• 터널과지하공간
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• 제12권3호
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• pp.142-151
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• 2002

대전 식품냉동저장창고 파일럿 공동주위의 거리에 따른 비정상상태의 온도 분포를 산정하기 위해 Claesson(2001)의 해석해 및 Dirichlet과 Neuman 내부 경계조건을 갖는 수치모델들을 검토하였다. 온도 강하 단계동안 일정 표면 온도 경계조건에 기초하고 있는 Claesson의 해석해를 활용한 결과, 실제 암반에서의 온도 계측결과를 오차 평균 0.89$^{\circ}C$ 수준으로서 비교적 정확히 예측할 수 있었는데, $0^{\circ}C$근처의 실험실 암석 열물성을 입력하였고 현지 암반 조건을 표현하기 위한 특별한 물성 보정을 하지 않았다. 내부 공동 암반 벽면을 통한 열유속을 갖는 수치해석의 경우, 대류 열전달계수와 공동 내부 온도가 냉각시간에 따라 변화하기 때문에 경계조건을 가하기 어려운 단점을 극복하기 위해 새로운 경계조건 설정 기법을 제안하였다. 그 결과 오차 평균 1.58$^{\circ}C$의 수준으로서 온도 계측치와 부합하였다. 또한 공동 벽면에서 고정 온도 조건을 갖는 수치해와 비교하였다. 마지막으로 Claesson의 해석해 및 다양한 내부 경계조건을 갖는 수치모델을 활용하여, 공동 주변의 온도 분포를 정확히 예측할 수 있는 일련의 해석 단계 프로그램을 제안하였다.

• 한국수소및신에너지학회논문집
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• 제21권4호
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• pp.258-263
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• 2010

A numerical stack model has been developed to predict the temperature at a constant-load operation of molten carbonate fuel cell stacks. For the validity of the model, the simulated results with several boundary conditions were compared in the cell temperature data obtained from 75 kW class MCFC stack operation. It was shown that the simulated results with the existing boundary condition, which the stack outlet temperature was fixed at $650^{\circ}C$, didn't match well with the measured data. On the other hand, the stack model with the outlet temperature modified by the outlet manifold temperature measured from the stack under several electric loads was found to explain the measured cell temperature distribution well. The results show that the model can be used to predict the cell temperature distribution in the stacks by the measurement of the manifold outlet temperature.

• Journal of Advanced Marine Engineering and Technology
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• 제30권6호
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• pp.709-715
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• 2006

The effects of thermal cycle condition and applied stress on the intergranular corrosion in austenitic 316 type stainless steels were investigated. Specimens were solution-treated at 1100$^{\circ}C$ for one hour and then sensitized in the temperature range of $500{\sim}800^{\circ}C$ by holding $2{\sim}300s$ with a various applied stresses of $0{\sim}8kg/mm^2$. Degree of sensitization. DOS %, was measured through polarization curve by electrochemical DL-EPR test. Microstructural observations were also conducted DOS % increased with an increase of sensitization temperature and/or holding time. Increase of applied stress resulted in increase of DOS % and more corroded surface because of acceleration of intergranular corrosion and fine grain size due to the stress. Cr depleted zone near grain boundary was observed. The amount of depletion was profounded with an increase of sensitization temperature, holding time and applied stress. $M_{23}C_6$ carbides were precipitated discontinuously at grain boundary. However, its amount was relatively small in the thermal cycle condition of 800$^{\circ}C$, 300sec and 4kg/mm$^2$.

• 한국화재소방학회논문지
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• 제24권6호
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• pp.69-75
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• 2010

콘크리트가 충전된 각형강관 기둥(CFT)은 외부에 강재가 노출된 형상으로 외측의 강관은 화재시 급격한 온도상승으로 인해 강도가 저하되나, 내부의 콘크리트는 열용량이 큰 재료로써 내화성능을 확보할 수 있는 구조로 구성되어 있다. CFT 기둥을 내화구조로서 적용하기 위해서는 구조적 성능에 영향을 미치는 인자에 대한 연구가 필요하며, 이에 대한 조건별 영향성에 관한 연구가 필요하다. 내화성능에 영향을 주는 주요인자는 콘크리트 압축강도.단면크기.축력비.경계조건이며, 그 중 기둥과 보의 경계조건은 구조적 측면에서 하중지지능력에 영향을 미치므로 내화성능을 지배하는 주요 인자 중에 하나이다. 실험결과 360단면에서는 양단 고정조건에서는 106분의 내화성능이 확보되나 양단 힌지 조건에서는 89분의 내화성능을 확보하는 것으로 나타났다. 280단면에서는 양단 고정조건에서는 113분의 내화성능이 확보되나 양단힌지 조건에서는 78분의 내화성능을 확보하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.1358-1363
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• 2004

The objective of this work is to propose calibration facility in which a thin film type heat flux sensor can be calibrated under convective flow condition by using a small wind tunnel with the constant temperature plate condition. A small wind tunnel has been built to produce a boundary layer shear flow above a constant temperature copper plate. 12-independent copper blocks, thin film heaters, insulators and temperature controllers were used to keep the temperature of flat plate constant at a specified temperature. Three commercial thin film-type heat flux sensors were tested. Convective calibrations of these gages were performed over the available heat flux range of $1.4{\sim}2.5kW/m^2$. The uncertainty in the heat flux measurements in the convective-type heat flux calibration facility was ${\pm}2.07%$. Non-dimensional sensitivity is proposed to compare the sensitivity calibrated by manufacturer and that of experiment conducted in this study.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2006년도 하계학술발표대회 논문집
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• pp.1255-1260
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• 2006

This present study analyzed temperature depreciation ratio of window inside surface by KS F 2295 'Procedure for determining fenestration product condensation resistance values'. it estimated window indoor surface condensation due to variable environmental condition. Performance of condensation resistance by using temperature depreciation ratio until applied Low-e and Ar glazing improved about 45% from 24 mm clear. Temperature depreciation ratio by KS F 2295 considers analytic index of window condensation due to variable boundary condition.

• 대한기계학회논문집A
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• 제25권12호
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• pp.1911-1918
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• 2001

Recently the non-destructive test technique which uses the grain boundary etching characteristics owing to the variation of material structures has been proposed. However, during in-serviced GEM test there are a lot of variables such as the changes of temperature and concentration of etching solution, the roughness condition of surface polished etc.. The purpose of this paper is to investigate the influences of these test variables on GEM test results in order to establish a reliable and sensitive of GEM evaluation technique. The experiments are conducted in various solution temperatures, 10$\^{C}$, 15$\^{C}$, 20$\^{C}$, and 25$\^{C}$ and in 70% and 100% concentrations of that, and in various surface roughnesses polished by #800, #2000, and 0.3㎛ alumina powder. Through the test with variables, it is verified that the decrease of temperature and concentration of etching solution and the coarsened surface roughness by not using polishing cloth and powder induce some badly and/or greatly influences on GEM test results like grain boundary etching width(W$\_$GB) and intersecting point ratio(N$\_$i/N$\_$0/). Therefore, to get reliable and good GEM test results, it must be prepared the surface of specimen polished by polishing cloth and 0.3㎛ alumina powder and the saturated picric acid solution having 25$\^{C}$ and be maintained the constant temperature(25$\^{C}$) during GEM test.

• Journal of Advanced Marine Engineering and Technology
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• 제40권5호
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• pp.412-417
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• 2016

A fin of finite width with infinitely small thickness is assumed to be placed horizontally between two horizontal parallel plates of infinite extension in the exactly central position. The lower plate and the half of the upper plate are kept at a constant lower temperature, and the remaining upper plate is kept at a constant higher temperature. The fin is also kept at a constant temperature (variable). Steady-state two-dimensional laminar natural convection is analyzed as a problem of boundary value under a boundary-fitted conformal mapping system, using a spectral finite difference scheme, with a condition of doubly-connectedness. The steady-state solution is obtained as a limit of the transient solution.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.282-289
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• 2000

Direct numerical solution for flow and heat transfer for Benard convection with a body is obtained using an accurate and efficient Fourier-Chebyshev collocation and multi-domain method. The flow and temperature fields are obtained fur different Rayleigh numbers and thermal boundary conditions of body. The body has adiabatic and constant temperature conditions. The existence of a body gives different flow and heat transfer fields in the system, compared to pure Benard convection. The flow and temperature fields are also affected by the thermal boundary condition of a body.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2002년도 추계 학술대회논문집
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• pp.109-113
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• 2002

Numerical analysis of aerodynamic heating for KPSAM is performed using aerodynamic heating model suitable to KPSAM, which has complex flow field resulting from the spike attached to the dome, such as large separation area and the strong shock/boundary layer interaction region around reattachment point on the dome. The aerodynamic heating model is validated and modified through the comparison between the flight test measurement and the thermal analysis results. TFD temperature sensors are installed on the dome to measure surface temperature during the flight. Computation results, obtained from the heat transfer analysis on the sensors, agree well with flight test data. The aerodynamic heating model provides heat transfer rate into surface as a boundary condition of unsteady 1D/axisymmetric thermal analysis on the missile structure. The axisymmetric thermal analysis using FLUENT is more versatile than the 1D analysis and can be applied to the heating problem related with complex structures and multi-dimensional heat transfer problems such as prediction of temperature rise at contact surface of different materials.