• Journal of Bio-Environment Control
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• v.28 no.3
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• pp.273-278
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• 2019

The multi-layer insulating curtains used in the experiment was produced in six combinations using non-woven fabric containing aerogel and compared and analyzed by measuring heat flux and heat perfusion rates due to weight, thickness and temperature changes. Using silica aerogel, which have recently been noted as new material insulation, this study tries to produce a new combination of multi-layer insulating curtains that can complement the shortcomings of the multi-layer insulating curtains currently in use and maintain and improve its warmth, and analyze the thermal properties. The heat flux means the amount of heat passing per unit time per unit area, and the higher the value, the more heat passing through the multi-layer insulating curtain, and it can be judged that the heat retention is low. The weight and thickness of multi-layer insulation curtains were found to be highly correlated with thermal insulation. In particular, insulation curtains combined with aerogel meltblown non-woven fabric had relatively higher thermal insulation than insulation curtains with the same number of insulation materials. However, the aerogel meltblown non-woven fabric is weak in light resistance and durability, and there is a problem that the production process and aerogel are scattering. In order to solve this problems, the combination of expanded aerogel non-woven fabric and hollow fiber non-woven fabric, which are relatively simple manufacturing processes and excellent warmth, are suitable for use in real farms.

• Journal of the Korean Institute of Gas
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• v.14 no.1
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• pp.37-41
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• 2010

The most important element for improving the process safety that occurs from the flare system installed to convert into safe materials by burning the inflammable or toxic gases within the process and this is specified in the API 521 Code so that the radiation does not cause a risk factor. The flames that occur from the flare stack holds the shape of jet fire due to the pressure and flow velocity of discharge gas. This study has identified the shape of flames by using the Chamberlain Model rather than the API 521 Code method, analyzing the radiation due to this.

• Journal of the Korean Society of Propulsion Engineers
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• v.10 no.4
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• pp.85-92
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• 2006

A design program has been developed to predict film cooling performance of a liquid rocket engine. A thermal protecting effect of low mixture ratio gas layer has been analysed by CFD. A one-dimensional film cooling model based on the CFD results has been implemented to the previously developed design program of regenerative cooling. Satisfactory agreement has been achieved by comparing the predicted maximum heat flux at the throat of a subscale chamber and the average measured value, and the predicted nozzle average heat flux and the measured value for a full scale chamber with film cooling. It is ascertained that the film cooling is effective to reduce the throat heat flux in rocket engine chamber.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05b
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• pp.461-466
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• 1996

원전에서 가상적인 중대사고 발생시 격납용기 하부 캐비티에서 고온의 노심용융물과 콘크리트와의 반응시 생성되는 기체의 종류 및 양, 콘크리트 침식율 및 주변 열전달 특성은 중대사고 연구의 쟁점으로 이에 대한 많은 연구가 수행되고 있다. 본 연구에서는 용융 유사물로 고온의 금속 용융물(SS304) 및 Thermite (Fe＋A1$_2$O$_3$)를 영광 3,4호기 원전에 사용한 콘크리트 시편에 부어 침식율, 생성가스 종류 및 주변 열전달 계수를 측정하였고 후에 MELCOR 로드내 MCCI 해석 부분인 CORCON MOD-3 코드와 비교할 계획이다. 본 논문에서는 MCCI scoping test의 실험 장치, 실험 방법 및 곁과를 소개하였다. 약 1$600^{\circ}C$ 의 SUS 304 용융물(10kg)은 충분치 않은 melt superheat와 용융물 이송과정시 열손실로 인해 침식이 거의 일어나지 않았으나, Thermite 실험에서는 측면 및 하부 방향으로 최대 2.7cm/min 의 침식율을 보였으며 하부방향으로의 최대 열유속은 약 3.1MW/$m^2$로 나타났다. 본 연구의 결과 및 실험 기술은 차세대 원전의 중대사고 완화를 위한 원자로 캐비티 설계 실증실험에 응용될 예정이다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.25 no.12
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• pp.1676-1683
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• 2001

An experimental study on condensation heat transfer characteristics of helically coiled spiral tubes was performed. The refrigerant is R-113. A refrigerant loop was established to measure the condensation heat transfer coefficients. Experiments were carried out uniform heat flux of 15 kw/m$^2$, refrigerant quality of 0.1∼0.9, curvature ratio of 0.016, 0.025 and 0.045. The curvature of a coil was defined as the ratio of the inside diameter of the tube to the diameter of the bending circle. To compare the condensation heat transfer coefficients of coiled spiral tubes, the previous results on coiled plain tubes and straight plain tubes were used. The results shows that the condensation heat transfer coefficients of coiled spiral tubes largely increase, as increasing Re and quality, compared to those of coiled plain tubes and straight plain tubes. As increasing degree of subcooling, however, the condensation heat transfer coefficients on coiled spiral tubes decrease. It is found that the heat transfer enhancement is more better than coiled plain tubes and straight plain tubes, as increasing curvature ratio.

• Proceedings of the Korea Institute of Fire Science and Engineering Conference
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• 2010.04a
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• pp.37-42
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• 2010

실제 규모 ISO 9705 표준 화재실에서 과환기(over-ventilated) 및 환기부족(under-ventilated) 화재에 대한 열 및 화학적 특성에 관한 실험이 수행되었다. 또한 FDS(Fire Dynamic Simulator)를 이용하여 수치적 예측성능에 대한 평가와 환기부족화재에서 건물 내부의 다차원 화재현상에 대한 해석이 이루어졌다. 과환기 및 환기부족화재의 특성은 연소효율, 총괄 당량비 뿐만 아니라 고온 상층부의 온도분포, 연소 생성물의 농도에 의해 명확하게 구분되었다. 실험결과와의 비교를 통해 과환기 및 환기부족화재에서 FDS는 공간내부의 온도, 열유속 및 다양한 화학종의 분포를 정량적으로 잘 예측함을 확인하였다. 과환기화재와 비교할 때, 환기부족화재에서 내부유동은 반대방향의 다차원 재순환 유동구조를 갖고 있음을 발견하였다. 동시에 공간내부의 $O_2$ 및 CO의 분포 역시 다차원 구조를 갖기 때문에 기존화재연구에서 측정되는 고온 상층부의 열 및 화학적 특성은 환기부족화재를 이해하는데 많은 한계가 있음을 확인하였다.

• Aerospace Engineering and Technology
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• v.3 no.1
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• pp.197-204
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• 2004

A design of regenerative cooling system of 30 ton level thrust combustion chamber for ground test has been performed. The 1-D design code has been validated by comparing with the heat flux of the NAL calorimeter for high chamber pressure and water-cooling performance of the ECC engine of MOBIS. The present design code has been confirmed to predict accurately the heat flux and water-cooling performance for high chamber pressure condition. The maximum hot-gas-side wall temperature is predicted to be about 720 K without thermal barrier coating and the coolant-side wall temperature is less than the coking temperature of RP-1. The coolant temperature rises nearly 100 K with thermal barrier coating when Jet-A1 is used as coolant.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.276-280
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• 2007

In this paper, heat transfer changes due to the shock/boundary layer interaction were investigated on surfaces where protruding bodies such as a cylinder and a secondary jet are mounted. With an infra-red thermography, surface temperature was measured and the measured data was used to obtain the convective heat transfer. Heat transfer phenomena around these two solid and fluid bodies were appeared to be very comparable each other. The inclination of a cylinder and the jet injection ratio were the important factors for the change of heat transfer on the effective surfaces.

• Proceedings of the Korean Nuclear Society Conference
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• 1997.10a
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• pp.784-789
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• 1997

원자력 발전소에서의 중대사고시, 고온의 노심 용융물이 원자로 공동으로 떨어지면 노심용융물과 콘크리트간의 반응(MCCI)에 의한 여러가지 현상으로 인해 격납용기의 건전성을 위협할 수 있다 본 연구에서는 국내 원전에서의 MCCI 현상에 대한 실험과 해석결과를 살펴보았다. 실험은 영광원전 3,4호기 원자로 공동구조물의 콘크리트를 대상으로 thermite 20kg을 사용한 것이며 해석은 MELCOR 코드내의 MCCI 상세해석 모듈인 CORCON-MOD3를 이용하였다. 해석에 사용된 콘크리트의 화학성분과 열물성은 실험을 통하여 측정한 값을 사용하였으며 해석결과는 실험 결과와 비교하였다. 또한 GORCON 코드에서의 MCCI 현상의 해석시 용융물의 초기온도, 용융물의 질량, 콘크리트의 종류에 따른 예측결과들을 비교하였다. MCCI 현상의 해석시 콘크리트의 종류에 따른 가스발생량과 구성성분의 변화가 크게 나타남으로 콘크리트의 화학적 구성성분을 적합하게 입력하여야 한다. 콘크리트로의 종류에 따른 하부로의 열유속은 크게 차이가 없으나 침식율은 크게 차이가 나며 이는 콘크리트의 상변화 잠열의 차이에서 기인한 것이다. CORCON 코드는 실험에 비해 작은 침식율을 예측하고 있으며 콘크리트의 침식율은 용융물의 양에 비해 초기온도의 변화에 더 큰 영향을 받는 것으로 예측하고 있다.

• Journal of the Korea Institute of Military Science and Technology
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• v.21 no.1
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• pp.74-85
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• 2018

This study has analyzed the convective heat transfer on the deck exposed to the high-temperature impingement exhausting from a VTOL vehicle. The heat flow of the impingement on the deck is modeled by the convection heat transfer. The convective heat flux generated by the hot impinging jet is investigated by using both convective heat transfer formulation and conjugate heat transfer formulation. Computational fluid dynamics(CFD) code was used to compute the heat flux distribution. The RANS equation and the k-e turbulence model were used to analyze the thermal flow of the impinging jet. The heat flux distribution near the stagnation zone obtained by the conjugate heat transfer analysis shows more reasonable than the convective heat transfer analysis.