• 대한기계학회논문집B
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• 제24권4호
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• pp.570-577
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• 2000

Local heat transfer characteristics inside a hard disk driver(HDD) are investigated in this study. The investigation is considered between disks co-rotating in a cylindrical enclosure. The gap spacing, rotating speed and head-arm positions are mainly considered to understand the flow and heat transfer in the co-rotating disks. The naphthalene sublimation technique is used to determine local heat/mass transfer coefficients on the rotating disk. Flow patterns inside the co-rotating disks are investigated using a Laser Doppler Anemometer (LDA) and also analyzed numerically. The results show that the heat transfer coefficients on the disk changed little with the gap spacing between disks. Heat transfer rates in the outer region increases with increasing rotating Renolds number, but the values normalized by that on a free rotating disk give a similar pattern for the tested cases. The head-arm inserted between the rotating disks destroys the inner region resulting in enhancement of heat transfer in that region.

• 대한기계학회논문집B
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• 제28권5호
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• pp.535-544
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• 2004

The heat (mass) transfer characteristics in the tip-leakage flow region of a high-turning first-stage turbine rotor blade has been investigated by employing the naphthalene sublimation technique. The heat transfer data in the tip-leakage flow area for the tip clearance-to-span ratio, h/s, of 2.0% are compared with those in endwall three-dimensional flow region without tip clearance (h/s : 0.0 %). The result shows that the thermal load in the tip-leakage flow region for h/s = 2.0% is more severe than that in the endwall flow region for h/s : 0.0%. The thermal loads even at the leading and trailing edges for h/s = 2.0% are found larger than those for h/s = 0.0%. The tip-leakage flow results in heat transfer augmentations near the tip on both pressure and suction sides in comparison with the mid-span results.

• 대한기계학회논문집B
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• 제24권8호
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• pp.1029-1037
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• 2000

The present study investigates the local heat/mass transfer characteristics on a rotating disk which is the top disk covered with a shroud in HDD. The naphthalene sublimation technique is employed to determine the local heat/mass transfer coefficients on the rotating disk. Flow field measurements using Laser Doppler Anemometry (LDA) and numerical calculations are performed to analyze the flow patterns induced by the disk rotation. HDD has been developed for compactness and speedy data access, thus the rotating velocity of the disk is increased and the height of a hub is decreased. The experiments are conducted for the various hub heights of 5, 10 and 15 mm, for the rotating Reynolds numbers of $5.5{\times}10^4$ to $1.1{\times}10^5$ and for the effects of the presence of a read/write head arm. The results show that the heat transfer on the rotating disk is enhanced considerably for the decrease of the hub height and for the increase of the rotating Reynolds number. The head arm inserted in the cavity decreases the heat transfer despite the enhancement of tangential RMS velocity because of the deficit of the momentum in the flow field.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1997년도 하계학술대회 논문집 C
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• pp.1391-1392
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• 1997

The thin films of $\alpha$-Sexithiophene($\alpha$-6T) were deposited by Organic Molecular Beam Deposition(OMBD) technique. The $\alpha$-6T was synthesized and Purified by the sublimation method The thin films of the $\alpha$-6T were deposited under various deposition conditions. The effects of deposition rate substrate temperature, and vacuum pressure on the formation of these films have been studied. The molecular orientations of $\alpha$-6T films were investigated with the polarized electronic absorption spectroscopy. The molecules in the $\alpha$-6T film deposited at a low deposition rate under a high vacuum were almost aligned Perpendicular to the substrate. The film deposited at an elevated substrate temperature(${\sim}90^{\circ}C$) showed higher conductivity than deposited at room temperature.

• 대한기계학회논문집B
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• 제32권3호
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• pp.207-215
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• 2008

The heat/mass transfer characteristics on the plane tip surface of a high-turning first-stage turbine rotor blade has been investigated by employing the naphthalene sublimation technique. At the Reynolds number of $2.09{\times}10^5$, heat/mass transfer coefficients are measured for the tip gap height-to-chord ratio, h/c, of 2.0% at turbulence levels of Tu = 0.3 and 14.7%. A tip-surface flow visualization is also performed for h/c = 2.0% at Tu = 0.3%. The results show that there exists a strong flow separation/re-attachment process, which results in severe local thermal load along the pressure-side corner, and a pair of vortices named "tip gap vortices" in this study is identified along the pressure and suction-side tip corners near the leading edge. The loci and subsequent development of the pressure- and suction-side tip gap vortices are discussed in detail. The combustor-level high inlet turbulence, which increases the tip-surface heat/mass transfer, provides more uniform thermal-load distribution.

• 대한기계학회논문집
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• 제12권6호
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• pp.1415-1427
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• 1988

본 연구에서는 막냉각되고 있는 수평평판에서 분사각도와 분사율의 변화가 열 전달계수에 미치는 영향을 주 연구대상으로 하였다. 열전달계수의 측정을 위하여 나 프탈렌 승화법을 이용하였고, 열전달 계수에 가장 큰 영향을 미치는 유동장에 대한 이 해를 위해 슐리렌 광학계를 이용한 유동의 가시화 실험을 수행하였다. 분사각도는 Fig.1에서와 같이 y축 방향으로의 수직분사(case 1), 유동방향(x축방향)dp eogo 35˚ 경사진 분사(case 2), 그리고 유동의 직각방향(Z축)dp eogo 35˚경사진 분사(case 3) 등 3가지의 경우에 대해 실험하였고, 분사율은 0.5, 1.0, 1.8로 변화시켰다.

• 대한기계학회논문집B
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• 제25권3호
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• pp.405-413
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• 2001

The present study investigates convective heat/mass transfer and flow characteristics inside a rotating two-pass rectangular duct. A naphthalene sublimation technique is employed to determine the detailed local heat transfer coefficients using the heat and mass transfer analogy. The objective of this study is to determine the effects of turning geometry with rotation for 0.0$\leq$Ro$\leq$0.24. The results reveal that the sharp-turn corner has the larger pressure drop and lower heat transfer in the post-turn region than those of the round-turn corner. The strong secondary flow enhances heat transfer for the round-turn corner. Coriolis force induced by the rotation pushes the high momentum core flow toward the trailing wall in the first passage with radially outward flow and toward the leading wall in the second passage with radially inward flow. Consequently, the high heat transfer rates are generated on the trailing surface and the leading surface in the first and second passage, respectively. However, the strong secondary flow due to the turning dominates the flow pattern in the second passage, thus the heat transfer differences between the leading and trailing surfaces are small with the rotation.

• International Journal of Air-Conditioning and Refrigeration
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• 제13권4호
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• pp.196-205
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• 2005

In this paper, recent research trend on heat transfer in impinging jet is reviewed. We focused on submerged jet that air issued into air or liquid issued into liquid. To control and enhance the heat transfer in single jet, researchers have performed a lot of experiments by considering the nozzle geometry, impinging surface and active method such as jet vibration, secondary injection and suction flow. The studies on multiple jet have been mainly focused on finding out the optimum condition and on investigating many different factors concerned with application condition (crossflow, rotation and geometry etc.) and combined techniques (rib turbulator, pin fin, dimple and effusion hole etc.). All most experiments showed the detailed heat transfer data by using liquid crystal method, infrared camera technique and naphthalene sublimation method. Many numerical calculations have been performed to investigate the flow and heat transfer characteristics in laminar jet region. Various turbulence models such as $k-\varepsilon-\bar{\nu^2}$, modified $k-\varepsilon-f_{\mu}$ were applied to the calculation for turbulent jet and the predicted results showed a good agreement with the experimental data. Although a lot of studies on impinging jet have performed consistently up to recently, further studies are still required to understand the flow and heat transfer characteristics more accurately, and to give a guideline for optimum impinging jet design in various applications.

• 설비공학논문집
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• 제18권11호
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• pp.888-895
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• 2006

The present study has been conducted to investigate the effects of Reynolds number on heat/mass transfer and pressure drop characteristics in a rotating smooth two-pass duct. For stationary cases, the heat/mass transfer and pressure drop Is decreased on turning region of both leading and trailing surfaces as Reynolds number increases. For rotating cases, increment of Reynolds number affects differently the heat/mass transfer and pressure drop on the leading and trailing surfaces. In the first pass, for example, the heat/mass transfer on the leading surface is greatly increased, though the heat/mass transfer on the trailing surface is almost the same. The reason is that effect of the main flow is more dominant than effect of secondary flow. In particular, it gave decrement of the heat/mass transfer and the pressure drop at turning region and upstream region of second pass for both non-rotating and rotating cases.

• 한국정보통신학회:학술대회논문집
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• 한국정보통신학회 2012년도 춘계학술대회
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• pp.734-736
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• 2012

II-VI족 화합물반도체인 CdTe는 태양광을 전기로 변화하는데 있어서 이상적인 1.45eV의 직접천이형 에너지 band gap을 가지고 있으며, $1{\mu}m$ 내외의 두께로도 가시광의 99%이상을 흡수하는 높은 광흡수 계수를 가지므로 얇은 두께로도 태양전지 제작이 가능하다. 현재 CdTe를 이용한 태양전지는 최고 16.5%의 변환효율을 보이고 있으며, 대면적의 module에서는 10% 이상의 효율을 나타내고 있다. CdTe 박막의 제작 방법으로는 스크린 프린팅법(screen printing), 스퍼터링법(sputtering), 근접승화법(CSS:close space sublimation) 등이 있는데, 이중 마그네트론 스퍼터법의 경우, 대면적으로 균일하게 증착이 가능하기 때문에 양산화에 적합하고, 증착 온도를 낮출 수 있으며, 성장 중 도핑 제어가 용이한 장점을 갖고 있다. 특히, 필름 형태의 polyimide (PI), molybdenum (Mo) 기판의 경우, 유리기판에 비해 가벼우면서 깨지지 않아 취급이 용이하다는 장점이 있다. 또한 필름 형태로 제작할 경우 유연성이 있는 태양전지 제작이 가능하여 그 응용 범위를 넓힐 수 있다. 본 연구에서는 PI 및 Mo, 유리 기판 위에 마그네트론 스퍼터법으로 CdTe 박막을 증착하고, 제조 조건에 따른 박막의 구조적, 광학적 물성을 조사하였다.