• Proceedings of the KSME Conference
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• 2005.11a
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• pp.105.1-105.1
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• 2005

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.77.2-77.2
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• 2005

• Defense and Technology
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• no.7 s.281
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• pp.66-75
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• 2002

과거 10년전만해도 산업, 난방, 발전 등이 대기오염의 주된 원인이었으나 자동차의 증가로 말미암아 최근에는 자동차의 배기가스 즉 질산화물질(NOx), 일산화탄소(CO), 탄화수소(HC), 총먼지(TSP : Total Solid Particlate), 아황산가스(SO2) 등이 대기를 오염시키는 주요 물질이 되었다. 인구의 증가, 산업의 발달, 경제수준의 향상은 자동차 증가를 촉진시키는데 촉매제 역할을 해왔으며 대도시에서의 자동차에 의한 오염물질 배출량은 앞으로도 차량의 증가와 더불어 가속화할 전망이다.

• Proceedings of the Korean Society of Marine Engineers Conference
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• 2005.06a
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• pp.783-788
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• 2005

This document provides the concerning information of the MEPC Committee and DE sub-Committee of International Maritime Organization in accordance with enforcement of an International Air Pollution Prevention Certificate at May 19 2005years.

• Journal of the KSME
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• v.32 no.10
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• pp.876-882
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• 1992

여기에서는 삼원촉매 장착엔진을 정밀하게 제어(연료 제어, 공회전 제어, 점화시기 제어, Purge Air 제어 등)하여 삼원촉매의 효율을 향상시키고, 그 결과 배기가스를 감소시킴과 더불어 운전성 및 동력성능을 향상시킨 엔진 전자 제어 시스템의 개요를 간단히 소개하였다. 앞으로도 북미지 역의 배기가스 관련법규가 더욱 강화될 것으로 예상되며, 이에 대응한 엔진 제어 시스템에 대한 지속적인 연구 개발이 필요하리라 생각된다.

• Journal of the korean Society of Automotive Engineers
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• v.12 no.1
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• pp.10-19
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• 1990

본 기고에서는 농도분석에 사용되는 많은 측정장비 중에서 여러가지의 가스성분을 한번에 측정할 수 있고, 다른 전용가스분석기에 비하여 경제적인 가스크로마토그라프를 소개하고, 특히 탄화수소(hydrocarbon)계열의 연료를 사용하는 열기관의 배기가스분석에 국한하여, 적용예와 문제점을 검토하여 가장 최적의 가스크로마토그라프 운용조건을 찾는데 도움이 되고자 한다.

• Korean Journal of Environmental Agriculture
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• v.27 no.2
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• pp.150-155
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• 2008

This study was carried out to determinate the location and the number of air inlet and outlet, optimum air inlet velocity for effective ventilation in windowless weaning piglet house($2.90(W){\times}9.90(L){\times}2.80(H)$ m) by CFD(Computation Fluid Dynamics) simulation. The weaning piglet house for this experiment was consisted of 11 air inlets and 9 outlets, modified and simulated using CFD code, FLUENT. The simulation result for the original weaning piglet house, which was not modified, showed ununiform ventilation for each room. Therefore, for uniform ventilation, 4 air inlets and 1 outlet were completely closed, and 2 air outlets were partially closed. The simulation result for the modified weaning piglet house showed uniform ventilation for each room and the optimum air inlet velocity of 0.5 $m\;sec^{-1}$.

• Journal of Energy Engineering
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• v.22 no.4
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• pp.413-419
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• 2013

The present study used the MILD combustor, which has coaxial cylindrical tube. The outside tube of the MILD combustor corresponds to the exhaust gas passage and the inner side tube is the furnace passage. A numerical analysis was accomplished to elucidate the characteristics of exhaust gas entrainment toward the inner furnace with the changes of venturi nozzle geometrical parameters, nozzle position, nozzle gap between high pressure air nozzle and venturi nozzle, and with the change of high pressure nozzle inlet velocity. The entrainment flow rate for the case with the high pressure air nozzle attached at the exhaust gas wall has relatively small change with the change of nozzle gap. That for the case with the high pressure air nozzle exposed to the exhaust gas has monotonically increase with the change of nozzle gap. The flow rate ratio of entrainment flow rate has considerably increase tendency with relatively lower air inlet velocity, on the other hand, that with relatively higher air inlet velocity could be seen relatively small increase.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.4
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• pp.300-309
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• 2017

A spacecraft obtains a reaction momentum required for an orbit correction and an attitude control by exhausting a combustion gas through a small thruster in space. If the exhaust plume collides with spacecraft surfaces, it is very important to predict the exhaust plume behavior of the thruster when designing a satellite, because a generated disturbance force/torque, a heat load and a surface contamination can yield a life shortening and a reduction of the spacecraft function. The purpose of the present study is to ensure the core technology required for the spacecraft design by analyzing numerically the exhaust gas behavior of the 10 N class bipropellant thruster for an attitude control of the spacecraft. To do this, calculation results of chemical equilibrium reaction between a MMH for fuel and a NTO for oxidizer, and continuum region of the nozzle inside are implemented as inlet conditions of the DSMC method for the exhaust plume analysis. From these results, it is possible to predict a nonequilibrium expansion such as a species separation and a backflow in the vicinity of the bipropellant thruster nozzle.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.40 no.4
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• pp.263-273
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• 2016

The effect of recirculated exhaust gas on performance and exhaust emissions with FGR rate are investigated by using a natural circulation, pressurized draft and water tube boiler with FGR system operating at several boiler loads and over fire air damper openings. The purpose of this study is to apply the FGR system to a power plant boiler for reducing $NO_x$ emissions. To activate the combustion, the OFA with 0 to 20% is supplied into the flame. When the suction damper of two stage combustion system installed in the upper side of wind box is opened by handling the lever between $0^{\circ}$ and $90^{\circ}$, also, the combustion air supplied to burner is changed. It is found that the fuel consumption rate per evaporation rate did not show an obvious tendency to increase or decrease with rising the FGR rate, and $NO_x$ emissions at the same OFA damper opening are decreased, as FGR rates are elevated and boiler loads are dropped. While a trace amount of soot is emitted without regard to the operation conditions of boiler load, OFA damper opening and FGR rate, because soot emissions are eliminated by the electrostatic precipitator with a collecting efficiency of 86.7%.