• Transactions of the Korean Society of Mechanical Engineers B
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• v.36 no.2
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• pp.225-232
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• 2012

A chemical reactor network (CRN) was developed for a lean premixed gas turbine combustor to predict the emission of pollutants such as NOx and CO. In this study, the predictions of NOx and CO emissions from lean premixed methane-air combustion in the gas turbine were carried out using CHEMKIN and a GRI 3.0 methane-air combustion mechanism, which includes the four NO formation mechanisms for various load conditions. The calculated results were compared with experimental data obtained from a modified test combustor to validate the model. The contributions of the four NO pathways were investigated for various load conditions. The effects of nonuniformity of the mass flux and of the equivalence ratio of the injector on the NOx formation were investigated, and a method of reducing the pollutant formation was suggested for the development of a sub-10 ppm gas turbine combustor.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.10a
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• pp.15-15
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• 1999

램 가속기에 대한 연구는 램 가속기의 작동 조건이 고온, 고압, 초고속이라는 점과 가속기 내부에서 급격한 화학반응이 수반된다는 특성으로 인하여 실험과 해석상의 상당한 어려움이 존재한다. 램 가속기는 작동 모드에 따라 탄체 후방의 열적 질식 조건을 이용한 열적 질식 모드(Thermally Choked Mode)와 탄체 표면에 형성되는 데토네이션파를 이용한 초폭굉모드(Superdetonative Mode)로 나뉘어진다. 본 연구는 초폭굉 모드로 작동하는 램 가속기의 작동 성능 향상을 위한 방법으로 수치 최적화 기법을 이용한 램 가속기 내부 예 혼합기의 조성비 최적화를 수행하였다. 설계 변수로는 수소와 질소의 조성비를 선정하였으며, 최적 설계 목표는 일정한 질량과 형상을 갖는 탄체를 초기속도 2500m/s에서 3000m/s로 가속시키기 위하여 필요한 최소 램 가속관의 길이로 정하였다. 본 연구에서는 구베법에 기반한 Simplex 방법 및 SLP(Sequential Linear Programming)등의 수치 최적화 기법을 적용하였고, 가속기 내부의 유동장은 해석의 효율성을 고려하여 이차원 비점성 유동으로 가정하였고, 비평형 화학반응 해석을 수행하였다.

• Journal of the Korea Computer Graphics Society
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• v.3 no.2
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• pp.65-76
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• 1997

본 논문은 인체의 최종효과기 (예: 손)가 주어진 공간상의 목표위치를 성취하도록 새로운 동작을 다수의 기존 동작을 혼합하여 생성하는 동작혼합기법을 제시한다. 전형적인 동작혼합기법에서는 동작들을 구성하는 관절커브들에 사용자가 적절한 가중치를 주고 이들의 가중치 합을 구하여 새로운 동작의 관절커브로 삼는다. 그러나 생성될 동작이 특정 제약조건 (예: 손의 최종위치)를 만족해야 될 경우에는 사용자가 성분동작에 적절한 가중치를 부여하는 것이 쉽지 않다. 따라서 본 논문은 원하는 동작의 타입 (예: 걷기, 손 뻗기) 과 동작의 최초 및 최종상태가 주어지연, 주어진 최초 및 최종상태를 만족하는 새로운 동작을 기존동작들을 혼합하여 자동적으로 생성하는 기법을 제안한다. 이 기법은 성분동작들의 집합을 연속적이고 완만한 곡면으로 표현하고 사용자가 생성하기 원하는 동작의 최초 및 최종상태를 정하면 이 곡면상에 있으면서 주어진 최초 및 최종상태를 만족하는 특정 동작을 구하여 원하는 동작으로 삼는다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.34 no.12
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• pp.1043-1050
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• 2010

Fuel stratification and thermal stratification occur in the HCCI combustion chamber on a microscopic scale. They affect the ignition and combustion processes. In this study, the effect of the inhomogeneity in the mixture gas on the HCCI combustion process was investigated. Two-dimensional chemiluminescence images were captured using a framing camera to evaluate the flame structure. DME was used as the test fuel. First, the effect of inhomogeneity in the fuel distribution in the premixture was investigated for the four-stroke optically accessible engine. Then, by comparing the combustion of the homogeneous mixture in the rapid compression machine, which does not contain any residual gas, with the combustion in the four-stroke engine, the effect of inhomogeneity in temperature due to the residual gas was analyzed. The results showed that a time lag appears spatially in combustion under inhomogeneous conditions in the four-stroke engine. The spatial variation in the combustion without the residual gas in the rapid compression machine is less than that in the combustion in the four-stroke engine.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.37 no.2
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• pp.161-170
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• 2013

The flow and combustion characteristics in a premixed swirl combustor with a double cone burner are numerically analyzed to adopt a swirler model. The internal recirculation zone formed at the burner exit can be realized by a swirler with inner and outer diameters of 56 and 152 mm, respectively, and accordingly, the flow rate and radial velocity were determined. To select the tangential velocity, swirl and recirculation angles are introduced. A tangential velocity of 40 m/s produces an internal recirculation zone similar to that in a combustor. At the liner exit, the errors in temperature and velocity are 2.8% and 0%, respectively, and they are negligibly small. However, NOx emissions are underestimated by 67% in the numerical results obtained using the swirler model. Although considerable quantitative errors are induced by the swirler model, it can be useful numerical model for the EV burner because it can approximately simulate the essential flow and combustion characteristics in a premixed swirl combustor with a double cone burner and it is expected to make combustion analysis efficient in a gas turbine combustor with complex geometries.

• Journal of the KSME
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• v.30 no.4
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• pp.358-366
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• 1990

이 글은 최근 대두되는 CFC 문제와 연관하여 혼합냉매를 사용함으로서 얻어지는 이점과 이들의 예를 알아보고 이에 수반하여 열교환기의 설계 및 제작에 있어서 필수적인 역할을 하는 혼합매 체에서의 2상유동열전달의 중요성과 체계적인 연구의 필요성을 강조하기 위하여 기술한 것이며 이 분야에 대한 새로운 지식을 전반적으로 집약하거나 자료를 광범위하게 수집한 것이 아니다.

• Transactions of the Korean Society of Automotive Engineers
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• v.4 no.3
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• pp.156-167
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• 1996

The present work is a continuation of our previous study to investigate the effects of parameters such as equivalence ratio, hydrogen supplement rate and initial pressure on combustion characteristics in a disk-shaped constant volume combustion chamber. The main results obtained from the study can be summarized as follows. The flames in near stoichiometric mixture of methane-air are propagated with a spherical shape, but in excess rich or lean mixtures are propagated with a elliptical shape. And, they are changed to an unstable elliptical shape flame with very regular cells by increasing the hydrogen supplement rate. Also, flame is sluggishly propagated at increased initial pressure in combustion chamber. Volume fraction of burned gas and flame radius as the combustion characteristics are increased by increasing the hydrogen supplement rate, especially at the combustion middle period, but then are slowly increased by increasing the initial pressure.

• Transactions of the Korean Society of Automotive Engineers
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• v.11 no.3
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• pp.48-57
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• 2003

A cylindrical constant volume combustion chamber was used to investigate the flow characteristics at spark plug and the combustion characteristics of homogeneous charge methane-air mixture under various initial pressure, excess air ratio and ignition times in quiescent mixture. The flow characteristics such as mean velocity and turbulence intensity was analyzed by hot wire anemometer. Combustion pressure development measured by piezoelectric pressure transducer and flame propagation acquired by ICCD camera were used to investigate the effect of initial pressure, excess air ratio and ignition times on pressure, combustion duration, flame speed and burning velocity. Mean velocity and turbulence intensity had the maximum value at 200 or 300ms and then decreased to near 0 value gradually after 3 seconds. Combustion duration, flame speed and burning velocity were observed to be promoted with excess air ratio of 1.1, lower initial pressure and ignition time of 300ms.

• Transactions of the Korean Society of Automotive Engineers
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• v.11 no.4
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• pp.29-36
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• 2003

A cylindrical constant volume combustion chamber was used to investigate the flow characteristics at spark plug and the combustion characteristics of inhomogeneous charge methane-air mixture under several parameters. The flow characteristics such as mean velocity and turbulence intensity was analyzed by hot wire anemometer. Combustion pressure development measured by piezoelectric pressure transducer was used to investigate the effect of initial charge pressure, excess air ratio and ignition times on combustion pressure and combustion duration. Mean velocity and turbulence intensity had the maximum value at 200 or 300ms and then decreased to beneath 0.05m/s gradually at 3 seconds. Second mixture is accompanied by an increase in the combustion rate, and that the higher the mass which is added in the second stage injection, the faster the burn rate.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.11
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• pp.57-64
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• 2005

Large Eddy Simulation (LES) of turbulent premixed combustion flow is performed by using the dynamic subgrid scale model based on -equation describing the flame front propagation. After introducing the LES governing equations with dynamic subgrid scale (DSGS) model newly introduced into the -equation, the turbulent premixed combustion flow over backward facing step is analyzed to validate present formulation. The calculated results can predict the velocity and temperature of the combustion flow in good agreement with the experiment data.