• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.537-541
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• 2003

In order to control the missiles by aerodynamics, control surfaces sometime called fins are used. Deflection angles of these fins are the right control variables of the aerodynamics, but aerodynamicists prefer to use analytic variables called aileron, elevator and rudder instead of these physical variables, because these three analytic variables dominantly influence on the roll, pitch and yaw channels of the missile maneuver, respectively, and each can be assumed a linear combination of four fin deflection angles. On that basis, roll, pitch and yaw autopilots for controlling the attitudes or lateral acceleration of the missile are designed, and as a consequence outputs of each autopilot are aileron, elevator and rudder commands, respectively. In the existing fin control scheme for the typical tail-fin controlled cruciform missiles, firstly these outputs are distributed to four fin defection commands, and after that four fins are actuated by fin controllers so that their deflections follow the commands. This paper shows that performance of such control schemes can be degraded significantly when fin actuators have certain physical constraints such as slew rate, voltage or current limit, uncertainty of actuator dynamics, and so on, and propose a new control scheme which alleviates such problems. This scheme can be widely applied to various fin actuation systems. But in this paper, for convenience, tail-fin controlled cruciform missile is taken as an example, and it is shown that a proposed control scheme gives better performance than the existing one.

• 청정기술
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• 제14권4호
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• pp.265-270
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• 2008

본 연구는 전자기기 모듈의 공기 냉각용 정렬 배열된 핀-휜 열교환기에서 휜 형상의 변화가 유동 및 열전달에 미치는 영향을 수치적으로 해석하였다. 휜 단면의 기하학적 형상은 세 가지로서 원형, 타원형, 그리고 날개형이었다. 취급된 모든 휜의 단면적과 높이는 서로 동일하지만, 그 표면적만은 서로 달랐다. 그 결과, 휜의 표면적, 열전달계수, 그리고 열전달 성능은 휜의 형상에 크게 의존하였다. 적절한 형상을 갖는 휜의 열전달 성능은 세 가지 형태의 핀-휜 중에서 날개형 핀-휜이 가장 우수하였다. 이러한 결과로부터 공기의 유량증가측은 휜의 밀도증가 없이 적절한 핀-휜의 형상변화만으로도 핀-휜 열교환기의 냉각성능을 크게 향상 시킬 수 있음을 알 수 있었다.

• International Journal of Air-Conditioning and Refrigeration
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• 제13권3호
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• pp.152-157
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• 2005

This paper reviews the literature on the performance of fin-and-tube heat exchangers under frosting and defrosting conditions. The effects of frosting and defrosting on the following parameters were discussed: frost growth, overall heat transfer coefficient, surface roughness, and surface characteristics on the heat exchanger. Comparisons of the experimental results and empirical correlations that were obtained from open literature were presented. In addition, a review of the defrosting methods was conducted.

• 설비공학논문집
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• 제7권1호
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• pp.161-170
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• 1995

This study is concerned with the numerical analysis of performance on fin-tube heat exchanger under frosting condition. In this work, tube-by-tube method using LMED is employed. The present results are compared with O'Neal's experimental and numerical results. A standard evaporator model with 2rows-2columns is selected to investigate the effects of the various parameters such as fin pitch, air flow velocity, and humidity. The results show that frost thickness and the amount of frost per unit area decrease as fin-pitch becomes narrower. In the meantime, frost thickness and accumulation rate increase with higher inlet air humidity. It is shown that heat transfer rate increases during 30minutes and then it decreases. Heat transfer rate and the amount of frost increase with air velocity, however frost thickness does not increase over a certain velocity.

• 전자공학회논문지
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• 제52권10호
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• pp.33-46
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• 2015

본 논문에서는 ITRS(International Technology Roadmap for Semiconductors)를 따라 스케일 다운된 FinFET 소자의 디지털 및 아날로그 회로의 성능을 예측했다. 회로 성능의 정확한 예측을 위해 기생 커패시턴스와 기생 저항 모델을 개발해 3D Technology CAD 해석 결과와 비교해 오차를 2 % 미만으로 달성했다. 기생 커패시턴스 모델은 conformal mapping 방식을 기반으로 모델링 되었으며, 기생 저항 모델은 BSIM-CMG에 내장된 기생 저항 모델을 핀 확장 영역 구조 변수($L_{ext}$) 변화에 따른 기생 저항 성분 변화를 반영 할 수 있도록 개선했다. 또한, 공정 단위 변화에 대해 소자의 전압전류의 DC 특성을 반영하기 위해 BSIM-CMG 모델의 DC 피팅을 진행하는 알고리즘을 개발했다. BSIM-CMG에 내장된 기생 모델을 본 연구에서 개발한 저항과 커패시턴스 모델로 대체해 압축 모델 내부에 구현하여, SPICE 시뮬레이션을 통해 스케일 다운된 FinFET 소자의 $f_T$, $f_{MAX}$, 그리고 링 오실레이터와 공통 소스 증폭기의 기생 성분으로 인한 특성변화를 분석했다. 정확한 기생 성분 모델을 적용해 5 nm FinFET 소자까지 회로 특성을 정량적으로 제시했다. 공정 단위가 감소함에 따라 소자의 DC 특성이 개선될 뿐만 아니라 기생 성분의 영향이 감소하여, 회로 특성이 향상됨을 예측했다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.82-85
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• 2006

측면 기울기가 변하는 사다리꼴 핀이 일차원 해석적 방법에 의하여 최적으로 설계된다. 각기 다른 네 경우의 대류특성계수에 대하여 핀 끝 길이를 따른 열손실의 변화경향이 보여 진다. 최적의 열손실은 다소 임의적으로 최대열손실의 92%로 선택된다. 이러한 최적의 열손실이 발생할 때의 최적의 핀 길이 대 대류특성계수의 변화가 나타내진다. 최적의 유용성과 특정한 경우의 유용성이 핀 형상 계수의 함수로 보여 진다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집B
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• pp.314-320
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• 2000

In this study, the wet surface heat transfer coefficients and friction factors of PF heat exchangers are presented. Two sample with different fin pitch(1.25mm, 1.5mm) were tested. Tests were conducted in a open loop wind tunnel. The wet surface heat transfer coefficient was reduced following the procedure given in ARI 410-81. Results showed that the heat transfer coefficients of the heat exchanger with 1.5mm fin pitch were approximately the same as those with 1.25mm fin pitch, except at low reynolds number(Re<100), where the heat transfer coefficients of 1.5mm fin pitch were slighly higher than those with 1.25mm fin pitch. The friction factors of the 1.25mm fin pitch, however was 120 % to 160 % higher than those of the 1.5mm fin pitch. The wet surface heat transfer coefficients were lower than those of the dry surface. The wet surface friction factors, however, were higher than those of the dry surface.

• Journal of the Korean Society for Industrial and Applied Mathematics
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• 제6권2호
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• pp.109-120
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• 2002

The dimensionless heat loss from a modified asymmetric rectangular fin is investigated as a function of the fin top and tip Biot numbers using the two-dimensional separation of variables method. A rectangular fin is modified by attaching the wing on the top side of the fin. Fin effectiveness and efficiency with the variation of the location of the wing and the width of the wing are presented. The relationship between top surface Biot number and bottom surface Biot number as well as the relationship between the dimensionless wing height and the location of the wing for equal amount of heat loss is also discussed.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2006년도 하계학술발표대회 논문집
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• pp.633-638
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• 2006

This study presents the air side heat transfer and friction characteristics of fin-tube heat exchangers with various fin types. A total of 8 samples of heat exchangers are tested. Fin patterns tested are slit, louver and plate fins. Each fin type has three cases of number of tube rows(N=1, 2, 3) and two different fin pitches. The results are plotted in terms of Colburn j-factor and friction factor f with respect to Reynolds number in the range of 200 to 510.

• 한국지열·수열에너지학회논문집
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• 제8권2호
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• pp.48-54
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• 2012

To analyze the cooling performance of fin-tube evaporator in the refrigerator truck using R744 according to frost growth, the analytical model of evaporator was developed under frost and non-frost conditions. The performance of fin-tube evaporator was investigated with frost thickness and indoor temperature. Besides, the performance of evaporator under frost condition was compared to that under non-frost condition. As a result, area of air passage and system performance were decreased as the frost thickness increased. The cooling capacity was reduced by 10%, 20%, 30% when the frost thickness was 0.7 mm, 1.1 mm, and 1.6 mm respectively. At these conditions, the block ratio was 31%, 48%, and 71%. In addition, the outlet quality of refrigerant was not over 1 when the frost thickness was 1.6 mm in spite of high indoor air temperature.