• Journal of Power System Engineering
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• v.16 no.6
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• pp.19-23
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• 2012

DME HCCI기관의 단점은 디젤 엔진에 비해 기관부하 영역이 굉장히 좁다는 것이고 이는 저온산화반응이 너무 빨리 일어나서 노크를 발생시키기 때문이다. 저온산화반응을 억제하기 위해서 DME 연소에 미치는 천연가스의 영향을 실험한 결과, 천연가스가 DME의 저온산화반응을 억제시키기 때문에 기관부하영역이 확대된다는 것을 알았다. 본 연구에서는 서로 다른 세탄가를 가진 첨가연료가 DME 저온산화반응에 미치는 영향을 실험적으로 조사하였다. 그 결과 저온산화반응의 최고 열발생율은 세탄가에 의존하지 않지만 착화온도는 세탄가에 의존한다는 사실을 밝혔다.

• Journal of the Korean Society of Industry Convergence
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• v.20 no.1
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• pp.56-66
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• 2017

In this experimental study, it is designed and used the test engine bed which is installed with the exhaust gas recirculation, and in addition to equipped using by oxygen adder. It has been tested and analyzed the combustion and emission characteristics, cycle variability and engine performance by controlling the oxygen volume fraction, EGR rate, engine speed and equivalence ratio.

• Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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• 1997.04a
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• pp.131-135
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• 1997

최근 자동차에 요구되는 주요한 기술과제 중에서 최우선으로 해결해야 될 문제는 환경규제와 관련된 대응방안을 강구하는 것이다. 또한 지속적으로 강화되고 있는 환경규제를 만족하면서 소비자가 요구하는 자동차의 주행성, 안전성, 연비, 메인터난스 등과 관련된 고성능화가 추구되고 있다. 엔진유 측면에서는 배기규제, 연비향상, 장수명화 및 고성능화와 관련이 되는 성능 개선이 요구되고 있다. 특히 배기 규제와 관련해서는 오일 소모량의 감소와 배기 정화 장치에의 피독작용 감소등의 측면에서 물성이 규제되고 있는데 Noack증발 감량 및 함유량 규제가 대표적인 예이다. 본 보고에서는 제1보의 실험에 추가하여 윤활유의 혼입이 휘발유의 연소및 배기에 주는 영향에 관하여 연구하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.10a
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• pp.22-22
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• 1998

155mm 탄에 항력감소장치를 부착하여 탄의 비행중에 형성되는 탄저부의 항력(Base drag)을 감소시켜 사거리를 연장한 무기체계가 미국 등을 비롯한 많은 국가에서 실용화되고 있다. 국과연은 이미 155mm 신형 자주포탄에 적용되는 항력감소장치(항력감소제 그레인, Base & Closure, 점화장치)는 개발하여 사거리를 연장(약 35%)한 것으로 보고하고 있다. 본 연구는 추후 실용화가 예상되는 155mm 성능개량형 DPICM탄(미제 M864급)에 적용할 수 있는 항격감소제용 저연소속도 혼합형 추진제 개발을 목표로 하여, 이에 동등한 추진제 특성(기계적성질, 연소특성, 접착력, 발열량 등)을 가지는 추진제, 라이너(Inhibitor)의 조성개발을 실시하였다. 그리고 개발된 혼합형 추진제 조성의 성능(사거리 및 분산도)을 확인하기 위하여 항력감소제용 그레인을 제작, 155mm 성능개량형 DPICM탄에 적용하여 발사시험을 실시하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.05a
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• pp.332-335
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• 2008

The purpose of this study is analysis of flow field where is around of injector of supersonic combustor which is bluff-body stabilized flame and hyper-mixer type of supersonic combustor injector by using hydrogen or hydrocarbon fuel. Various schemes are evaluated to supersonic backward step flow filed with massive separation region in validation step. Compounded scheme of 5th-order TVD-MUSCL, Roe FDS, S-A DES/DDES has a good performance in base and base-bleed flow.

• Transactions of the Korean Society of Mechanical Engineers
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• v.19 no.8
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• pp.2030-2038
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• 1995

In this study, three turbulent flame propagation models are compared using experimentally measured data of a 4 valves/cylinder spark-ignition engine. First two conventional models are B.K model and GESIM combustion model. The burning rates calculated from the two models are compared with the burning rates calculated from measured pressure data using the one-zone heat release analysis. GESIM combustion model predicts burning rates closer to the data acquired from the experiment in wide operating ranges than B-K model does. The third model is refined based on GESIM combustion model by including the effect of flame stretch, turbulent length scale band pass filter and a variable that considers flame size and the area of flame contacting the cylinder wall surface. The refined combustion model predicts burning rates closer to experimental results than GESIM combustion model does. Also, the refined combustion model predicts flame radius close to the experimental result measured by using optical fiber technique.

• Transactions of the Korean Society of Mechanical Engineers
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• v.18 no.10
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• pp.2787-2796
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• 1994

The modeling of combustion process is an important part in an engine simulation program. In this study, calculated results using a conventional B-K model and the other model which is called GESIM were compared with experimentally measured data of a three-cylinder spark-ignition engine under wide range of operating conditions. The burn rates calculated from the combustion models were compared with the burn rate calculated from the one-zone heat release analysis that uses measured pressure data as an input data. As a result of the two models' comparison, the GESIM combustion model conformed to be closer to the data acquired from the experiment in wide operating ranges. The GESIM model has been improved by introducing a variable that considers the flame size, the area of flame conacting the piston surface into the model, based on the comparison between the experimental result and the calculated results. The improved combustion model predicts experimental results more precisely than that of GESIM combustion model.

• Proceedings of the Korea Air Pollution Research Association Conference
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• 2000.11a
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• pp.330-331
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• 2000

환경오염 유기물질 중 다이옥신류는 높은 화학적 안정성과 생화학적 잔류성으로 인해 1970년대 이후 외국에서는 가장 중요한 환경물질의 하나로 취급되면서 다양한 연구가 이루어지고 있다. 이러한 다이옥신은 여러 가지 경로를 통해 생성되는데 이 중에서도 연소과정, 특히 폐기물 소각로에서 생성되는 것이 주 배출원으로 알려져 있다. 국내에서 1997년도 1차로 실시한 전국의 소각시설 다이옥신 배출 실태조사 이후 정부에서는 신설 도시쓰레기 소각장에 대해서는 0.1 ng-TEQ/Nm$^3$의 배출기준을 설정하고 정기적인 다이옥신 측정을 의무적으로 실시할 것을 법규화한 바 있다. (중략)

• 한국전산유체공학회:학술대회논문집
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• 1998.05a
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• pp.117-122
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• 1998

A numerical study is carried out to investigate the transient process of combustion phenomena associated with hypersonic propulsion devices. Reynolds averaged Navier-Stokes equations for reactive flows are used as governing equations with a detailed chemistry mechanism of hydrogen-air mixture and two-equation SST turbulence modeling. The governing equations are discretized by a high order accurate upwind scheme and solved in a fully coupled manner with a fully implicit time accurate method. At first, oscillating shock-induced combustion is analyzed and the comparison with experimental result gives the validity of present computational modeling. Secondly, the model ram accelerator experiment was simulated and the results show the detailed transient combustion mechanisms. Thirdly, the evolution of oblique detonation wave is simulated and the result shows transient and final steady state behavior at off-stability condition. Finally, shock wave/boundary layer interaction in combustible mixture is studied and the criterion of boundary layer flame and oblique detonation wave is identified.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.28 no.11
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• pp.1339-1347
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• 2004

Development of the low NOx heating boiler was strongly asked due to severe air pollution and the large number of boilers in korea. Compactness of the commercial boiler was also important because of low manufacturing cost and easy installation. In this study. newly developed compact low NOx burner, using turbulent gas diffusion combustion with multi-staged air supplies and multiple fuel nozzles, was investigated. Comparison study of the new burner was performed between experimental results and computational analysis. Commercial computational fluid dynamic(CFD) program named CFX-5.6 was used for numerical analysis of the low NOx burner inside the test combustor. Comparisons of experiment data and numerical result were performed under various equivalence ratio and fuel flow rate.