• 대한기계학회논문집B
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• 제21권6호
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• pp.830-840
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• 1997

In this study, condensation heat transfer coefficients(HTCs) of CFC-11, HCFC-123 and HCFC-141b are measured, which are used/or considered as working fluids in centrifugal chillers. The main objectives of this study are to measure and compare the HTCs of various refrigerants on plain and low fin tubes and also to find out the optimum fin density of the low fin tubes. To accomplish these goals, HTCs of three refrigerants are measured for the plain tube as well as 4 types of low fin tubes. All measurements are carried out at the vapor temperature of 39.deg. C with the wall temperature difference of 3 .deg. C ~ 8.deg. C. For all the refrigerants tested, a low fin tube of 28 fins per inch yielded the best performance among all the tubes tested. For the plain tube, the HTCs of CFC-11 and HCFC-141b were very similar and those of HCFC-123 were 10% lower than those of CFC-11.Thus, it can be concluded that HCFC-123 and HCFC-141b are acceptable as alternative refrigerants for CFC-11 from the view point of condensation heat transfer.

• Journal of Advanced Marine Engineering and Technology
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• 제40권8호
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• pp.686-691
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• 2016

This paper employs numerical tools to obtain an optimal thermal design of a heat exchanger with plain-fins. This heat exchanger is located at the condensing section of a crevice-type heat pipe. The plain-fins in the heat exchanger are radically mounted to two tubes in the condensing section. To obtain the optimal design parameters, a computational fluid dynamics technique is introduced and applied to different placement configurations in a system module. Owing to its effects on the heat pipe performance, the temperature difference between the tube surfaces and ambient air is investigated in detail. A greater heat dissipation rate occurs when the plain-fin offsets change from 2 to 3 mm. When this temperature difference is ${\Delta}T=70^{\circ}C$, the upper part of the plain-fins undergoes an accumulation of heat. At below $70^{\circ}C$, the dissipation of heat is accepted. A rectangular plain-fin geometry with varying widths and heights does not have a significant impact on the heat dissipation through-out the overall system. In addition, the temperature distributions between different plain-fin pitches show an equal profile even with different fin pitches.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회B
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• pp.2131-2136
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• 2008

The characteristics of heat transfer and pressure drop in an offset strip fin heat exchanger was studied with a steady-state three dimensional numerical model. Flow Reynolds number $Re_{dh}$ ranged from 10 to 3500 and Prandtl number Pr ranged from 0.7 to 50. The dimensionless performance factors, i.e. 'the pumping power factor F' and 'the heat transfer performance factor J' were analyzed and obtained a relationship between them. Finally, the prediction of F and J factors was generalized for different Prandtl numbers.

• Journal of Advanced Marine Engineering and Technology
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• 제41권1호
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• pp.1-7
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• 2017

두 판을 맞대기 용접할 경우 용접부 시종단부 측면에 열전도도가 큰 금속(예를 들어 구리)으로 만든 엔드 탭을 장착하고 용접을 진행하면 용접부 끝부분의 비드흘러내림과 결함을 방지할 수 있다. 본 논문에서는 엔드 탭의 방열 성능을 강화시키기 위하여 자연 대류에 의한 방열 특성이 뛰어난 것으로 알려진 평판 휜 모양을 적용하였고, 실험 및 수치해석을 통하여 엔드 탭에 평판 휜 모양의 구멍이 있는 형상이 구멍이 없는 형상보다 방열 성능이 더 뛰어남을 확인하였다. 그리고 열, 유동해석을 통하여 엔드 탭의 휜 형상에 대한 냉각 속도를 평가하여, 방열 성능 측면으로 도움이 될 형상 인자적인 특성을 파악하였다. 그 결과, 엔드 탭에 수직 휜이 있으며 휜 간 간격에 최적 휜 간 간격 식을 적용한 구조가 우수한 형상으로 판단되었다.

• 한국태양에너지학회 논문집
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• 제33권6호
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• pp.85-91
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• 2013

It is essential to reduce the amount of fossil fuel because facing with the natural problem such as a global warming. To achieve this goal, many of interests in the use of renewable energy is growing. Especially, as one of these renewable energy systems, a solar air heater invention has been conducted for enhancing the efficiency of solar air heater. According to this trend, scale-down sized experiment apparatus was constructed and performed for searching a proper fin and confirming the heat transfer performance by fin shape on constant heat condition to enhance efficiency of solar air heater. In this experiment, heat gain, convection heat transfer coefficient, number of transfer units, Nusselt number, Reynold's number, friction factor, performance factor were investigated in order to evaluate the thermal characteristics based on the real data obtained. By comparison with the each fin performance, a zigzag shape keeping a right angle to the plate had the highest value among them.

• 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.

• 제어로봇시스템학회논문지
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• 제10권7호
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• pp.658-668
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• 2004

This paper is concerned with a control allocation strategy using the dynamic inversion and the pseudo inverse control which generates the nominal control input trajectories. In addition, an autopilot design method is proposed by using time-varying control technique which is time-varying version of the pole placement of linear time-invariant system for an agile missile with aerodynamic fin and thrust vectoring control. The control allocation proposed in this paper is capable of extracting the maximum performance by combining each control effector, aerodynamic fin and thrust vectoring control. The adopted time-varying control technique for the autopilot design enhances the robustness of the tracking performance for a reference command. The main results are validated through the nonlinear simulations with aerodynamic data.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.525-530
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• 2003

This paper is concerned with a control allocation strategy using the dynamic inversion which generates the nominal control input trajectories, and autopilot design using the time-varying control technique which is time-varying version of pole placement of linear time-invariant system for an agile missile with aerodynamic fin and thrust vectoring control. Dynamic inversion can decide the amount of the deflection of each control effector, aerodynamic fin and thrust vectoring control, to extract the maximum performance by combining the action of them. Time-varying control technique for autopilot design enhance the robustness of the tracking performance for a reference command. Nonlinear simulations demonstrates the dynamic inversion provides the effective nominal control input trajectories to achieve the angle of attack command, and time-varying control technique exhibits good robustness for a wide range of angle of attack.

• International Journal of Air-Conditioning and Refrigeration
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• 제15권1호
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• pp.25-33
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• 2007

The investigation has been made into the prediction of heat exchange performance of a counter flow type double-tube condenser for natural refrigerant mixtures composed of Propane/n-Butane or Propane/i-Butane in a smooth tube and micro-fin tube. Under various heat transfer conditions, mass flux, pressure drop and heat transfer coefficient of the mixed refrigerants were calculated using a prediction method, when the length of condensing tube, total heat transfer rate, mass flux and outlet temperature of coolant were maintained constant. Also, the predicted results were compared with those of HCFC22. The results showed that the mixed refrigerants of Propane/n-Butane or Propane/i-Butane could be substituted for HCFC22, while the pressure drop and overall heat transfer coefficient of the refrigerants were evaluated together.

• Journal of the Korean Society for Industrial and Applied Mathematics
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• 제3권2호
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• pp.147-156
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• 1999

A numerical simulation has been carried out for the performance characterization of heat sinks in electronic equipment. Heat transfer characteristics have been analyzed for various design parameters including the shape of heat sink, thickness of fin base and fin pitches. A commercial program called Flotherm has been employed for the numerical calculation. Optimal design of the heat sink has been persued which is closely related with the reduction of heat resistance involved in conduction and convection of heat.