• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.1
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• pp.61-70
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• 2019

A primary investigation on the underexpanded flow generated in a 0.4 MW class high enthalpy supersonic arc-heated plasma wind tunnel is conducted experimentally. The diameter and the position of the Mach disk from the nozzle exit is measured for overall pressure ratios ranging from 200 to 30. The empirical correlations for Mach disk diameter and position are determined which show very good agreement with experimental results.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 2003.05a
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• pp.567-572
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• 2003

하수슬러지로부터 재활용 가스 에너지를 얻을 수 있다. 슬러지 가스화의 공정 개발을 위해서는 초기에 휘발분이 방출되는 열분해 단계의 거동이 매우 중요하다. 열분해 생성물(가스, 타르, 촤 등)의 수율은 열분해 조건(가열속도, 체류시간, 온도, 압력, 가스분위기)뿐만 아니라 연료입자의 물리적 구조에 따라 좌우된다. 석탄의 경우에는 열분해과정에서 휘발분의 수율에 대한 상관식들이 많이 제시되었다.(중략)

• Aerospace Engineering and Technology
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• v.7 no.1
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• pp.40-48
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• 2008

Air mixing system which is composed of air pressure control system, hot pipe system and air mixer, is the facility for mixing hot air($1000^{\circ}C$, 10kg/s) from storage air heater (SAH) and decompressed air($20^{\circ}C$, 15kg/s) from high pressure air supply system. Air pressure control system reduce the pressure of the air, from 32MPa to 3.5 MPa and supply the decompressed air to air mixer. The hot pipe system supply hot air from SAH to air mixer which mix hot with the decompressed air from air pressure control system. Fully mixed air flow rate is 25kg/s and mixed temperature is up to $400^{\circ}C$. So, we can expand the operating envelop of the supersonic ground test facility to low Mach number and low altitude region.

• Proceedings of the KAIS Fall Conference
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• 2008.11a
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• pp.415-418
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• 2008

에탄올아민 (ETA; Ethanolamine)은 에틸렌옥시드를 진한 암모니아수와 함께 가열하여 얻어지는 물질로 흡수성이 있는 무색의 액체 또는 고체이며 탄소, 질소, 산소로 이루어진 매우 안정된 유기화합물이다. 이러한 ETA는 부식방지제, 산성가스 흡수제, 화장품 등 각종 산업에서 매우 유용하게 사용되는 물질이다. 하지만 ETA는 눈, 피부, 호흡기, 폐 등에 접촉하여 호흡기 질환 및 만성 천식을 유발하고 피부에 자극을 일으키므로 ETA를 제거하기 위한 물리화학적 연구가 필요하다. 따라서 본 연구에서는 냉각온도 및 진공펌프압력에 따른 ETA 응축 특성과, 흡착제에 따른 ETA 흡착특성을 조사하였다. 조사결과 ETA는 냉각수의 온도 및 진공펌프압력에 영향을 받았으며 냉각수 온도 및 진공펌프압력이 증가할수록 응축율은 감소하였다. ETA 흡착에서 활성탄의 경우 액상의 ETA와 상호간에 흡착력은 존재하지 않았으며, 기상의 ETA는 흡착되지만, $100^{\circ}C$이상에서 탈착 반응이 일어났다. 제올라이트의 경우 액상 및 기상의 ETA를 모두 흡착하였다.

• Proceedings of the KAIS Fall Conference
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• 2008.11a
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• pp.423-426
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• 2008

에탄올아민(ETA: Ethanolamine)은 탄소, 질소, 산소로 이루어진 유기화합물로 각종 산업에서 널리 사용되는 물질이다. 이러한 ETA는 상온에서는 휘발성을 띠지만 산 염기의 평형상수가 9.4 이므로 그 이하에서는 양이온 형태로 존재한다. 또한 수중에 존재할 경우 COD 및 T-N을 유발하는 물질이므로 이를 제거해야 한다. 따라서 본 연구에서는 수중에 존재하는 ETA를 제거하기 위해 온도, pH, 내부압력에 따른 ETA 증발 특성을 조사하였다. ETA증발 초기에는 끓는점의 차이로 인하여 물이 먼저 증발하며 일정시간 경과 후 농축된 ETA가 급격히 증발하였다. 내부압력이 낮아짐에 따른 ETA 수용액의 끓는점은 낮아졌으며 내부압력이 160mmHg이하일 때 가열온도에 영향을 받지 않고 ETA는 전량 증발하였다. 대기압 상태에서 ETA의 증발량은 pH에 영향을 받지만 진공상태에서는 ETA의 부분압이 낮아져 그 영향력은 매우 적었다.

• Journal of the Korean Society of Food Culture
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• v.16 no.4
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• pp.323-329
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• 2001

This study was carried out to observe the character change of expanded rice grain for Salyeotgangjung at various gelatinization methods. The expansion and structure change of rice grain was different at conditions of heating methods and gelatinization, respectively. The boiling showed good expansion compared to other heating methods by electric rice-cooker, pressure cooker, and steam cooker. There was not difference in expansion of rice grain between the boiling and the boiling after soaking. Rice grain did greatly expand as the boiling time was extended. But the quality for Salyeotgangjung would be not good because of crack of expanded rice grain surface when the boiling time was too long.

• Journal of the Mineralogical Society of Korea
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• v.16 no.2
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• pp.161-169
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• 2003

A phase transformation study on a synthetic amorphous diopside, $(Ca,Mg)SiO_3$has been carried out up to ∼30 GPa, and ∼$1000^{\circ}C$ using a diamond anvil cell and YAG laser heating system, respectively. A starting amorphous material shows a direct transition to cubic $(Ca,Mg)SiO_3$perovskite at high pressure, which contradicts to the crystalline diopside phase transformation sequence disproportionating into mixtures of the orthorhombic$ MgSiO_3$perovskite and the cubic $CaSiO_3$perovskite phases. This discrepancy might be due to the different starting materials as well as the temperature variations at each specific experiment performed. The present phase transfor mation sequence would modify the mineralogical assemblage in the Earth transition region and the lower mantle depending upon the pressure, temperature and the oxygen partial pressure.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.14 no.12
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• pp.6072-6081
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• 2013

In this study, experiments were performed on air heater samples with three different shapes (chevron, wave and dimple type) to reduce the plumes from cooling towers. The tests were conducted for a range of frontal air velocities of 1~3 m/s and water flow rate 0.19~0.33 kg/s. The results showed that the heat transfer rate increased with increasing air velocity or water flow rate. The air-side pressure drop also increased with increasing air velocity. At the same frontal air velocity, the highest heat transfer rate was obtained for the chevron sample (1.5~1.7 times compared to that of the plate sample), followed by the dimple, wave and plate samples. The heat transfer rate per unit power consumption was also 15% larger than that of the dimple sample. On the other hand, there was no noticeable difference between the other samples.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.2
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• pp.15-22
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• 2011

Unlike most aerodynamic wind-tunnel, Scramjet Engine Test Facility(SETF) of Korea Aerospace Research Institute should simulate enthalpy condition at a flight condition. SETF is a blow-down type, high-enthalpy wind tunnel. To attain a flight condition, a highly stagnated air comes into the test cell through a supersonic nozzle. Also, an air ejector of the SETF is used for simulating altitude conditions of the engine, and facility starting. SETF has a free-jet type test cell and this free-jet type test cell can simulate a boundary layer effect between an airplane and engine using facility nozzle, but it is too difficult to predict the nature of the facility. Therefore it is required to understand the starting characteristics of the facility by experiments. In this paper, the starting characteristics of the SETF and modifications of the ejector are described.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.451-458
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• 2010

Unlike most aerodynamic wind-tunnel, Scramjet Engine Test Facility(SETF) of Korea Aerospace Research Institute should simulate enthalpy condition at a flight condition. SETF is a blow-down type, high-enthalpy wind tunnel. To attain a flight condition, a highly stagnated air comes into the test cell through a supersonic nozzle. Also, an air ejector of the SETF is used for simulating altitude conditions of the engine, and facility starting. SETF has a free-jet type test cell and this free-jet type test cell can simulate a boundary layer effect between an airplane and engine using facility nozzle, but it is too difficult to predict the nature of the facility. Therefore it is required to understand the starting characteristics of the facility by experiments. In this paper, the starting characteristics of the SETF and modifications of the ejector are described.