• Proceedings of the Korean Vacuum Society Conference
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• 2012.02a
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• pp.116-116
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• 2012

위성의 발사, 천이궤도, 운영궤도 등에서 위성체에 주어지는 극한 온도와 진공상태에서 위성체와 열제어시스템이 요구 조건을 만족시키는가를 확인하기 위하여 열진공시험을 수행한다. 우주에서 일어나는 환경변화는 극도로 심해서 지상에서 이와 유사한 열적 환경을 모사하는 방법은 쉽지가 않고, 일반적으로 위성체에 대한 열진공/평형 시험을 위해서는 열유속 흡수법과 열유속 투사법의 두 가지 방법을 사용한다. 한국항공우주연구원에서는 종래 접촉식 히터를 위성체에 직접 부착하는 방법에서 탈피하여 새로이 IR Lamp를 이용한 열유속 흡수법을 이용하여 위성체에 계산된 열유속을 인가하는 방법으로 위성체 열진공/평형시험을 수행하였으며, IR Lamp는 요구되는 100W~400W 사이의 열량을 오차 범위 5% 이내로 인가하여 균일한 온도 분포를 유지하고 성공적인 시험을 수행하였다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.39 no.12
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• pp.953-963
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• 2015

There is an increasing need to understand the thermal-hydraulic phenomena, including the critical heat flux (CHF), in narrow rectangular channels and consider these in system design. The CHF mechanism under a saturated flow boiling condition involves the depletion of the liquid film of an annular flow. To predict this type of CHF, the previous representative liquid film dryout models (LFD models) were studied, and their shortcomings were reviewed, including the assumption that void fraction or quality is constant at the boundary condition for the onset of annular flow (OAF). A new LFD model was proposed based on the recent constitutive correlations for the droplet deposition rate and entrainment rate. In addition, this LFD model was applied to predict the CHF in vertical narrow rectangular channels that were uniformly heated. The predicted CHF showed good agreement with 284 pieces of experimental data, with a mean absolute error of 18. 1 % and root mean square error of 22.9 %.

• Nuclear Engineering and Technology
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• v.20 no.2
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• pp.112-119
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• 1988

The purpose of this work is to obtain the experimental data for the forced How dryout heat flux in a heat generating stratified debris bed which simulates the degraded nuclear reactor core after severe accident. The present observations were mainly focused on the effect of coolant mass flux on the dryout heat flux in the stratified debris bed which consists of several layers with selected particle sizes under constant bed depth and temperature of inlet coolant flow conditions. The following results were obtained from this experimental work: (1) The dryout heat flux in the stratified debris bed increases with increase of upward forcing mass flux of coolant. The similar trend of increase rate of dryout heat flux in the stratified bed was observed in the uniform particle size bed. (2) For the comparison of theoretical values and experimental data, the use of surface area mean diameter as a particle diameter was suitable for the calculation of dryout heat flux.

• Proceedings of the Korean Nuclear Society Conference
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• 1999.05a
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• pp.166-166
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• 1999

• Proceedings of the Korean Nuclear Society Conference
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• 2002.05a
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• pp.116-116
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• 2002

• Journal of Energy Engineering
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• v.18 no.2
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• pp.108-113
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• 2009

An experimental study of jet impingement on aluminum foam mounted on the surface with constant heat flux is conducted with the presentation of the heat transfer rate measured when jet impinges normally to a flat plate. Effects of pore density, foam thickness and Reynolds number on the heat transfer are analyzed. Experimental results show that the significant enhancement in Nu is obtained when the aluminum foam is mounted on the heated plate and that the increase in the heat transfer due to the porous material insertion is dominated by both the increase in the heat transfer area and the decrease in the momentum flux resulted from the pressure drop.

• Transactions of the Korean Society of Mechanical Engineers
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• v.18 no.7
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• pp.1799-1807
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• 1994

Natural convection from a slightly inclined circular cylinders immersed in quiescent cold pure water was studied experimentally. The experiment was carried out for circular cylinders with uniform heat flux ranging from $100W/m^{2} to 800 W/m^{2}$ and inclined angle ranging from horizontal $({\phi}=0^{\circ}) to 15^{\circ}$. The flow fields around cylinder were visualized and heat transfer characteristics investigated by measuring the surface temperatures for each case. As the results, it is shown that flow patterns are changed consecutively through the sequence of steady state downflow, unsteady state flow and steady state upflow with increasing heat flux. At the same inclined angle, as heat flux increases, the average Nusselt number decreases and then increases. At the same heat flux, as inclined angle increases, the average Nusselt number decreases.

• Fire Science and Engineering
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• v.10 no.3
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• pp.51-57
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• 1996

반응시간지수(Response Rime Index : RTI)를 사용하여 스프링클러의 열응답(thermal response) 특성을 분류할 수 있다. 반응시간지수는 plunge test에서 균일한 고온의 공기속도의 제곱근과 스프링클러 열감지부의 시정수(time constant)의 곱으로 나타낼 수 있다. 고온의 주위 공기온도에서 스프링클러가 작동하는 시간을 측정하므로서 열감지부의 시정수를 계산할 수 있다. 스프링클러의 RTI가 시정수에 비하여 실험조건에 따른 변화 폭이 적으므로 실제 화재시의 스프링클러 자동시간을 예측하는데에는 RTI가 사용된다. 스프링클러의 작동시간 예측을 위해서는 RTI값과 스프링클러 열감지부 주위의 유속이 필요하며, 유속은 화재의 발열량과 스프링클러가 설치된 구획의 높이로부터 실험식으로 결정된다. 따라서 Plunge test를 이용하여 얻은 스프링클러 열감지부의 기본자료로부터 실화재시의 스프링클러 작동시간을 예측하게 되며, ZONE 모델과 같은 화재 simulation 프로그램과 같이 사용된다면 스프링클러 작동시의 연층의 높이도 예측 가능하게 된다.

• Proceedings of the Korean Nuclear Society Conference
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• 1999.05a
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• pp.165-165
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• 1999

• Proceedings of the KSME Conference
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• 2000.04b
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• pp.290-295
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• 2000

An experimental study was carried out in a cavity with upper channel and square heat surface by visualization equipment with Mach-Zehnder interferometer and laser apparatus. The visualization system consists of 2-dimensional sheet light by Argon-Ion Laser with cylindrical lens and flow picture recording system. Instant simultaneous velocity vectors at whole field were measured by 2-D PIV system(CACTUS'2000). Obtained result showed various flow patterns. Severe unsteady flow fluctuation within the cavity are remarkable and sheared mixing layer phenomena are also found at the region where inlet flow is collided with the counter-clockwise rotating main primary vortex. Photographs of Mach-Zehnder are also compared in terms of constant heat flux.