• 한국가스학회지
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• 제16권1호
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• pp.1-7
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• 2012

복합 화력발전소 배열회수보일러에서의 입구 덕트 확관 형상 변화에 따른 전열관군 전단에서의 유동 균일화 특성을 유동수치해석을 통하여 분석하였다. 배열회수보일러의 입구는 가스터빈 후류의 출구에 해당하고 가스터빈 후류는 강한 선회 및 난류 유동이다. 본 연구에서 배열회수 보일러 입구 유동 경계조건은 가스터빈을 통과한 출구 유동 해석 결과를 이용하여 수행하였다. 배열회수보일러의 전열관군 전단에서의 유동 균일화 특성이 배열회수 보일러의 효율에 직결되므로 입구 덕트 확관 변곡점의 위치 변화에 따라 유동 균일화 특성을 파악함으로써 배열회수 보일러의 형상 최적화의 기반을 마련하는 것을 목적으로 하였다. 본 연구로부터 배열회수 보일러 확관의 변곡점의 위치가 기준 형상에서 낮은 위치에서 전열관군 전단에서 최적의 유동 균일화가 이루어짐을 알았다.

• 산업기술연구
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• 제36권
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• pp.3-7
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• 2016

The change of flue gas residence time with the location of air inlet in an incinerator is analysed. An independent numerical variable is the location of air inlet and dependant is the residence time of flue gas. The mean value of turbulence energy in a primary combustion chamber is also analysed. The flow field and the distribution of turbulence energy are investigated to evaluate their influence on the residence time of flue gas and the turbulence energy. As the position of secondary air inlet approaches to the top of primary combustion chamber, the residence time of gas and the turbulence energy become longer and larger respectively.

• Applied Science and Convergence Technology
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• 제23권4호
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• pp.169-178
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• 2014

Fluid model based numerical analysis is done to simulate a low damage etch back system for 20 nm scale semiconductor fabrication. Etch back should be done conformally with very high material selectivity. One possible mechanism is three steps: reactive radical generation, adsorption and thermal desorption. In this study, plasma generation and transport steps are analyzed by a commercial plasma modeling software package, CFD-ACE+. Ar + $CF_4$ ICP was used as a model and the effect of reactive gas inlet position was investigated in 2D and 3D. At 200~300 mTorr of gas pressure, separated gas inlet scheme is analyzed to work well and generated higher density of F and $F_2$ radicals in the lower chamber region while suppressing ions reach to the wafer by a double layer conducting barrier.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2008년도 하계학술발표대회 논문집
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• pp.1172-1177
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• 2008

Diverging channel from gas burner exit to the inlet section of Heat Recovery Steam Generator (HRSG) has been re-designed for 1 MW steam supply and power generation system. Three different test geometries have been chosen for the numerical simulation. The existing design for 300 kW HRSG system (CASE B) has been improved by geometry and position changes of inlet guide vanes along with gas velocity entrance angle at the diverging channel inlet (CASE C). Both cases has been compared with the case where hot combustion gas is directly injected without any guide vanes (CASE A). Improved design shows overall uniform velocity and temperature distribution compared to existing design.

• 한국연소학회:학술대회논문집
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• 대한연소학회 2003년도 제27회 KOSCO SYMPOSIUM 논문집
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• pp.287-298
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• 2003

A numerical investigation of a catalytically stabilized thermal (CST) combustor was conducted for a multi-channel catalyst bed, and both the catalyst bed and thermal combustor were simultaneously modeled. The numerical model handled the coupling of the surface and gas reaction in the catalyst bed as well as the gas reaction in the thermal combustor. The behavior of the catalyst bed was investigated at a variety of operating conditions, and location of the flame in the CST combustor was investigated via an analysis of the distribution of CO concentration. Through parametric analyses of the flame position, it was possible to derive a criterion to determine whether the flame is present in the catalyst bed or the thermal combustor for a given inlet condition. The results showed that the maximum inlet temperature at which the flame is located in the thermal combustor increased with increasing inlet velocity.

• 에너지공학
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• 제23권3호
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• pp.51-57
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• 2014

MILD 연소는 고온의 배기가스가 연소로 내에 유입되는 연료와 공기의 혼합물과 고온의 배기가스 가 만나는 위치에 따라 질소산화물 저감 특성이 많은 영향을 받는다. 본 연구에서는 폐기물소각로에 적용한 MILD 연소로에서 배기가스 재순환 여부에 따른 유동 특성과 배기가스 재순환 위치에 따른 유동 특성을 살펴보아 최적의 배기가스 재순환 위치를 선정하는 것을 목적으로 하였다. 본 연구의 전산 해석의 결과는 배기가스 재순환이 없는 경우에는 수직 격벽 상부의 단면에서 속도 분포는 수직 격벽 바로 상부에 큰 속도가 있고 더 상부는 역류가 일어나는 것을 확인할 수 있었다. 배기가스 재순환이 있는 경우는 상부 자유공간에서의 유동 균일도를 수직 격벽 상부 단면에서의 x 방향 속도의 %RMS 값으로 비교하였으며 재순환 흡입구 위치가 자유공간 우측 상단에 위치한 경우가 %RMS 값이 57.4%로 가장 작은 값을 가지며 따라서 가장 효과적임을 알 수 있었다.

• 동력기계공학회지
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• 제17권3호
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• pp.17-22
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• 2013

Diesel particulate filter has been adopted in new vehicle with diesel engine. Since the flow of exhaust gas was clogged as particulate matters were deposited in the filter, it have bad effects on a fuel consumption and power. It was investigated that a particulate filtering system with vacuum pump in the exhaust gas line could be free from clogging in previous research. In this study, the effects of water injection and position of inlet port in filtering system on reducing in particulate matter were investigated. It was noticed that particulate matter were decreased remarkable by water injection and moving the position of inlet port.

• 대한기계학회논문집
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• 제11권5호
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• pp.725-730
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• 1987

본 연구에서는 2사이클 기관의 흡입 포오트 부근의 가스 유동을 레이저 도플 러 유속계를 이용하여 측정하고 가스의 평균 속도, 속도 변동, 유속 벡터 등을 기관의 회전 속도, 실린더 헤드의 모양 및 실린더로의 흡입 속도 측정점의 위치 변화에 대하 여 비교 검토하고, 유동 특성을 고찰하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.853-858
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• 2000

The working fluid from the combustor to the turbine stage of a gas turbine makes various boundary layer thickness. Since the inlet boundary layer thickness is one of the important factors that affect the turbine efficiency. It is necessary to investigate secondary flow and loss with various boundary layer thickness conditions. In the present study, the effect of various inlet boundary layer thickness on secondary flow and loss and the proper height of the boundary layer fences for various boundary layer thickness were investigated. Measurements of secondary flow velocity and total pressure loss within and downstream of the passage were taken under 5 boundary layer thickness conditions, 16, 36, 52, 69, 110mm. It was found that total pressure loss and secondary flow areas were increased with increase of thickness but they were maintained almost at the same position. At the fellowing research about the boundary layer fences, 1/6, 1/3, 1/2 of each inlet boundary layer thickness and 12mm were used as the fence heights. As a result, it was observed that the proper height of the fences was generally constant since the passage vortex remained almost at the same position. Therefore once the geometry of a cascade is decided, the location of the Passage vortex and the proper fence height are appeared to be determined at the same time. When the inlet boundary layer thickness is relatively small, the loss caused by the proper fence becomes bigger than endwall loss so that it dominates secondary loss. In these cases the proper fence hight is decided not by the cascade geometry but by the inlet boundary layer thickness as previous investigations.

• 한국표면공학회:학술대회논문집
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• 한국표면공학회 2007년도 춘계학술발표회 초록집
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• pp.97-98
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• 2007

$SiH_4-Ar-O_2$ ICP-CVD에서 증착된 $SiO_2$막의 두께 균일도를 개선시키기 위해 반응가스 주입구의 위치가 두께 균일도에 영향을 주었을 것으로 예상하고, CFD-ACE를 이용하여 2차원 모델링을 하여 최적데이타를 도출하였다.