• 한국자동차공학회논문집
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• 제2권1호
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• pp.26-37
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• 1994

In this study, flow of a model intake port/valve system is analyzed by using low Reynolds number $k-{\varepsilon}$ model. Discharge coefficient was obtained from computational results for the various cases of valve lifts. Discharge coefficient becomes maximum when the valve lift is 20mm, and does not increase or decrease in proportional to valve lift. Most of pressure drop and production of turbulent kinetic energy occur at the edge points of the valve and the valve seat Thus, in order to improve discharge coefficient, rounding of edge points in valve and valve seat is recommended. As valve lift is increased, the velocity of the intake jet in the valve passage decreases, and the direction of the jet is more inclined toward the valve seat.

• 항공우주시스템공학회지
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• 제2권4호
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• pp.7-12
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• 2008

Averaged heat transfer coefficients were measured in a turbine blade internal cooling passage model with three blockage walls. Each blockage wall was equipped with 9 staggered holes or slots in order to create different shaper of repeated jet impingement. The effect of jet shape on the averaged heat transfer coefficient was studied by the copper-thermocouple method and three Reynolds number of 10,000, 20,000, and 30,000 were tested. Results showed that the repeated stagger jets could increase the averaged heat transfer coefficient by at least 9 times compared to the smooth channel cases. Due to the large pressure drop induced by the repeated jet impingement, the thermal performance was less than 1 for all cases and decreased as the Reynolds number increased. Among the tested cases, the widest slot showed the best thermal performance. The measurement results showed that the thermal performance of the heat transfer augmentation by repeated stagger jets could be improved by altering the jet shape, and other shape of impingement jet will be studied in near future.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2008년도 하계학술발표대회 논문집
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• pp.436-439
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• 2008

This paper is to research the heat transfer performance of the sintered pipe. Recently, oil prices is to be 127 $ per barrel, we expect higher costs this summer. We promote alternative fuels, after oil and gasoline prices reached record highs. The governments have made efforts to avoid future crisis by continuing the move toward renewable energy and energy saving. In this paper, we have fabricated a sintered pipe, the heat transfer performance of sintered pipe is achieved experimentally. The pipe is copper tube of outer diameter of 15.88 mm, the length of the pipe is 800 mm. Based on the experimental results, it is shown the overall heat transfer coefficient of sintered pipe is increased as compared with that of a straight pipe, is equal as compared with that of a spiral pipe. The overall heat transfer coefficient was $0.075{\sim}0.09\;kW/^{\circ}C$

• 설비공학논문집
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• 제16권11호
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• pp.1044-1050
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• 2004

The present study has been conducted to develop a heat pipe heat exchanger for middle-high temperature ranged from 300 to $600^{\circ}C$. Heat transfer rate, overall heat transfer coefficient and temperature effectiveness were investigated using a heat pipe heat exchanger with Dowtherm A as working fluid. Theoretical analysis was also conducted, and the followings were obtained: (1) Heat exchange rate increased as waste gas temperature supplied to evaporator and frontal velocity in condenser increased, (2) Overall heat transfer coefficient increased by $3{\sim}7\%$ as frontal velocity in evaporator and condenser increased, (3) Temperature effectiveness was about $30\%$ in evaporator and was about $40\%$ in condenser, (4) Heat recovery rate was about $38\%$, (5) Pressure drop did not exceed $8\;mmH_{2}O$ under the running condition of $1{\sim}3Nm/s$, (6) Simulation results were corresponded with experimental results.

• 청정기술
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• 제13권2호
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• pp.151-158
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• 2007

프레온계 냉매의 지구온난화와 오존층파괴 문제로 인해 대체냉매로서 R-410A가 주목을 받고 있다. 이러한 대체냉매를 세관에 적용시킬 경우 효율을 향상시킬 뿐만 아니라 지구환경에 미치는 영향을 감소시키고, 대기를 청정하게 만드는 기술 및 방안으로 각광 받고 있다. 따라서 본 연구에서는 R-22의 대체냉매로 각광받고 있는 R-410A의 세관응축기 내에서의 응축열전달 특성에 대해 실험적으로 고찰하고자 하였다. 실험장치는 유동양식, 열전달, 압력강하 특성을 파악할 수 있도록 제작되었고, 주요 구성품은 냉매펌프, 증발기, 응축기(시험부), 사이트 글라스(가시화부), 압력탭, 측정장치 등이다. 시험부의 내관은 내경 3.36 mm와 5.35 mm인 수평평활 동관이다. 실험변수들의 범위로서 질량유속 $200{\sim}500\;kg/m^2s$이고, 열유속은 $1.0{\sim}2.4\;kW$이다. R-410A의 응축열전달 계수가 R-22에 비해 최대 5% 정도 높은 것을 알 수 있었다. 세관 내 R-410A와 R-22의 유동양식은 환상류 영역이 지배적으로 나타남을 관찰하였고, 건도가 0.2 이하인 영역에서는 성층류가 나타남을 확인할 수 있었다. 내경 3.36 mm의 압력강하가 내경 5.35 mm에 비해 $30{\sim}50%$정도 높았다. 종래의 응축 열전달 상관식과 실험데이터를 비교한 결과, Fujii의 상관식과 최대 40%이내에서 일치하였다.

• Journal of Biosystems Engineering
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• 제24권6호
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• pp.513-522
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• 1999

This study was performed to get the optimal operating conditions of an water-air compact heat pump system using R-134a. The experiments was done for three elvels of the air mass flow rate and the compressor driving speed during air-heating process. The temperature of the air at the condenser inlet and outlet was 17~23$^{\circ}C$, 36~44$^{\circ}C$, respectively. The average temperature of the refrigerant at the evaporator and condenser was 1$0^{\circ}C$, 6$0^{\circ}C$, respectively. The temperature of the refrigerant was not depending on the air mass flow rate and the compressor driving speed. The pressure of the refrigerant at the condenser inlet and outlet was ranged of 10~18.5kg/$\textrm{cm}^2$ and that at the evaporator was ranged of 3.1~3.3kg/$\textrm{cm}^2$. The pressure drop at the condenser and evaporator was about 1.5, 1.2 kg/$\textrm{cm}^2$, respectively. The performance of coefficient for air heating was about 3.3~4.0.

• 대한기계학회논문집B
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• 제25권12호
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• pp.1748-1755
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• 2001

The shell and tube heat exchangers were introduced to apply to a big capacity condenser and a high pressure feed water heater for power plant in the beginning of 1990s. Design and manufacturing technology fur shell and tube heat exchangers have been developed until now. But it is very difficult to calculate the expected performance characteristics of the shell and tube heat exchanger, because there are many design parameters to be considered according to internal structure and the shell side heat transfer mechanism complicately related to the design parameters. Design parameters to be considered in the design stage of shell and tube heat exchanger are shell and tube side fluids, flow rate, inlet and outlet temperature, physical properties, type of heat exchanger, outer diameter, thickness, length of tube, tube arrangement, tube pitch, permissive pressure loss on both sides, type of baffle plate, baffle cutting ratio. The propose of study is an analysis TEMA(Tubular Exchanger Manufacturers Association) E shell and tube heat exchanger performance with changing a number of baffles(3, 5, 7, 9, 11) and tubes(16, 20) and determined optimal baffle spacing.

• 한국해양공학회지
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• 제2권2호
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• pp.130-137
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• 1988

This thesis introduced that character of a treatment technique for a mading synthetic resin Hifiow-Ring. The material system of packings make an experiment air$NH_{3}$/air$H_{2}SO_{4}$, $SO_{2}$-air/NaOH, $NH_{3}$-air/$/H_{2}SO_{4}$ under general conditions. Lattices packing compared with conventional packings was proved low pressure loss and high separation efficiency for high loading per trans unit. And an inflow materal tested for absorption and rectification, it made an experiment under a range regular temperature, low energy and small amount of money. That made possible in simple equation, volume material tranfer coefficient$\beta_{L}$ . a by absorption or $\beta_{V}$ .a calculated in all range loading. The peculiarity pressure loss $\Delta\;P/NUT_{ov}$ for Hiflow-ring contributed to a fall cost of energy, a grade number of a vacuum rectification and absorption calculation.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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• pp.173-176
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• 2010

75톤급 가스발생기 기술검증시제에서 나타난 산화제 분사기 차압의 증가 원인을 파악하기 위하여 축소형 가스발생기를 설계, 제작하였다. 설계점 및 탈설계점 시험 조건을 포함한 총 6회의 연소시험을 성공적으로 수행하였다. 연소시험 결과 연소압을 고정한 후 혼합비를 증가시킨 경우 연료 및 산화제 유량계수는 일정한 것으로 나타났으며, 혼합비를 고정한 후 연소압을 증가시킨 경우에도 연료 및 산화제 유량계수는 변함이 없는 것으로 파악되었다.

• 한국산학기술학회논문지
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• 제16권7호
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• pp.4364-4374
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• 2015

본 연구에서는 복합 전열 촉진 핀 열교환기의 열전달 및 압력손실에 대하여 실험적으로 검토하였다. 비교를 위하여 널리 사용되는 루버 핀 열교환기에 대한 실험도 수행하였다. 핀 피치(1.5mm~1.7mm)와 열수(1열~3열)를 변화시키며 열전달 및 압력손실에 미치는 영향을 검토하였다. 실험범위에서 핀 피치가 j와 f 인자에 미치는 영향은 크지 않았다. 열수가 증가하면 j 인자는 감소하고 f 인자는 열수와 무관하였다. 루버 핀의 j와 f 인자가 복합 전열 촉진 핀의 값들보다 크게 나타났다. 1열의 경우 평균 j 인자와 f 인자는 23%, 27% 크고, 2열에서는 11%, 8%, 3열에서는 10%, 9% 크게 나타났다. 하지만 동일 압력 손실 대비 전열 성능은 복합 전열 촉진 핀 열교환기가 1열에서 6.4%, 2열에서 11.1%, 3열에서 13.6% 크게 나타났다. 기존 루버 핀 상관식은 j 인자를 과대 예측하고 f 인자를 과소 예측하였다.