• Journal of the Korean Society of Propulsion Engineers
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• v.14 no.4
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• pp.10-15
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• 2010

Light gas guns have a large number of applications in various fields of engineering. A two-stage light-gas gun can produce an extremely high pressure in a very short interval of time. In general, the two-stage light-gas gun is made up of a high pressure tube, a compression tube and a launch tube, each stage being separated by diaphragms. This can be employed efficiently in the application of ultra-high pressure liquid jets. In the present study, experiments are carried out to investigate the projectile velocity and pressure behavior in the tubes according to the pressure changes at the frist diaphragm opening. In the present study result was found that the rupture pressure of the first diaphragm has a dominant influence on piston acceleration.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.11
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• pp.70-75
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• 2006

The cabin pressurization system response should be consistent with the design limits such as the cabin pressure schedule, the pressure regulation tolerance, the maximum rate of pressure change during normal and abnormal operation and the maximum cabin air inflow rate change. In this paper, the results of pressure loss analysis and flight test for cabin pressurization system of T-50 advanced trainer are introduced. The pressure tolerance at unpressurized condition using calculated exit area of pressurization components through pressure loss analysis is predicted. Pressurization components of D company are selected and the predicted pressure tolerance is in good agreement with flight test results. Finally, T-50 pressurization system is verified by some flight tests of T-50 advanced trainer to comply with various pressurization design criteria of MIL-E-18927.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.7
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• pp.85-93
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• 2003

Droplet vaporization at various ambient pressures is studied numerically by formulating one dimensional evaporation model in the mixture of hydrocarbon fuel and air. The ambient pressure ranged from atmospheric conditions to the supercritical conditions. The modified Soave-Redlich-Kwong state equation is used to account for the real gas effects in the high pressure condition. Non-ideal thermodynamic and transport properties at near critical and supercritical conditions are considered. Some computational results are compared with Sato's experimental data for the validation of calculations. The comparison between predictions and experiments showed quite a good agreement. The droplet lifetime increases with increasing pressure at temperature lower than the critical temperature, however, it decreases with increasing pressure at temperature higher than the critical temperature. The solubility of nitrogen can not be neglected in the high pressure and it becomes higher as the temperature and the pressure go up.

• Journal of the Korean Institute of Gas
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• v.3 no.3 s.8
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• pp.23-28
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• 1999

Variation of explosion characteristics by the blocks in closed vessel was investigated to analyse the effect of the block volume(volume blockage) and the surface area of the blocks(ratio of block surface area to vessel volume). Volume and surface area of blocks in explosion vessel were changed by the combination of blocks. The volume of explosion vessels was 270 liter, and the LPG-air or NG-air mixtures were ignited by the electric spark. Explosion pressure was measured with the strain type pressure transducer. From the experimental results, explosion pressure was decreased by the increase of the volume blockage and the block surface area. And the decrease of explosion pressure was more affected by the volume blockage than the surface area.

• Proceedings of the Korean Vacuum Society Conference
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• 2011.02a
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• pp.460-460
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• 2011

그래핀은 탄소원자로 구성된 2차원의 나노재료로서 우수한 기계적, 전기적, 광학적 특성을 지닌다. 이러한 특성들을 기반으로 그래핀은 디스플레이, 터치스크린, 전 자기 차폐재 등의 다양한 분야로의 응용이 가능하다고 예측되고 있다. 한편 이러한 특성은 그래핀의 구조 및 결함, 불순물 등에 의하여 변화한다고 알려져 있으며, 이러한 특성의 변화를 통해 전자소자로의 응용도 가능 하다고 예측되고 있다. 따라서 그래핀의 구조를 제어하고 적절한 결함 및 불순물을 부여하는 것은 그래핀의 기초물성 연구 뿐 아니라 응용연구 에 있어서도 매우 중요하다고 할 수 있다. 본 연구에서는 공기 플라즈마를 이용하여 그래핀의 구조변형을 도모하였다. 그래핀은 열화학 기상증착법 (thermal chemical vapor deposition; TCVD)을 이용하여 300 nm 두께의 니켈박막이 증착된 기판위에 합성하였다. 합성된 그래핀은 산화처리 시 기판의 영향을 배제하고자 트렌치(trench) 구조의 산화막 실리콘 기판위로 전사함으로서 공중에 떠 있는 (air suspended) 구조를 구현하였다. 산화처리를 위한 장치는 직류 플라즈마 장치를 이용하였으며 0.1 Torr의 압력에서 0.4W의 파워로 공기 플라즈마를 방전하여 5분간의 산화처리와 특성평가를 매회 반복함으로서 처리시간에 따른 산화처리의 영향을 관찰하였다. 그 결과 공기 플라즈마 산화처리를 통해 그래핀에 결함을 부여하고 그래핀의 구조변형이 가능함을 확인하였다. 그래핀의 특성분석을 위해서는 광학현미경, 라만 분광기, 원자간힘현미경 등을 이용하였다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.13 no.8
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• pp.3345-3351
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• 2012

In this study, simulation of an underwater platform system which is able to perform the underwater test is implemented to predict its dynamic characteristics. Accordingly, its governing equations are derived to construct the mathematical model. From the proposed model, the time in flooding and the pressure of ballast tank in blowing air to come up are predicted. In addition, simulation of the stability of the system for repulsive force of the tube by compressed air is carried out. Their results will be used to select valves, air tanks as well as design the system including ballast tanks. And they will help users operate it efficiently.

• Journal of the Korean Society of Propulsion Engineers
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• v.7 no.4
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• pp.27-32
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• 2003

The Performance of micro combustor in various condition was exploited experimentally. Various geometric conditions of combustor were considered to figure out the performance of micro combustor. The micro combustor studied in this study was constant volume with cylindrical shape. Geometric parameters of combustor were defined to be combustor height and diameter. The effect of height was exploited parametrically with the size of 1mm, 2mm and 3mm. The effect of diameter was observed parameterized with 7.5mm and 15mm. Three different combustibles or Stoichiometric mixture of methane/air, hydrogen/air were used. Pressure transition during combustion process was recorded. The maximum pressure by combustion responded favorably with the change of height of combustor and the initial pressure. The flame propagation was visulized using Schlieren method. The flame propagation within combustor was observed when specific conditions such as combustor height and initial pressure over critical value was satisfied.

• Journal of the Korean Society for Railway
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• v.17 no.3
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• pp.186-192
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• 2014

In this paper, a reliability analysis is performed where the pressure change inside a concrete tube is probabilistically estimated considering the uncertainties inherent in the material and the system discontinuity. A set of uncertain quantities related to the equivalent system air permeability and the atmospheric pressure, are defined as random variables with specific distribution. The pressure change inside a concrete tube is then probabilistically described using both analytical and simulation approaches. The reliability analysis confirms that the geometric configuration of a concrete tube needs to be changed from the initial configuration obtained from the deterministic analysis.

• Proceedings of the KIEE Conference
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• 2002.07c
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• pp.1470-1472
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• 2002

3원계 51wt%Ni-4lwt%Cr-8wt%Si 합금 타겟을 가지고 DC/RF 마그네트론 스퍼터를 이용하여 박막저항을 제조하였고, 낮은 저항온도계수(TCR)를 가지는 박막을 만들기 위해 제조공정의 변화에 따른 박막의 미세구조와 전기적인 특성을 조사하였다. 스퍼터링 제조공정 변수로써 DC/RF Power, 반응압력, 기판온도를 변화시켰고, 제조된 박막은 공기중에서 $400[^{\circ}C]$까지 열처리 하였다. 반응압력을 감소시킴에 따라 TCR값은 감소하였고, 기판온도 및 열처리 온도의 증가에 따라 TCR값도 증가하였다. 또한, 비저항은 DC Power에서 $172[{\mu}{\Omega}cm]$, RF인 경우에는 $209[{\mu}{\Omega}cm]$을 나타내었고, 각각 +52, $-25[ppm/^{\circ}C]$의 TCR값을 나타냈다. 이와 같은 결과로부터 제조공정을 변화시킴에 따라 면저항 및 저항온도계수의 제어가 가능함을 알 수 있었다.

• Membrane Journal
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• v.27 no.1
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• pp.43-52
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• 2017

The air injection nozzle tube was inserted inside of the tubular membrane module to reduce membrane fouling and improve the permeate flux. The average pore size of membrane was $0.1\;{\mu}m$ and the yeast was used as a foulant. All of permeate experiments were started without air injection for the module equipped with the nozzle tube, then carried out continuously with air injection. Finally, the nozzle tube was removed from the module and the permeate was measured without air injection. The measured permeate fluxes were compared to examine the effect of air injection. The fluxes for air injection were consistently maintained or increased. The fluxes of no-air injection with the nozzle tube were greater than those of the empty tubular module. As operating pressure decreased to 0.4 bar, the flux enhancement of air injection based on no-nozzle case increased to 21%. Flux enhancements of air injection were above 30% as the gas/liquid two-phase flow was changed from the stratified-smooth to the intermittent pattern due to increase of gas flowrate.