한국유체기계학회 논문집
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• 제11권6호
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• pp.24-30
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• 2008

In order to enhance the heat/mass transfer, a turbulator has been installed at the exit of injection hole for the impingement/effusion cooling system. The local heat/mass transfer coefficients have been obtained by a naphthalene sublimation method. Experiments have been carried out at the fixed jet Reynolds number of 10,000. Two turbulators with different diameter have been used in the current study. The result presents that the turbulator leads to the increase in flow mixing and jet velocity, consequently enhancing the heat/mass transfer at a stagnation region. Further, the stagnation region is divided into four small areas with peak value. In the existence of initial crossflow, the stagnation regions move downstream and low heat/mass transfer regions are formed regardless of the installation of turbulator. However, the increased jet velocity by turbulator reduces the crossflow effect against the jet, resulting in decrease of low heat/mass transfer regions. Compared to the case without turbulator, the installation of turbulator yields $5{\sim}10%$ augmentation in averaged Sh value.

• 대한기계학회논문집B
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• 제24권2호
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• pp.195-203
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• 2000

The local heat/mass transfer coefficients for arrays of impinging circular air jets on a plane surface are determined by means of the naphthalene sublimation method. Fluid from the spent jets is constrained to flow out of the system in one direction. Therefore, the spent fluid makes a crossflow in the confined space. The present study investigates effects of jet-orifice-plate to impingement-surface spacing and jet Reynolds number. The spanwise- and overall-averaged heat/mass transfer coefficients are obtained by numerical integrating the local heat transfer coefficients. The local maximum heat/mass transfer coefficients move further in the downstream direction due to the increase of crossflow velocity. At the mid-way between adjacent jets, the heat/mass transfer coefficients have a small peak owing to the collision of the adjacent wall jets and are affected strongly by the crossflow. The effect of the crossflow occurs strongly at the small orifice-to-impingement surface distance.

• 대한기계학회논문집B
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• 제22권3호
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• pp.386-398
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• 1998

The present experiment is conducted to investigate heat transfer characteristics on the impinging surface with secondary flows around circular nozzle jets. The changed vortex pattern around jet affects significantly the flow characteristics and heat transfer coefficients on the impinging surface. The effects of the jet vortex control are also considered with jet nozzle-to-plate distances and main jet velocities. The vortex pattern around a jet is changed from a convective instability to an absolute instability with a velocity suction ratio of the main jet and the secondary counterflow. With the absolute instability condition, the jet potential core length increases and the heat transfer on the impinging surface is increased by small scale eddies. The region of high heat transfer coefficients is enlarged with the high Reynolds number due to increasing secondary peak values. The effect of suction flows is influenced largely with collars attached the exit of the jet nozzle because the attached collar guides well the counterflow around the main jet.

• 대한기계학회논문집B
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• 제39권2호
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• pp.119-124
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• 2015

반도체 생산에 사용되는 액체용 극소 질량유량계측기의 새로운 설계 안에 대하여 수치해석적으로 연구하였다. 내경 0.3mm 정도인 원관 외부에 히터선을 일정 폭 권선하고, 히터로부터 일정거리 떨어진 후류에 온도계측용 써미스터선을 권선하는 형상이다. 히터에 단일펄스 가열을 하면 일정시간 경과 후 써미스터가 최고온도를 겪는다. 최고온도까지 걸리는 시간은 질량유량과 거의 반비례하며, 이를 이용하여 질량유량을 계측할 수 있다. 관벽을 통한 전도열전달과 액체유동에 의한 대류열전달이 복합적으로 작용하므로 관내유동의 평균속도와 관벽을 통한 최고온도의 이동속도는 큰 차이를 나타내며, 상호 비선형적인 특성을 보인다. 본 연구에서는 센서관의 내 외경, 히터의 권선폭 및 히터와 써미스터 사이의 거리를 설계변수로 고려하여 수치해석적으로 제안한 설계사항을 분석하였으며, 설계인자의 최적화에 대한 검토를 수행하였다.

• 한국연소학회지
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• 제10권1호
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• pp.20-26
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• 2005

In the present study, catalytic combustion of hydrogen-air premixture in a millimeter scale monolith coated with Pt catalyst was investigated. As the combustor size decreases, the heat loss increases in proportion with the inverse of the scale of combustion chamber and combustion efficiency decreases in a conventional type of combustor. Combustion reaction assisted by catalyst can reduce the heat loss by decreasing the reaction temperature at which catalytic conversion takes place. Another advantage of catalytic combustion is that ignition is not required. Platinum was coated by incipient wetness method on a millimeter scale monolith with cell size of $1{\times}1mm$. Using this monolith as the core of the reaction chamber, temperatures were recorded at various locations along the flow direction. Burnt gas was passed to a gas chromatography system to measure the hydrogen content after the reaction. The measurements were made at various volume flow rate of the fuel-air premixture. The gas chromatography results showed the reaction was complete at all the test conditions and the reacting species penetrated the laminar boundary layer at the honeycomb and made contact with the catalyst coated surface. At all the measuring locations, the record showed monotonous increase of temperature during the measurement duration. And the temperature profile showed that the peak temperature is reached at the point nearest to the gas inlet and decreasing temperature along the flow direction.

• Journal of Advanced Marine Engineering and Technology
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• 제35권4호
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• pp.421-428
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• 2011

최근 지구 온난화와 더불어 급격한 기후 변화 등으로 여름철 주간 냉방 수요가 급격히 증가하여 이에 따른 전력 수요량이 증가하고 있다. 또한 주간 전력 피크로 인한 급격한 전력부하 상승은 전력 수급의 불균형을 가져 와 사회적 문제로 대두되고 있다. 이를 위해 개발된 축냉시스템은 전력사용량이 상대적으로 적은 심야시간에 냉열을 만들어 탱크에 저장해 두었다가 그것을 주간 냉방 전력 사용 피크시간에 이용함으로써, 냉동기의 용량이 작아지고 냉동기를 고효율로 운전할 수 있으며, 갑작스런 부하 증가에 적절히 대응할 수 있는 등 여러 가지 장점을 갖고 있다. 이로 인하여 주간전력 피크를 줄여주는 효과를 가진다. 축냉시스템 중 하나인 슬러리아이스형은 슬러리아이스가 과냉되지 않은 작은 입자형태를 갖고 있어 해빙특성이 뛰어나므로 부하변동에 빠르게 반응할 수 있으며, 그 저장과 재생 및 수송 분야에서 그 장점과 기능이 입증되었다. 본 실험에서는 슬러리아이스 생성 효율을 높이기 위하여 역전유동층을 이용하였다. 이러한 역전유동층은 냉각관 표면에 얼음 부착이 심화되기 전에 얼음 입자를 분리시켜 수 내지 수십 미크론 단위(0.1~0.001 mm)의 슬러리아이스를 생성하도록 하였다.

• Nuclear Engineering and Technology
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• 제33권2호
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• pp.241-253
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• 2001

Under severe accidents, the pressure and temperature response has an important role for the integrity of a nuclear power plant containment. The history of the pressure and temperature is characterized by the amount and state of steam/air mixture in a containment. Recently, the heat transfer rate to the structure surface is supposed to be increased by the wavy interface formed on condensate film. However, in the calculation by using CONTAIN code, the condensation heat transfer on a containment wall is calculated by assuming the smooth interface and has a tendency to be underestimated for safety. In order to obtain the best- estimate heat transfer calculation, we investigated the condensation heat transfer model in CONTAIN 1.2 code and adopted the new forced convection correlation which is considering wavy interface. By using the film tracking model in CONTAIN 1.2 code, the condensate film is treated to consider the effect of wavy interface. And also, it was carried out to investigate the effect of the different cell modelings - 5-cell and 10-cell modeling - for KNGR(Korean Next Generation Reactor) containment phenomena during a severe accident. The effect of wavy interface on condensate film appears to cause the decrease of peak temperature and pressure response . In order to obtain more adequate results, the proper cell modeling was required to consider the proper flow of steam/air mixture.

• 한국대기환경학회지
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• 제12권4호
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• pp.479-485
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• 1996

Volatile organic compounds are air pollutants exhausting from industrial process, evaporation of solvent, and so on. Most of VOCs are the combustible gas of low calorific value as it is diluted by air. The systems burning such a hazardous gas need to increase enthalpy in order to increase flame stability. In this study an incinerator with reciprocating flow in the honeycomb ceramic has been used for the experiment of VOCs control. By the reciprocating flow system, the enthalpy of combustion gas is effectively regenerated into the enthalpy increases of the combustible gas through the honeycomb ceramic, which provides a heat storage. The position of the reaction zone is strongly dependent on the parameters of mixture velocity and time frequency. Flame front is changed to the point where burning velocity is coincided with burning velocity in the honeycomb ceramic. In this system it is important that flame front should be located symmetrically at the center of honeycomb ceramic for the purpose of increasing the reaction rate at one point. Peak temperature becomes higher with decreasing time frequency, at which the flow direction is regularly reversed.