• 한국산학기술학회논문지
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• 제14권2호
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• pp.523-528
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• 2013

본 실험에서는 산업용 발전 설비에 사용되는 인버터 내부의 압입형과 압출형 두 종류 히트싱크의 방열 성능을 평가하였다. 실험에 사용된 압입형 히트싱크는 62개의 핀을 가지고 있고, 압출형은 38개의 핀을 가지고 있으며 두 히트싱크의 외형의 크기는 같다. 반면 압출형 히트싱크는 핀의 표면에 반경 1mm의 곡률을 주어 전열면적을 압입형과 같게 하였다. 결과적으로 압입형과 압출형 히트싱크는 전체 입력열량에 대해 각각 70.7%, 63.8%를 방열하였다. 입력열량 중 나머지는 자연대류 및 복사를 통해 외부로 방열되었다. 압출형 히트싱크는 단순히 핀의 개수로 보면 압입형 히트싱크보다 40% 감소했지만, 방열양은 6.9% 만 감소하였다. 이는 표면 곡률을 통한 유효 전열면적의 증가와 압출형 히트싱크의 상대적으로 우수한 전열특성의 효과로 판단하였다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2010년 춘계학술대회논문집
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• pp.530-533
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• 2010

This paper presents numerical analysis and design optimization of various turbine blade cooling techniques with three-dimensional Reynolds-averaged Navier-Stokes(RANS) analysis. The fluid flow and heat transfer have been performed using ANSYS-CFX 11.0. A fan-shaped hole for film-cooling has been carried out to improve film-cooling effectiveness with the radial basis neural network method. The injection angle of hole, lateral expansion angle of hole and ratio of length-to-diameter of the hole are chosen as design variables and spatially averaged film-cooling effectiveness is considered as an objective function which is to be maximized. The impingement jet cooling has been performed to investigate heat transfer characteristic with geometry variables. Distance between jet nozzle exit and impingement plate, inclination of nozzle and aspect ratio of nozzle hole are considered as geometry variables. The area averaged Nusselt number is evaluated each geometry variables. A rotating rectangular channel with staggered array pin-fins has been investigated to increase heat transfer performance ad to decrease friction loss using KRG modeling. Two non-dimensional variables, the ratio of the eight diameter of the pin-fins and ratio of the spacing between the pin-fins to diameter of the pin-fins selected as design variables. A rotating rectangular channel with staggered dimples on opposite walls are formulated numerically to enhance heat transfer performance. The ratio of the dimple depth and dimple diameter are selected as geometry variables.

• 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.

• 한국항공우주학회지
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• 제41권5호
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• pp.357-365
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• 2013

본 연구에서는 미사일형상의 몸체(쉘)와 쉘의 헤드부에 조종면을 부착한 발사체에서 힘과 모멘트를 측정하였다. 쉘과 헤드부는 상호 분리되어 있으며, 쉘은 모터에 의하여 회전되도록 하였다. 헤드부는 쉘의 회전방향과는 반대로 회전하며, 헤드부의 회전은 한 쌍의 조종면에 동일한 회전 방향으로 각변위을 주어서 비행하는 경우에 자연적으로 회전력이 발생되도록 하였다. 실험에서의 유속은 40 m/s로 설정하였으며, 레이놀드수는 헤드직경을 기준으로 $1.3{\times}10^5$였다. 발사체의 자세제어 및 방향전환을 위하여 헤드부에 있는 다른 한쌍의 조종면은 각변위의 조정이 가능하도록 하였다. 회전하는 발사체에서 힘과 모멘트의 변화가 측정되었으며, 측정된 결과로부터 FFT 분석을 통하여 영향력이 있는 진폭과 주파수를 얻었다.

• 대한기계학회논문집B
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• 제27권5호
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• pp.579-588
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• 2003

Optimum fin effectiveness of geometrically and thermally asymmetric trapezoidal fins is represented as a function of the ratio of the fin bottom to top Biot numbers, the ratio of the fin tip to top Biot numbers and fin shape factor. Optimum fin effectiveness is taken as 98% of the maximum fin effectiveness by comparing the increasing rate of fin effectiveness with that of dimensionless fin length. For this analysis, two dimensional separation of variables method is used. Also, the value of the slope of upper surface of the fin and fin efficiency corresponding to optimum effectiveness are presented.

• 설비공학논문집
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• 제14권11호
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• pp.871-879
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• 2002

The characteristics of flow and heat transfer in the heat exchanger of heat pipes with fins have been studied numerically for cooling enhancement of electronic components of KTX (Korea Train eXpress). Numerical analysis and methodology have been conformed by comparing the experimental results for inlined array of heat pipes. The staggered arrangement of heat pipes has been proposed in order to achieve heat transfer enhancement. As results, the geometry change to the staggered array is conformed to increase the heat transfer of the system accompanied by an increase of pressure drop. The current results of friction factor and Colburn j factor are presented in terms of Reynolds number and staggered distance, and are expected to use for design and manufacture of such a system.

• Journal of Mechanical Science and Technology
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• 제16권12호
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• pp.1725-1732
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• 2002

Combined convection and radiation heat transfer in a circular tube with circumferential fins and circular disks is investigated for various operating conditions. Using a finite volume technique for steady laminar flow, the governing equations are solved in order to study the flow and temperature fields. The P- 1 approximation and the weighted sum of gray gases model (WSGGM) are used for solving the radiation transport equation. The results show that the total Nusselt number of combined convection and radiation is higher than that of pure convection. If the temperatures of the combustion gas and the wall in a tube are high, radiation becomes dominant. Therefore, it is necessary to evaluate the effect of radiation on the total heat transfer.

• 한국군사과학기술학회지
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• 제22권5호
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• pp.625-636
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• 2019

Recently, research on projectiles with wings for precision guidance is actively underway. In this study, we analyzed how the tail fins attached to the projectile affect the base drag. Aerodynamic analysis was performed with RANS(Reynolds Averaged Navier-Stokes) equations using FLUENT, a commercial CFD(Computational Fluid Dynamics) code. Through the aerodynamic analysis, the base drag characteristics of the projectile by parameters (number, length, thickness, position, shape of tail fin) were investigated. The results of this study are expected to be applicable to aerodynamic design of tail fins mounted on projectiles.

• 설비공학논문집
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• 제9권3호
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• pp.259-267
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• 1997

Average heat transfer coefficients and friction coefficients have been measured from staggered short pin-fin arrays to investigate the effect of fin shapes. Flow entering into the test section is a fully developed duct flow and the Reynolds number ranges from 5,000 to 25,000 based on fin diameter and average approaching velocity. The fin has three different shapes; uniform-diameter circular fin, two stepped-diameter circular fins. Average heat transfer rates change slightly with the fin shapes. However, friction loss(pressure loss) for the stepped-diameter fins is significantly less than that for the uniform-diameter fin. This results indicate that the stepped-diameter fin arrays in duct flow enhance heat transfer rates largely based on unit pumping power.

• 한국기계가공학회지
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• 제18권5호
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• pp.96-102
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• 2019

This study investigated the heat dissipation characteristics of a heat-sensitive LED. More than 80% of the power supply is converted into heat energy, which has a fatal impact on the lifetime of the LED. Therefore, the effective heat dissipation characteristics of a heatsink, such as a 30W floodlight, through forced convection were grasped and the heat transfer characteristics were tested. As a result, it was confirmed that the smaller the number of fins, the more the temperature distribution varies according to the wind velocity. In addition, the larger the number of fins, the smaller the temperature difference according to the wind velocity. Therefore, it was found through this experiment that excellent heat dissipation performance was exhibited as the heat dissipation area and wind velocity increased.