• Korean Journal of Remote Sensing
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• v.30 no.6
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• pp.743-754
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• 2014

In this present paper, we, for the first time, calculated $SO_2$ inflow from China to Korea peninsula based on OMI $SO_2$ products and HYSPLIT (Hybrid Single Particle Lagrangian Integrated Trajectory Model) backward trajectory calculations. The major factors used to estimate $SO_2$ flux are long range transported $SO_2$ concentration, transport speed of air mass, and thickness of transported air mass layer. The mean and maximum $SO_2$ fluxes are estimated to be 0.81 and $2.11g{\cdot}m^{-2}{\cdot}h^{-1}$, respectively based on OMI products while, those of $SO_2$ fluxes are 0.50 and $1.18g{\cdot}m^{-2}{\cdot}h^{-1}$ respectively using insitu data obtained at the surface. For most cases, larger $SO_2$ inflow values were found at the surface than those estimated for the air mass layer which extends from surface up to 1.5 km. However, increased transport speed of air mass leads to the enhanced $SO_2$ flux at the altitude up to 1.5 km at the receptor sites. Additionally, we calculate uncertainties of $SO_2$ flux using error propagation method.

• Journal of the Korean Institute of Gas
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• v.23 no.1
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• pp.12-18
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• 2019

Exhaust gas recirculation method is widely used among various methods for reducing nitrogen oxides in automobile engines and incinerators. In the present study, the computational fluid dynamic analysis was accomplished to derive the optimal location of air nozzle exit position by changing its position in a venturi tube for the maximum flue gas recirculation effect. In addition, the flue gas recirculation characteristics with a cone at the exit of air nozzle was elucidated with flue gas recirculation flow rate ratio and mixed gas exit temperature. When the air nozzle exit position was changed from the start position (z = 0) to the end position (z = 0.6m) of the exhaust gas recirculation exit pipe, the change of streamline and temperature distribution in the venturi tube was observed. The exhaust gas recirculation flow rate and the average temperature at the mixed gas exit position was quantitatively compared. From the present study, the optimal location of air nozzle exit position for the maximum flue gas recirculation flow rate ratio and maximum mixed gas exit temperature is z = 0.15m (1/4L). In addition, when the cone is installed at the outlet of the air nozzle, the velocity of the air nozzle outlet is increased, the flue gas recirculation flow rate was increased by about 2 times of the flow rate without cone, and the mixed gas exit temperature is increased by $116^{\circ}C$.

• KOREAN JOURNAL OF CROP SCIENCE
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• v.39 no.6
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• pp.526-530
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• 1994

This study was conducted to investigate photosynthetic response to four sequential air influx rate with rice(Oryza sativa L.)plants moved from a natural condition to constant condition with automatic regulation selected environmental variables on 13th~15th days after anthesis. In time course of photosynthetic response to increasing air influx rate(200-280-360-440 ml / min.), stomatal conductance decreased rapidly at the beginning after treatment and then oscillated with a free-running period of a approximately 1 hour to 1 hour 30 minutes until reached up to steady-state condition. Similar change was also observed $CO_2$ assimilation rate. Stomatal conductance decreased throughout the air influx rate sequence, but the rate of decrease was similar to the decrease in $CO_2$ assimilation rate observed under continuous air influx rate conditions. In starch granules during grain filling period under air influx rate(440 ml / min.) , compound starch granules were loosing and a number of hollows were observed in surface of single starch granules. Evidences from several approaches indicate that synchronization of stomatal conductance and$CO_2$ assimilation rate was closely inter-related tinder increase of air influx rate and increase of air influx rate influenced the$CO_2$ uptake in photosynthetic processes and compound starch granule, as 'end products' of photosynthesis.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.04a
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• pp.11-11
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• 1999

액체 램제트 연소기는 흡입공기와 분무, 혼합 그리고 이에 따른 연소 등 일련의 과정에 따라 다수의 복잡한 현상들이 상호 밀접하게 관련되어 있다. 본 연구에서는 액체 램제트 연소기내의 유동특성을 파악하기 위해서 2차원 및 3차원 연소기 형상에 대해서 수치적 실험을 수행하였으며, 격자구성은 연소기에 공기를 공급하고 연료를 분무하는 공기 유입관 영역과 연소실 영역, 그리고 출구 대기 영역으로 나누어 독자적으로 격자를 생성시켰다. 2차원과 3차원 유동해석을 비교하였고 분무모델의 적용에 따른 연소특성 및 분사위치에 따른 연소특성을 비교하였다. 유동해석 결과 2차원과 3차원의 유동특성은 달랐으며, 분무모델을 적용해야 정확한 연소 유동 현상을 예측할 수 있음을 알 수 있었다. 그리고 유입관의 안쪽에 연료의 분사위치를 준 경우가 연소의 안정화에 필요한 재순환영역으로의 연료의 혼합이 잘 되어 유입관 바깥쪽에 연료를 분사시키는 것보다 좋은 분사위치임을 알 수 있었다.

• Air Cleaning Technology
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• v.27 no.2
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• pp.30-40
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• 2014

• Air Cleaning Technology
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• v.32 no.4
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• pp.1-8
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• 2019

• Journal of Advanced Marine Engineering and Technology
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• v.34 no.6
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• pp.864-870
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• 2010

Air embolism can be a lethal complication of surgical procedures during which venous pressure at the site of surgery is sub-atmospheric or air is forced under pressure into a body cavity. To solve the problem, we developed the air detector using relative dielectric constant change, which is expected to be used broadly in industrial circles. We designed air detection system with air control equipment, detection circuit and LabVIEW system for air sensing. In experiments with a mock system, the proposed system showed a signal difference depending on the amount of air in the Tygon tube of the mock system.

• Proceedings of the Korea Water Resources Association Conference
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• 2015.05a
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• pp.174-174
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• 2015

국내의 국지성 집중호우와 같은 기후변화와 토지피복율 증가 등 복합적인 원인으로 인한 표면 유출수의 증가로 도시에서의 내수침수가 매년 빈번하게 발생하고 있다. 이러한 도심지 돌발홍수로 인한 피해에 대한 구조적인 대책으로 지하방수로가 효과적인 방안으로 대두되고 있으며, 현재 신월빗물저류배수시설이 설계단계에 있다. 그러나 미국, 일본 등의 국외의 기설치된 지하방수로에서 발생되는 Geyser 현상으로 인한 피해에 대한 연구는 국외에 비해 미비한 편이므로, 선행적으로 Geyser에 대한 물리기반의 동수역학적인 이해가 필요한 실정이다. Geyser는 홍수 시 급격한 유량의 유입으로 단파가 발생하여 지하방수로 내 공기의 압축이 발생하고 수직관을 통해 공기가 물과 함께 지상으로 분출되면서 발생된다. 따라서 공기와 물의 혼합 유동을 모의해야 하며 동시에 단파의 불연속성을 모의하기 위해서는 기존의 상용프로그램으로는 다소 어려움이 있다. 이에 본 연구에서는 지하방수로의 Geyser 현상의 발생 예측을 위해 1차원 Saint-Venant 방정식을 지배방정식으로 선정하였으며, 단파 발생을 수치적으로 안정적으로 모의하기 위해 Roe Approximate Riemann 수치기법을 사용하였다. 또한 공기의 압력항을 고려하기 위해서 수정된 형태의 Preissmann slot 모형을 적용하였다. Geyser 현상의 영향인자로서 지하방수로 수평관의 직경, 마찰계수, 바닥경사, 초기수위, 유입유량을 고려하였으며 상류에서 유입되는 유량에 의한 하류에서의 동수역학적 거동을 분석하였다. 5개의 영향인자의 변화에 따른 단파의 유입속도 및 공기부 압력의 변화를 관찰하여 Geyser 현상에 대한 동수역학적 검토를 수행하였다. 추후 본 연구결과를 적절히 활용한다면 지하방수로의 사용 안정성을 확보하고, 홍수발생 시 모니터링 인자도출에 도움이 될 것으로 예상된다.

• Journal of the Society of Cosmetic Scientists of Korea
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• v.37 no.1
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• pp.43-53
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• 2011

The conditions in fluid-bed processor for nanoencapsulation of azelaic acid-milk nano powder for acne nanocosmetics were optimized by response surface methodology (RSM). The maximum value of yield was 70.97 %. The yield was appreciably influenced by inlet air temperature, atomizing pressure, and feeding speed. The particle size increased with an increase in the feeding speed and a decrease in the atomizing pressure. The elution rate in saline solutions was appreciably influenced by inlet air temperature and atomizing pressure. The moisture content increased with higher atomizing pressure, which was demonstrated to be similar to the nanoencapsulation characteristics related to water activity. The Hunter's L and b values increased with an increase in the inlet air temperature. The optimum conditions estimated by RSM for the maximized values of yield, moisture content, particle size and elution rate in skin suitability were $67{\sim}73^{\circ}C$ of inlet air temperature, 0.6 ~ 0.8 mL/min feeding speed and 1.8 ~ 2.0 kg/$cm^2$ of atomizing pressure, respectively. These estimated values were in agreement with those measured by real experiments.

• Aerospace Engineering and Technology
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• v.9 no.2
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• pp.98-104
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• 2010

The moisture in the atmosphere exerts a lot of influence upon Gas turbine engine performances. There is a noticeable influence of wet air at the summer sea level, high flight mach number and low engine rpm increasingly. An altitude Engine Test Facility is used to accomplish the engine performance tests at dry air condition and wet air condition, through which engine performance results is revealed. Also, Gas turbine Simulation Program is used to predict the variation of engine performance due to inlet humidity. In the result, net thrust and specific fuel consumption measured -2.826% and 1.325%, respectively at wet air condition compared to dry air condition.