• 대한기계학회논문집B
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• 제34권5호
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• pp.515-522
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• 2010

본 연구의 목적은 무착상 조건에서 나선형 원형핀-튜브 열교환기의 형상변수에 따른 열전달특성을 고찰하고 평판 사각핀-튜브 열교환기와 열전달성능을 비교하는 것이다. 나선형 원형핀-튜브 열교환기는 Lfoot 길이 2.7 mm 에서 열전달계수가 최대로 나타났으며, 공기측 열전달계수는 튜브열수가 2 열에서 5 열로 증가하면서 평균 10% 감소하였고 핀피치가 5 mm 에서 10 mm 로 증가하면서 평균 17.5% 증가하였다. 모든 풍량조건에서 나선형 원형핀-튜브 열교환기의 튜브피치 30 mm 가 35 mm 보다 열전달량이 평균 5.1% 높게 나타났고 튜브두께 0.5 mm 가 0.7 mm 보다 열전달량이 평균 4.1% 높게 나타났다. 나선형 원형핀-튜브 열교환기의 열전달계수가 평판 사각핀-튜브 열교환기에 비하여 평균 24.3% 정도 높게 나타났다.

• 한국전자파학회논문지
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• 제15권12호
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• pp.1168-1177
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• 2004

본 논문에서는 전자기적 결합 급전 소형 광대역 디스크-로디드 모노폴 안테나의 사각 디스크에 연결된 단락핀의 수와 배열 간격 등의 변화에 따른 안테나 특성을 연구하고 각각의 단락핀 수에 따른 최적화된 안테나를 설계하였다. 전자기적 결합 급전 소형 모노폴 안테나는 각각 모노폴로 동작하는 단락된 사각 디스크의 공진과 사각 스파이럴 스트립 급전 선로의 공진이 전자기적으로 결합하여 넓은 대역폭을 가지게 된다. 안테나에서 사각 디스크의 단락핀의 수와 배열 간격은 디스크의 캐패시턴스에 영향을 주게 되어 공진주파수는 1.90 GHz에서 2.556 GHz까지 이동하며 이에 따라서 안테나의 전기적 크기와 대역폭에도 영향을 미치게 된다. 사각 디스크에 단락핀이 3개 연결되었을 때 안테나는 2.556 GHz의 중심 주파수에서 전기적 부피가 $0.094\lambda_0{\times}0.094\lambda_0{\times}0.094\lambda_0$ 이하로써 소형의 크기를 가지며 $26.8\%$의 넓은 대역폭을 가진다.

• 한국산학기술학회논문지
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• 제13권12호
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• pp.5655-5660
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• 2012

본 연구의 목적은 경계층 해석법을 이용하여 고효율 열교환기 설계를 위한 이론적 접근법을 제시하고 기존 열교환기에 많이 사용되고 있는 사각 평판 핀과 이를 대체할 수 있는 원형 평판 핀에 대하여 경계층 형성과 간섭에 대하여 설명하고 속도 및 온도 경계층 성장에 따른 열전달계수의 변화를 나타내고자 한다. 더불어 한 개의 핀에서의 유동은 외부유동으로 간주할 수 있으나 다수의 핀 사이의 유동은 내부유동으로 간주하였고 이론적인 결과를 도출하였다. 결과적으로 열교환기의 고효율화 및 컴팩트화를 실현하기 위하여 경계층 간섭을 회피할 수 있는 방안을 이론적으로 제시하였고, 이러한 관점에서 원형 평판 핀이 사각 평판 핀에 비하여 열전달성능이 우수함을 알 수 있었다.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2009년도 하계학술발표대회 논문집
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• pp.1177-1181
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• 2009

Heat loss from a convective rectangular profile annular fin with variable inside fluid heat transfer coefficient and fin height is calculated by using both the one dimensional analytic method and two dimensional variables separation method. Heat loss from the two dimensional method and the relative error of heat loss between the one dimensional method and two dimensional method are presented as a function of the fin length, ambient convection characteristic number and fin height. One of the results shows that the relative error of heat loss between one dimensional method and two dimensional method is within 0.7% in the range of given parameters in this study.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2004년도 동계학술대회 논문집
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• pp.21-21
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• 2004

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.2414-2419
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• 2007

A rectangular fin with variable fin height, fin length and surrounding temperature is analyzed using a one-dimensional analytical method. Both the heat loss from a rectangular fin with non-insulated fin tip and that with insulated fin tip are presented as a function of the fin height, fin tip length and the convection characteristic number. The relative error in the heat loss of these two cases is also given as a function of the same variables. One of the results shows that the trend of heat loss for both cases with the variation of given variables is similar even though the relative error increases as the shape of the fin becomes shorter and fatter.

• 한국유체기계학회 논문집
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• 제8권4호
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• pp.39-47
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• 2005

The present study has been performed to investigate the influences of rectangular fins on heat transfer in an impingement/effusion cooling system with crossflow. To simulate the impingement/effusion cooling system with initial crossflow, two perforated plates are placed in parallel and staggered arrangements with a gap distance of 2 times of the hole diameter. The crossflow passes between the plates, and various rectangular fins are installed on the plates. Reynolds number based on the hole diameter is fixed to 10,000 and the flow rate of crossflow is changed from 0.5 to 1.5 times of that of the impinging jet. A naphthalene sublimation method is used to obtain the heat/mass transfer coefficients on the effusion plate. Also to analyze the flow characteristics, a numerical calculation is performed. When rectangular fins are installed, the flow and heat transfer pattern is changed greatly from the case without fins. In the injection hole region, the jet impinges on effusion plate without deflection and wall jet spreads symmetrically. In the effusion region, the crossflow accelerates due to the decrease of cross-sectional area in the channel. Local heat/mass transfer coefficients are enhanced significantly compared to the case without fins. As the blowing ratio increases, the effect of rectangular fins against the crossflow becomes more significant and then the higher average heat/mass transfer coefficients are obtained than the case without fins. However, the increase of blockage effect gives more pressure loss in the channel.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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• pp.289-296
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• 2004

The present study has been performed to investigate the influences of rectangular fins on heat transfer in an impingement/effusion cooling system with crossflow. To simulate the impingement/effusion cooling system with initial crossflow, two perforated plates are placed in parallel and staggered arrangements with a gap distance of 2 times of the hole diameter. The crossflow passes between the plates, and various rectangular fins are installed on the plates. Reynolds number based on the hole diameter is fixed to 10,000 and the flow rate of crossflow is changed from 0.5 to 1.5 times of that of the impinging jet. A naphthalene sublimation method is used to obtain the heat/mass transfer coefficients on the effusion plate. Also to analyze the flow characteristics, a numerical calculation is performed. When rectangular fins are installed, the flow and heat transfer pattern is changed greatly from case without fins. In the injection hole region, the jet impinges on effusion plate without deflection and wall jet spreads symmetrically. In the effusion region, the crossflow accelerates due to the decrease of cross-sectional area in the channel. Local heat/mass transfer coefficients are enhanced significantly compared to case without fins. As the blowing ratio increases, the effect of fins against the crossflow becomes more significant and then the higher average heat/mass transfer coefficients are obtained than the case without fins.

• 설비공학논문집
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• 제16권8호
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• pp.683-690
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• 2004

A modified rectangular fin is analyzed by two-dimensional analytic method and finite difference method. Relative error of heat loss from the modified rectangular fin between analytic method and finite difference method is presented. Comparisons of fin effectiveness and heat loss between a modified rectangular fin and a plane rectangular fin are made as a function of the non-dimensional fin length and wing height for different positions of wings by using analytic method. The ratio of the incremental rate of heat loss to that of the area of a modified rectangular fin is shown as a function of the wing height. One of the results shows that performance of a modified fin is more improved as the wing approaches the fin root.

• 대한기계학회논문집
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• 제18권6호
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• pp.1567-1571
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• 1994

Under the assumption that thermal conductivity of the fin is constant and the conditions ate steady state, effects of non-constant and thermally asymmetric root temperature and unequal surrounding convection coefficients of the fin on the heat loss from a fin of rectangular profile are investigated. The heat loss form a rectangular fin becomes maximum when the highest root temperature deviates from the fin center to the fin side which has a higher convection coefficient as surrounding convection coefficients of the fin increase and as the difference between the convection coefficient of fin top side and that of fin bottom side increases.