• 한국전산유체공학회지
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• 제13권2호
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• pp.20-26
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• 2008

A numerical study is carried out to analyze the steady three-dimensional turbulent flow and convective heat transfer in a staggered pin-fin array with diamond shaped elements at various geometrical configurations. Steady Reynolds-averaged Navier-Stokes equations and energy equation are solved using a finite volume based solver. Shear stress transport (SST) model is used as turbulence closure. The computational domain is composed of one pitch of pin-fin displacement with periodic boundary conditions on the surfaces normal to the streamwise direction and the cross-streamwise direction. The numerical results for Nusselt number and friction factor are validated with experimental results. The effects of pin angle, pin height and pitch on Nusselt number, friction factor and efficiency index are investigated.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 춘계학술대회논문집
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• pp.303-309
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• 2009

In this study, the heat transfer and flow field of condenser used on Kim-chi refrigerator is analysed with numerical method. Main objective is to present the base data for designing new condenser model with improvement of heat transfer performance. For CFD analysis, a commercial code, STAR-CCM+ was used. The water was used for the inner working fluid and the air was used for the outer fluid. The condenser type used in this study is a flat plate fin-and-tube heat exchanger. As factors for performance analysis, the effect of condenser geometry and air velocity was investigated. As a result, it has been observed that there is a suitable fin pitch with which heat transfer performance of condenser is maximized.

• 대한기계학회논문집B
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• 제26권8호
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• pp.1191-1200
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• 2002

The measurements of velocity vectors are made in the near wake(X/d=5.0) of a circular cylinder with serrated fins. Velocity of fluid which flow through fins decreases as increasing fin height and freestream velocity and decreasing fin pitch. Therefore the velocity distribution at X/d=0.0 has lower gradient with increasing freestream velocity and fin height and decreasing fin pitch. The discontinuity of the streamwise velocity gradient is observed near the fin edge and causes significant changes in V-component velocity distribution in the near wake. This change attributes to the differences in Strouhal number and entraintment flow behavior. Increased turbulent intensity around a circular cylinder due to the serrated fins and entrainment flow are important factors for the recovery of velocity defect. The widths of velocity and turbulent intensity distribution of fin tubes are wider than those of a circular cylinder. The normalized velocity and turbulent intensity distributions with a hydraulic diameter which is proposed in this paper are in closer agreement with those of a circular cylinder.

• 대한기계학회논문집B
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• 제35권3호
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• pp.269-278
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• 2011

본 연구에서는 구리 재질의 평판 핀과 나선형 핀-관 열교환기에 대하여 핀 피치와 열수의 변화에 따른 공기측 전열성능을 검토하였다. 두 형상 모두 핀 피치가 열전달계수에 미치는 영향은 미미하였다. 마찰인자는 핀 피치가 증가하면 증가하였다. 열수가 미치는 영향은 형상에 따라 다르게 나타났다. 평판 핀-관 열교환기의 경우 열전달계수는 열수가 증가할수록 감소하였다. 하지만 나선형 핀-관 열교환기의 열전달 계수는 열수가 증가하면서 그 값이 증가하는 경향을 보였다. 평판 핀-관 열교환기의 열전달계수는 나선형 핀-관 열교환기의 열전달계수보다 높게 나타났다. 하지만 열수가 증가하면 그 차이가 줄어들어 4열이 되면 거의 같았다. 한편 마찰인자는 평판 핀-관 열교환기에서 다소 높게 나타나고 열수의 영향은 크지 않았다. 본 실험 데이터를 기존 상관식의 예측치와 비교하였다.

• 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.

• 한국산학기술학회논문지
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• 제22권1호
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• pp.31-36
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• 2021

최근에 지구온난화 문제로 인하여 자동차 공조시스템은 GWP 지수가 높은 R134a 냉매를 대체할 수 있는 대체 냉매를 적용하고 있다. 본 연구에서는 R1234yf 냉매를 사용하여 내부열교환기와 가면용량형 팽창밸브인 TXV를 적용한 자동차 공조시스템의 성능특성을 해석하였다. 상용 소프트웨어인 Amesim을 이용하여 주요 부품인 압축기, 응축기, 팽창장치, 증발기와 내부열교환기를 모델링을 하여 외기온도와 응축기 휜 피치 변화에 따른 냉동사이클 시뮬레이션을 수행하였다. 외기온도가 30℃에서 40℃로 증가함에 따라 시스템의 냉방용량은 3.1% 감소하고, 압축기 소비동력은 17.1% 증가하였다. 또한, 응축기의 휜 피치를 0.8 mm에서 1.4 mm로 증가시키면서, 사이클 성능특성을 해석하였다. 휜 피치가 1.0 mm 클 경우에 응축기의 방열량은 감소하였고, COP는 5.9% 까지 감소하였다. 응축기 휜 피치가 1.0 mm 보다 작은 0.8 mm에서는 시스템 성능에 큰 변화가 없어 휜 피치 1.0 mm에서 최적의 성능을 나타내는 것으로 분석되었다.

• 대한기계학회논문집
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• 제16권7호
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• pp.1381-1390
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• 1992

본 연구에서는 경사원주에서 발생하는 소용돌이 여기진동을 억제하기 위한 방 법으로 원주구조물 주위에서 발생하는 규칙적인 소용돌이 방출에 의한 여진력을 감소 시키도록 원주표면에 fin이나 wire를 부착시켜 단면형상을 바꾸는 방안을 실험적으로 검토한다. 즉, 밀폐순환식 유로을 이용하여 흐름에 경사되도록 탄성지지된 원주에 나선상의 fin과 wire를 감아, 경사각(.theta.)을 45, 60, 75, 90도, 나선피치각(.alpha.)을 30, 35, 40, 45, 50, 55, 60도, 나선권수(n)를 1,2,3으로 하여, 진동특성을 실험적으로 조사하고, plain원주와 비교하여 제진효과를 확인하며, 더우기 나선핀 원주의 최적형 상을 구하는 것을 목적으로 한다.

• 대한기계학회논문집B
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• 제26권8호
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• pp.1183-1190
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• 2002

An experimental study is performed to investigate the characteristics of near wake behind a circular cylinder with serrated fins using the constant temperature anemometer and through flow visualization. Previous report(Boo et al., 2001) shows that there are three different modes in vortex shedding behavior. This paper is focused on the identification of the physical reasons why the difference iss occured in vortex shedding. The through flow velocity crossing fins decreases as increasing fin height and decreasing fin pitch mainly due to the flow resistence. Vortex shedding is affected strongly by velocity distribution around fin tube, especially by the velocity gradient. The velocity distribution at X/d=0.0 has lower gradient with increasing freestream velocity and fin height and decreasing fin pitch. Those differences in velocity gradients generate different vortex shedding mechanism.

• 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.

• 한국산학기술학회논문지
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• 제8권6호
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• pp.1337-1342
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• 2007

본 연구에서는 동시 냉난방 히트펌프용 열교환기의 성능평가 및 설계해석 기술의 확보를 위해 난방운전 온도조건에서 6종의 루버핀-관 열교환기의 공기측 열전달특성 및 마찰특성을 실험을 통하여 조사하였다. 실험을 위해 공기엔탈피방식의 칼로리미터와 항온수조를 이용하였다. 전열량의 증가는 핀피치보다 열수에 의해 더 크게 나타났고, 핀피치가 작을수록 열전달계수는 더 높았다. 또한 핀피치가 작을수록 열수증가에 의한 열전달계수의 증가폭이 커졌다. 핀피치와 열수변화에 대한 j-계수와 f-계수는 레이놀즈 수가 증가할수록 감소하였고, 레이놀즈 수 400부근의 영역에서 역전현상이 존재하였다.