• Nuclear Engineering and Technology
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• 제26권2호
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• pp.265-276
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• 1994

FLECHT-SEASET 실험에 대한 REIAP5/MOD3 평가시에 밝혀진 코드결함을 수정하기 위하여 RELAP5/MOD3 재관수 모델을 개선하였다. 모델개선은 재관수 열전달 모델의 수정과 분산유동영역의 액적 크기의 조절을 통하여 이루어졌으며 재관수 계산시 발생되는 압력 spike와 수위진동 등의 결함을 개선하기 위하여 벽면비등모델의 time-smoothing과 천이 유동시의 level tracking모델도 첨가되었다. FLECHT-SEASET 실험에 대한 개선모델의 검증과 발전소의 대형냉각재 상실 사고해석 응용에서 코드결함이 개선되었음을 알 수 있었다.

• 대한기계학회논문집
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• 제8권1호
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• pp.18-25
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• 1984

The transition boiling of a liquid droplet on a heated flat surface was studied utilizing Kotake's model with the effects of viscosity of a thin vapor layer between the droplet and the hot plate taken into account. This problem was analyzed considering the process of the droplet evaporation which resulted in hydrodynamic instability at the liquid-vapor interface. The results of the study are as follows; (1)The effect of the viscosity in the vapor layer at the interface appears as a dimensionless number N, namely .sigma. .delta.$_{0}$ /.rho.nu.$^{2}$ (2)The time required for evaporation at the transitional region increases with the temperature difference ratio .DELTA. T$_{r}$. The rate of increase of the total evaporation time becomes larger as increasing of N$_{m}$(N number at maximum heat flux) increases.s.

• 한국유체기계학회 논문집
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• 제12권1호
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• pp.51-56
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• 2009

The detailed heat transfer coefficient on a rotating dimpled channel were measured using the transient liquid crystal technique. The channel height to dimple diameter was 2, dimple center distance to dimple diameter was 1.5 and channel aspect ratio was 4. Tested Reynolds number based on the channel hydraulic diameter was varied from 15000 to 35000 and corresponding rotation number was ranged from 0.026 to 0.057. Results showed that the Coriolis force by rotation enhanced the heat transfer coefficient on the trailing surface. As the Reynolds number increased, i.e. rotation number decreased, the heat transfer coefficient increased and the thermal performance factor decreased.

• 유변학
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• 제1권1호
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• pp.71-79
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• 1989

임계연신비로 특징지어지는 비등온 방사공정에서의 Draw Resonance 발생을, White 의 변형속도에 따라 변하는 물질의 이완시간 모델에 의한 convected Maxwell 유체의 방사 모형을 사용해서 연구했다. 임계연신비의 계산에는 다른 연구자들이 이용하는 통상의 복잡 한 수치계산인 eigenvalue 방법을 쓰지 않고 전파하는 동적 waves 에 근거한 간단한 Hyun 의 이론을 사용했다. 그 결과 Staton Number와 냉각 공기온도로서 나타내지는 방사공정의 냉각이 공정을 안정시킨다는 것이 밝혀졌다. 다시 말해서 연신점도가 변형후화인 유체이거 나 변형박화인 유체이거난 상관없이 항상 Stanton Number가 켜지거나 또는 냉각공기온도 가 낮아질수록(즉냉각효과가 커질 때) 임계연신비가 커지는 것이다(단변형박화 dvcp의 빌부 구간을 제외하고) 한편 Draw Resonacnce 에 미치는 냉각의 효과는 무차원 이완시간(a Weissenberg Number 혹은 a Deborah number)이 커질수록 작아진다는 것도 발견됐다. 이 것은 process Time 이 작아지면 열전달이 작아지기 때문이다. 이러한 내용들은 다른 연구 자들의 결과와도 잘 부합된다.

• Tribology and Lubricants
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• 제22권4호
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• pp.173-181
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• 2006

In the present study, we developed a numerical analysis software to predict performance of tilting-pad thrust bearings. The finite element method was adopted to compute lubricant film pressure and temperature. Three-dimensional heat transfer equations were solved simultaneously for the lubricant film, pad, and runner. Groove temperature was assumed with two different models. From application of the software to a thrust bearing, it has been seen that the three-dimensional analysis predicts higher temperature than the average temperature analysis. It has also been found that the groove model with a hot-oil-carry-over factor predicts higher temperature.

• 한국건축시공학회:학술대회논문집
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• 한국건축시공학회 2010년도 춘계 학술논문 발표대회 1부
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• pp.219-220
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• 2010

The purpose of this study is to evaluate chloride ion attack durability of concrete structure having experienced the high temperature fire. Mechanical properties and anti chloride ion diffusivity of concrete specimens were measured which have experienced of 2 hours heating at $200{^{\circ}C},\;400{^{\circ}C},\;600{^{\circ}C},\;800{^{\circ}C}$. The coupling FE model of thermal transfer and chloride ion diffusion was built to predict the life expectancy of RC structure using the property values by a series of experiment.

• 한국유체기계학회 논문집
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• 제13권3호
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• pp.30-36
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• 2010

The detailed heat transfer coefficients on a rotating dimpled channel were measured by the hue detection based the transient liquid crystal technique. The dimples were fabricated on the one side of the channel and the tested channel aspect ratio was 4, 6, and 12 with fixed channel width. Tested Reynolds number based on the channel hydraulic diameter was varied from 21,000 to 47,000. A stationary case and two different rotating conditions were tested so that the dimple fabricated surface became leading or trailing surface. For all rotating conditions, the minimum averaged heat transfer coefficient was measured for the channel aspect ratio of 6. Generally, the highest averaged heat transfer coefficient was observed for the highest aspect ratio cases due to increased dimple induced vortex strength.

• 대한기계학회논문집B
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• 제30권4호
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• pp.328-336
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• 2006

Detailed heat transfer coefficient distributions an two. types of gas turbine blade tip, plane tip and squealer tip, were measured using a hue-detection base transient liquid crystals technique.. The heat transfer coefficients an the shroud and near tip regions of the pressure and suction sides af the blade were also. measured. The heat transfer measurements were taken at the three different tip gap clearances af 1.0%, 1.5%, and 2.5% of blade span. Results shaw the overall heat transfer coefficients on the tip and shroud with squealer tip blade were lower than those with plane tip blade. By using squealer tip, however, the reductions af heat transfer coefficients near the tip regions of the pressure and suction sides were nat remarkable.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 1992년도 제16회 학술강연회초록집
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• pp.13-18
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• 1992

대형 틸팅패드 저어널베어링은 고속안정성 특성이 우수한 베어링으로서 시스템의 안정성이 매우 중요시되는 터빈발전기 등 대형 고속 회전기계에 많이 사용되고 있다. 그런데 이들 대형 저어널베어링에서는 유막의 온도상승이 매우 많고, 유체의 흐름이 거의 난류영역에 이르기 때문에 베어링의 운전특성을 정확하게 예측하기가 어려운 실정이다. Hopf & Schuler는 대형 틸팅패드 저어널베어링에 대한 실험적 연구에서 유동상태에 따라 베어링의 온도분포가 서로 달라진다고 발표하였다. 대형 틸팅패드 저어널베어링은 구조적으로 유동상태가 복잡할 뿐만 아니라 계산과정도 까다로운 편이어서 온도상승과 난류를 고려하여 엄밀하게 운전특성을 예측한 연구는 거의 없다. 따라서 본 연구에서는 대형 틸팅패드 저어널베어리으이 운전특성을 보다 엄밀하게 예측하기 위하여 3차원 적으로 유막의 점도변화 및 패드에서의 열전달을 고려하고, 와점성계수를 이용한 난류윤활이론을 사용하여 유막의 온도상승 및 난류가 베어링의 온도분포, 부하능력, 마찰손실 등의 운전특성에 미치는 영햐을 보다 엄밀하게 제시하고자 한다.

• 한국항공운항학회지
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• 제14권2호
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• pp.33-38
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• 2006

Heat transfer coefficients and static pressure distributions on a gas turbine vane endwall were experimentally investigated in a 5 bladed linear cascade. The Reynolds number based on an axial chord length and the cascade exit velocity was 500,000. Both heat transfer and pressure measurements on the vane endwall were made at the two different turbulence intensity levels of 6.8% and 10.8%. Detailed heat transfer coefficient distributions on the vane endwall region were measured using a hue detection based transient liquid crystals technique. Results show various regions of high and low heat transfer coefficients on the vane endwall surface due to several types of secondary flows and vortices. Heat transfer coefficient and endwall static pressure distributions showed similar trends for both turbulence intensity, however, the averaged heat transfer coefficients for higher turbulence intensity case was higher than the lower turbulence intensity case by 15%.