• 한국결정성장학회지
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• 제2권2호
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• pp.77-82
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• 1992

FZ법에 의한 결정성장에 있어서 용융대는 고액 계면의 장력에 의해 유지되고 상.하부의 고체봉 사이에 위치하고 있다. 따라서, 용융대의 표면에서는 온도와 농도 차이에 의해 표면장력의 구배가 발생하고 있는 marangoni 대류의 구동력으로 작용한다. 본 연구에서 정상상태의 결정성장시는 결정의 가장자리 영역에서의 Solute 농도는 결정내부 보다도 높아지게 되고 전위의 분포도 불규칙하여 지며, void나 기포 침투, Secondary phase의 생성 및 미소균열등의 결함 발생 확률이 계면부근에서 높아지는 결과를 알 수 있었다. 이는 고액성장 계면이 marangoni 대류에 의하여 이 영역에서 온도의 국부적인 변동에 의해 불규칙하여 지게 되기 때문이라 사료된다.

• 한국산학기술학회논문지
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• 제13권8호
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• pp.3295-3300
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• 2012

3차원 유한요소법은 구조물에 존재하는 표면균열과 내재균열들의 응력확대계수를 구하는데 이용되어 진다. 기하모델, 즉 솔리드모델은 3차원 균열들을 포함하고 있다. 국부적인 절점밀도가 선택되어 지면 자동적으로 기하모델 영역에 중첩되어 지며 절점은 버블패깅 방법에 의해 생성되어지고 10절점 사변형 솔리드요소는 데라우니 삼각화 기술에 의해 생성하였다. 시스템의 정확도와 효용성을 체크하기 위해 인장하중을 받는 평판에 하나의 균열이 존재하는 경우의 응력확대계수를 구해 Raju-Newnam식과 비교하여 5%이내의 차이를 보였다. 또한, 인장하중을 받는 평판에 두개 균열이 존재하는 경우의 해석을 통해 상호 간섭 효과를 분석하였다.

• Korean Chemical Engineering Research
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• 제49권5호
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• pp.605-610
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• 2011

내경이 0.105 m이고 높이가 2.5 m인 삼상(기체-액체-고체) 유동층에서 상대적으로 큰 기포와 작은 기포의 체류량 특성을 고찰하였다. 기체유속(0.01~0.07 m/s), 액체유속(0.01~0.07 m/s) 그리고 입자크기($0.5{\sim}3.0{\times}10^{-3}m$)가 상대적으로 큰 기포와 작은 기포의 체류량에 미치는 영향을 검토하였다. 삼상 유동층에서 이들 두 종류 기포들의 체류량은 동력학적 기체 유출 방법(Dynamic gas disengagement method)에 의해 측정된 각각 기포들에 의한 압력강하 정보로부터 정압강하법(static pressure drop method)에 의해 산출되었다. 기체조절기에 의해 조절되는 건조되고 여과된 공기와 물 그리고 밀도가 2,500 $kg/m^3$인 유리구슬을 각각 기체, 액체 및 고체유동입자로 사용하였다. 삼상유동층에서 이들 두 종류의 기포, 즉 상대적으로 큰 기포와 작은 기포들은 유동층 탑에 유입되는 기체와 액체의 흐름을 정지시킨 후 경과시간에 따른 탑 내부의 압력강하를 측정함으로써 효과적으로 조사하고 분리할 수 있었다. 이들 두 종류의 기포들은 경과시간에 따라 증가하는 압력강하의 기울기가 서로 매우 다르게 나타났다. 실험결과 상대적으로 큰 기포들의 체류량은 기체의 유속이 증가함에 따라 증가하였으나 액체의 유속이 증가함에 따라서는 감소하였다. 그러나, 이들 큰 기포의 체류량은 유동입자의 크기가 변화함에 따라 국부적인 최소값을 나타내었다. 상대적으로 작은 기포들의 체류량은 기체유속 또는 고체입자의 크기가 증가함에 따라 증가하였으나 액체의 유속이 증가함에 따라서는 약간 감소하였다. 이들 두 종류 기포들의 체류량들은 각각 본 연구의 실험 범위 내에서 조작변수들의 상관식으로 나타낼 수 있었다.

• 대한기계학회논문집B
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• 제28권8호
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• pp.895-901
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• 2004

Single-phase convection and nucleate boiling heat transfer were locally investigated for confined planar water jets. The detailed distributions of the wall temperature and the convection coefficient as well as the typical boiling curves were discussed. The curve for the single-phase convection indicated the developing laminar boundary layer, accompanied by monotonic increase of the wall temperature in the stream direction. Boiling was initiated from the furthest downstream as heat flux increased. Heat transfer variation according to the streamwise location was reduced as heat flux increased enough to create the vigorous nucleate boiling. Velocity effects were considered for the confined free-surface jet. Higher velocity of the jet caused the boiling incipient to be delayed more. The transition to turbulence precipitated by the bubble-induced disturbance was obvious only for the highest velocity, which enabled the boiling incipient to start in the middle of the heated surface, rather than the furthest downstream as was the case of the moderate and low velocities. The temperature at offset line were somewhat tower than those at the centerline for single-phase convection and partial boiling, and these differences were reduced as the nucleate boiling developed. For the region prior to transition, the convection coefficient distributions were similar in both cases while the temperatures were somewhat lower in the submerged jet. For single-phase convection, transition was initiated at $x/W{\cong}2.5$ and completed soon for the submerged jet, but the onset of transition was retarded to the distance at $x/W{\cong}6$ for the fee-surface jet.

• 대한기계학회논문집B
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• 제38권1호
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• pp.81-88
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• 2014

수평에 가깝게 설치된 튜브 원주면에 대해 평균 열전달계수를 결정하기 위한 실험적 연구를 수행하였다. 실험을 위하여 대기압 상태하의 물속에 잠긴 50.8 mm의 스테인리스강 튜브를 사용하였다. 과냉 및 포화 풀비등 조건을 모두 고려하였으며, 튜브 경사각은 수평으로부터 $9^{\circ}$까지 $3^{\circ}$ 간격으로 변경하였다. 포화상태에서는 튜브의 최하부로부터의 방위각이 $90^{\circ}$인 위치에서 측정한 국소비등열전달계수가 평균값으로 취급될 수 있으며, 이러한 경향은 튜브 경사각과는 무관함을 확인하였다. 그러나 물이 과냉상태인 경우, 평균 열전달계수의 위치는 경사각과 열유속에 의존한다. 열전달을 변화시키는 주된 열전달 기구는 액체교란 강도 및 기포군집에 의한 큰 기포 덩어리의 형성과 밀접한 관계가 있는 것으로 설명된다.

• Asian Pacific Journal of Cancer Prevention
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• 제15권5호
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• pp.1977-1980
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• 2014

Background: The popularity of the narghile waterpipe, also referred to as hookah, shisha or hubble-bubble has increased tremendously during the past few decades. The aim of this study was to expose perception of narghile among a representative sample of university students in Sakarya University campus. Materials and Methods: Written approval was taken from the local education authority. An anonymous questionnaire which was prepared by the investigators and contained 17 questions was administered. Nine of the questions were related to socio-demographic characteristics and eight were related to the students harm perceptions about waterpipe. A total of 1,320 questionnaries were received and after preliminary evaluation 1,255 (95.7%) were found to be suitable for evaluation. The data was evaluated in SPSS program by using percentages and averages. Results: The $mean{\pm}SD$ age of the students was $20.8{\pm}2.29$ years (min 18, max 32). There were 864 (68.8%) females and 391 (31.2%) males. A total of 6.3 % of the students (n=79) believed that waterpipe is not harmful because its smoke does not burn the lungs. Almost one-third (n=318) think that the carcinogenic chemicals are filtered while waterpipe smoke passes from the water; 12.1 % of the students (n=152) checked "true" for the statement of "waterpipe smoke contains no nicotine". It is seen that 14.0 % of the students (n=176) think waterpipe with fruit/aroma is healthier than plain waterpipe. Conclusions: As a result of this study, it is found out that a substantial number of university students have false beliefs on harmful effects of waterpipe smoking.

• 대한기계학회논문집B
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• 제20권4호
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• pp.1481-1490
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• 1996

This study is intend to improve flow pattern within evaporator, which is low quality and low mass flux, by installing narrow horizontal annular crevice so that enhance heat transfer coefficient. The motive, which made to study heat transfer enhancement by using narrow annular crevice, came from capillary phenomena and pumping force of generating vapor on refrigerant boiling. Tests were run about 5 models of turbulence promoter with CFC-12, in the range of evaporating temperature (15.deg. C), mass flux (50 to 100 kg/m$\^$2/s), heat flux (3.4 to 6.7 kW/m$\^$2/), quality (0.1 to O.5). It is observed that flow pattern within evaporator is changed closely to semi-annular flow or annular flow, of which refrigerant liquid is reached to the upper side of tube by using narrow annular crevice. When the narrow annular crevice is installed in the evaporator tube, local heat transfer coefficient is generally more improved than that of smooth tube. That fact is according to observed result of flow pattern. It is learned that narrow annular crevice has more efficiency at a low mass flux. At the TP-5, enhancement of heat transfer rate is about 170% compare to that of smooth tube on a low mass flux (50 kg/m$\^$2/s), and it is about 134% on a high mass flux (100 kg/M$\^$2/S), so that we know that it is on a very high condition.

• 천문학회보
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• 제39권1호
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• pp.61.1-61.1
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• 2014

GSH 006-15+7 is a Milky Way supershell discovered by Moss et al. (2012). This supershell shows large shell-like structures in H I velocity maps. We have analyzed FUV emission for the supershell regions based on the FIMS and GALEX observations. Bright FUV flux at the boundaries of the supershell is mostly originated from dust scattering of FUV photons by dust clouds which was also observed at the boundaries of the supershell. We could find the distance to the supershell can be closer more than 30% compared with the distance of 1500 pc suggested by Moss et al. (2012) from the dust scattering simulation. And we also found the albedo and the phase function asymmetry factor of interstellar grains were 0.30 and 0.40, respectively. The confidence range for the albedo covers the theoretical value of 0.40, but g-factor is rather smaller than the theoretical value of 0.65. The small g-factor might mean the environment of turbulent ISM of the supershell. Meanwhile, the excess of C IV and X-ray emissions in the inside of the supershell can support the existence of hot gas and cooling in the supershell. And the C IV and X-ray emissions are monotonically decrease as away from the center of the SNR. This indicates the size of the hot bubble has considerably shrunk. We applied a simple simulation model to the PDR candidate region of the lower part of the supershell and obtained a H2 column density N(H2) = 1017.0-18.0 cm-2 and total hydrogen density nH ${\geq}$ 10 cm-3. This result shows the PDR candidate region represents a transition region from the warm phase to the cool phase in the PDR.

• 천문학회보
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• 제37권2호
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• pp.99.2-99.2
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• 2012

We updated the far-ultraviolet (FUV) spectral images of the entire Vela supernova remnant (SNR) using newly processed FIMS/SPEAR data. In the present study, we compare the newly produced FUV images with the X-ray and $H{\alpha}$ images, and examine how the Vela SNR evolves and interacts with the ambient medium on a global scale. The comparison with X-ray images has revealed a FUV filamentary feature corresponding with the boundary of the northeast-southwest asymmetry of the X-ray shell. The relatively low O IV] ${\lambda}1404$ to O III] ${\lambda}{\lambda}1661$, 1666 ratio estimated on the FUV filament is compatible with the previous proposal that the observed asymmetry of the Vela SNR could be due to the ${\gamma}2$ Velorum stellar wind bubble (SWB). The southwest FUV features surrounding a faint extended X-ray region are characterized as the region where the Vela SNR is interacting slightly stronger with ambient mediums within the dim X-ray southwest section. From a comparison with the $H{\alpha}$ image, we identify a ring-like $H{\alpha}$ feature overlapped with an extended hot X-ray feature of similar size and two local peaks of C IV ${\lambda}{\lambda}1548$, 1551 emission. Their morphologies are consistent with the expected shape when the $H{\alpha}$ ring is in direct contact with the near or far side of the Vela SNR. We suggest that the B3V-type star HD 76161 found at the center of the $H{\alpha}$ ring would be the exciting source of the H II region.

• 대한기계학회논문집B
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• 제29권4호
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• pp.485-494
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• 2005

For the extensive investigation of local heat/mass transfer on the near-tip surface of turbine blade, experiments were conducted in a low speed stationary annular cascade. The turbine test section has a single stage composed of sixteen guide vanes and blades. The chord length and the height of the tested blade are 150 mm and about 125 mm, respectively. The blade has flat tip geometry and the mean tip clearance is about $2.5{\%}$ of the blade chord. Detailed mass transfer coefficient on the blade near-tip surface was obtained using a naphthalene sublimation technique. The inlet flow Reynolds number based on chord length and incoming flow velocity is changed from $1.0{\times}10^{5}\;to\;2.3{\times}10^{5}.$ Extremely complex heat transfer characteristics are observed on the blade surface due, to complicated flow patterns, such as flow acceleration, laminarization, transition, separation bubble and tip leakage flow. Especially, the suction side surface of the blade has higher heat/mass transfer coefficients and more complex distribution than the pressure side surface, which is related to the leakage flow. For all the tested Reynolds numbers, the heat/mass transfer characteristics on the turbine blade are the similar. The overall averaged $Sh_{c}$ values are proportional to $Re_{c}^{0.5}$ on the stagnation region and the laminar flow region such as the pressure side surface. However, since the flow is fully turbulent in the near-tip region, the heat/mass transfer coefficients are proportional to $Re_{c}^{0.8}.$