• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.4
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• pp.61-68
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• 2015

Reactive sprays of two propellant combinations(GOx/kerosene and $GN_2O$/ethanol) were observed and compared with each other as a basic research of visualizing supercritical combustion. A shadowgraph imaging method was used to visualize the reactive sprays, and shadowgraph images were converted to density gradient magnitude images to analyse the structure of reactive sprays. The gas-liquid interface of GOx/kerosene spray showed rougher boundary and steeper density gradient near the injector face than the $N_2O$/ethanol at similar combustion chamber pressure. Spray core length was calculated from averaged density gradient magnitude images and it was revealed that spray core length of GOx/kerosene was shorter than that of $GN_2O$/ethanol, although momentum flux ratio of GOx/kerosene propellant combination was lower.

• Journal of Biomedical Engineering Research
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• v.24 no.5
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• pp.391-399
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• 2003

Intravascular oxygenation represents an attractive. alternative support modality for therapy originated with acute respiratory distress syndrome(ARDS). However. the clinical study concluded that more gas exchange was needed for intravascular oxygenation to be clinically effective in ARDS treatment. In this study, we tried to enhance gas exchange on the VIVLAD using microencapsulation of hemoglobin and perfluorocarbon emulsion(PFC emulsion). Blood gas measurements were performed by collecting blood samples from the arterial and venous sides of the circuit, and processing them in a blood/gas analyzer. The function of hemosome. blood/hemosome mixed solution. and blood/PFC emulsion mixed solution were tested by an oxygen dissociation curve using a blood/gas analyzer. As a result, it was shown that the oxygen transfer of hemosome and blood/hemosome mixed solution were higher than that of whole blood. Also. it showed that the carbon dioxide transfer of whole blood/PFC emulsion mixed solution was higher than that of others. Therefore, we determined that hemosome and PFC emulsion could increase oxygen transfer and carbon dioxide transfer. respectively.

• Journal of the Korean Chemical Society
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• v.43 no.2
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• pp.150-155
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• 1999

The ignition delay times behind reflected shock waves in $C_2H_6-O_2-Ar$ systems containing $CH_3Cl$ were measured for the range of temperatures between 1270 and 1544 K. The measurements indicated that $CH_3Cl$ inhibited the ignition of ethane ignition and the inhibition effects increased with increasing $CH_3Cl$ concentration. To clarify the inhibition effects of $CH_3Cl$ from the viewpoint of the reaction mechanism, computational analyses were performed in $C_2H_6-CH_3CI-O_2-Ar$ mixtures.

• Journal of Advanced Marine Engineering and Technology
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• v.35 no.2
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• pp.216-223
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• 2011

TVC is a kind of ejector which entrains low pressure working fluid by using the high pressure working fluid. While most papers relating with ejectors treat the working fluid as an ideal gas for convenience, the fluid doesn't behave as the ideal gas when phase change occurs. In this study, numerical analysis is conducted by applying Redlich-Kwong equation of state instead of ideal gas equation of state. Two turbulent models are compared for the better prediction and SST k-${\omega}$ model is preferred rather than realizable k-${\epsilon}$ model by comparison. Energy loss at the diffuser inlet and throat using the real gas equation of state is relatively greater than that using ideal gas law. For the real gas case, pressure increase due to shock train at the diffuser outlet is relatively smaller than the ideal gas case, but both cases have the same pressure increase due to a pseudo shock.

• Membrane Journal
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• v.16 no.2
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• pp.144-152
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• 2006

Elastomer-clay nanocomposite membranes were prepared by melt intercalation mothod with internal mixer. We are used NMR, Ionomer, SEBS (Styrene Ethylene Butadien styrene Copolymer) as elastomer, and modified clay. Gas barrier property of the elastomer-clay nanocomposites membranes were investigated by a gas permeability of $CO_2,\;O_2,\;N_2$ at room temperature. Gas permeability through the elastomer-clay nanocomposite membranes increased due to increased tortuosity made by intercalation of clay in elastomer.

• Microbiology and Biotechnology Letters
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• v.1 no.1
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• pp.25-30
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• 1973

Experiments were carried out to clarify changes of intercellular gas composition, respiration and ethylene evolution by controlled external atmospheric pressure and external gas composition on apples. Jonathan apples, harvested 25, in September and Rolls apples, harvested 25, in October, 1971 and 1972 were used. Results obtained were as follows: 1. Intercellular gas volumes were proportionally changed by the given pressure, and the given pressure remarkably affected internal gas composition and volume of apples. As intercellular gas volumes were reached in their equilibrium within 5 min. after treatment, the internal atmospheric conditions became constant rapidly. 2. The increase of internal $CO_2$ production was co-related with an amount of internal $O_2$ consumption, therefore, the decreasing period of internal $O_2$ consumption was equalled to the period of climacteric rise in respiration. 3. The increasing of $CO_2$ production followed evolution of $C_2$H$_4$ and this phenomenon on SAP part. was subsequent to NAP part 4. In sub-atmospheric storage, CA effect was also obtained by control of low $O_2$ and high $CO_2$ concentration.

• Proceedings of the Korean Vacuum Society Conference
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• 2011.08a
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• pp.86-86
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• 2011

첨단 공정이 필요한 반도체와 LCD, PDP, LED 등의 디스플레이 및 IT 부품을 제조하는데 필요한 장비의 고성능화와 작업환경의 고청정화에 따른 초고진공펌프의 수요 확대와 앞으로 전개될 한-미 FTA에 따른 시장 확대로 인해 크라이오펌프의 국산화가 시급한 실정이다. 고성능 크라이오펌프를 만들기 위해서는 냉각판을 극저온으로 냉각하기 위한 극저온 냉동기 개발도 중요하지만 냉각판(cryoarray)에 최대한 많은 분자를 포획시키는 것 또한 최우선적으로 고려되어야 할 사항 중 하나이다. 이에 본 논문은 크라이오펌프용 냉각판의 기체분자 포획능력에 대하여 연구하였다. 냉각판의 분자포획능력의 해석은 형상계수법(view factor method)을 이용해 수행하였다. 해석에 이용한 냉각판은 현재 상용화된 모델들 중 원형 중앙판에 45$^{\circ}$ 하향 skirt가 달린 형태이며 8장의 냉각판이 일정한 간격을 두고 아래쪽으로 적층되어있고 이를 기본 모델로 하여 skirt의 형상이 다른 3장의 냉각판을 가진 네 가지 모델을 해석하였다. 해석에 이용한 냉각판의 기체분자 포획능력이 구속된 형상에서 얼마나 우수한가를 알아보기 위해 크라이오펌프의 입구 직경과 냉각판 중앙 원판의 직경비, 냉각판 사이의 거리, 그리고 skirt의 길이를 변화시켜가며 극저온 냉각판에 직접 응축되는 typeII가스와 흡착제가 도포된 부분에 의해 흡착되는 typeIII가스로 분류하여 해석을 수행하고 그 결과를 비교, 분석하였다. 크라이오펌프의 입구 직경과 냉각판 중앙 원판의 직경비가 증가함에 따라 typeII가스와 typeIII가스 모두 기체분자 포획능력이 증가하며 극저온 냉각판 사이 거리의 변화에 따른 기체분자 포획능력은 typeII가스의 경우 극저온 냉각판 사이의 거리가 증가할수록 증가한다. 하지만 typeIII가스는 모델 A, C의 경우 증가하고 모델 B, D의 경우 증가하다가 다시 약간 감소한다. skirt 길이 변화에 따른 기체분자 포획능력은 두 가스 모두 skirt 길이가 증가함에 따라 점점 급격하게 증가하고 모델 B, D는 나머지 두 모델에 비해 큰 값을 갖는다. 기체분자 포획능력을 해석한 결과를 실제 배기속도와 비교할 경우 절대적 수치로써의 비교는 어려우나 각 모델의 형상의 차이에 의한 상대적인 비교는 가능하다.

• Membrane Journal
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• v.25 no.2
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• pp.162-170
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• 2015

In this study, gas permeability of polyimide materials having a various amine group was measured and molecular dynamics was used to analyze the dynamic characteristics of the gas molecules in the polyimide by calculating the position and velocity of the gas molecules with change of the time. The gas permeability of polyimide membrane having substitution site which increase free volume in the polymer was increased. However, polyimide with rigid structure showed decreased gas permeability. As a result of analyzing the change in the gas permeation behavior using molecular dynamics simulations, we confirmed that the results show the same tendency with actual measurements of the gas permeability.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.9
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• pp.723-734
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• 2018

A structural weight estimation methodology for the multicopter design process is presented. In general, a multicopter is composed of an airframe, motors, propellers, battery and so on. Among these, the weight of motors, propellers and battery can be obtained from the weight trends with respect to design parameters. However, the structural weight is hard to be estimated due to the various configurations and design concepts of multicopters. Moreover, the airframe weights of most commercial multicopter products are not provided. Thus, an accurate airframe weight model is required for the reliable mutlcopter design process. Firstly, the standard configuration of multicopters is defined. Then, we proposed the structural weight estimation method using the number and diameter of propellers determined from the initial step of sizing process. Finally, we validated our suggested method using the commerical products.

• Journal of Nuclear Fuel Cycle and Waste Technology(JNFCWT)
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• v.8 no.3
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• pp.229-238
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• 2010

In order to acquire a realistic forecast for the lifetime and post-closure period of the LILW (Low- and Intermediate-Level Radioactive Waste) repository and to establish the overall management plan associated gas issues. it is essential to carry out the long-term experimental research in a similar condition to actual disposal environment. Regarding this, as a part of the following-up actions on a construction and operation license for the first stage of the LILW repository at Gyeongju city, a large-scale in-situ experiment is being planned. For securing basic data on the experiment, the experimental researches related to gas generation previously performed in foreign countries are reviewed in detail. Consequently, it is judged that data on the gas generation experiment in Finland could be practically applied as the benchmark for our large-scale in-situ experiment because the same disposal concept as the Korean repository is adopted and the experiment is performed in a scale large enough to allow the use of regular waste packages.