• 기계저널
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• 제18권1호
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• pp.47-57
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• 1978

자동차용기관의 설계론을 기술함에 있어서 이미 서론에서 언급한 바와 같이 기관전반에 관한 설계론을 편다는 것은 도저히 무리이고 기관의 성능상의 문제나 배기정화의 문제에 있어서도 연소실의 문제가 중심이 되기 때문에 Squish를 가지는 연소실을 중심으로 하여 squish velocity 특성에 관하여 논하였다. 물론, 전술한 것만으로 Squish에 관한 문제가 완벽하다고는 절대 말 할수 없으나 설계계획에 있어서 Squish를 고려한 연소실의 모양 및 치수를 조금이라도 합리적으 로 잡을 수 있는데 도움이 되었으면 한다.

• 대한기계학회논문집
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• 제18권3호
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• pp.793-804
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• 1994

Turbulence intensity caused by piston movement was almost as same tendency as the piston speed. The turbulence intensity was increased from 0.39m/s to 0.79m/s when mean piston speed increased from 2.33m/s to 4.67m/s. In this case the maximum turbulence intensity caused by piston speed was decreased about 82 percent near the top dead center at the end of compression stroke. The maximum turbulence intensity was created from 12m/s to 22m/s when inlet flow velocity was increased from 22m/s to 45m/s. Also turbulence intensity caused by inlet flow velocity was linearly increased from 0.97m/s at top dead center at the end of compression stroke. The ratio of turbulence intensity and mean inlet flow velocity was about 3 percent for inlet flow velocity.

• 대한기계학회논문집
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• 제16권8호
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• pp.1552-1565
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• 1992

본 연구에서는 공기와 연료의 혼합을 원활하게 함으로써 완전연소가 가능하도 록 하기 위하여 이용되는 스월 및 스쿼시 유동이 연소실 내부유동장 변화에 미치는 영 향을 조사하기 위하여 흡입행정 및 연료분무 직전까지의 압축행정에 대해 연소실 내부 유동장을 수치해석하고자 한다.수치해석에는 EPISO-SPRAY 코드를 수정, 보완하여 이용했는데 이 코드는 미국 Los Alamos 연구소를 중심으로 개발된 CONCHAS 계열이나 KIVA 계열의 코드와는 달리 밸브의 개폐운동을 처리할수 있도록 구성되어 있다. 난류모델은 피스톤의 압축 및 팽창에 따른 밀도변화를 고려하여 수정한 k-.epsilon. 모델을 이용한다. 계산은 편심밸브를 갖는 두가지 연소실 형상, 즉 피스톤 보울이 없는 경 우와 피스톤 보울이 있는 경우의 연소실에 대해 선회비를 변화시키며 ATDC 0도부터 ATDC 340도까지의 연료분무가 없는 경우의 3차원 유동장 해석을 통해 흡입 공기가 갖 는 스월과 압축행정 말기에 보울 형상에 따라 발생하는 스쿼시 유동이 유동장 변화에 미치는 영향을 조사하고 기존의 실험치 및 수치해석 결과들과 정성적으로 비교하고자 한다.

• 한국자동차공학회논문집
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• 제4권1호
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• pp.165-176
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• 1996

The flow field and spray characteristics for loop scavenged type 2stroke engine having pancake shape was numerically computed using KIVA-Ⅱ code. The cylinder has 1intake port, 2side intake ports and 1exhaust port with induced flow angle 25 deg. In engine calculation, the chop techniques is used to strip or add planes of cells across the mesh adjacent to the TDC and the BDC(ports parts) for preventing the demand of exceed time during the computation, providing a control on cell height in the squish region. The modified turbulent model including the consideration of the compressibility effect due to the compression and expansion of piston was also used. The case of 25 deg.(injection angle) which is opposite to scavenging flow direction shows better the distribution of droplets and the evaporation rate of droplets compared to other cases(0 deg., - 25 deg.). When injection pressure was increased, the spray tip penetration became longer. When injection pressure was increased, the interaction between the upward gas velocity and spray droplets strongly cause. Thus the breakup of droplets is strongly occurred and the evaporation rate of droplets was found to be better.

• 대한기계학회논문집
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• 제17권9호
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• pp.2339-2358
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• 1993

Since the rate and completeness of combustion in direct injection engines were controlled by the characteristics of gas flow fields and sprays, an understanding of those was essential to the design of the direct injection engines. In this study the numerical simulations of injection pressure effects on the characteristics of gas flow fields and sprays were preformed using the spray model that could predict the interactions between gas fields and spray droplets. The governing equations were discretized by the finite volume method and the modified k-.epsilon. model which included the compressibility effects due to the compression/expansion of piston was used. The results of the numerical calculation of the spray characteristics in the quiescent environment were compared with the experimental data. There were good agreements between the results of calculation and the experimental data, except in the early stages of the spray. In the motoring condition, the results showed that a substantial air entrainment into the spray volume was emerged and hence the squish motion was relatively unimportant during the fuel injection periods. It was found that as the injection pressure increased, the evaporation rate of droplets was decreased due to the narrow width of spray and the increased number of droplets impinged on the bottom of the piston bowl.