• 한국추진공학회지
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• 제22권1호
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• pp.28-35
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• 2018

전단 동축형 인젝터를 통해 분사된 기체메탄-기체산소 확산화염의 가연한계와 구조분석을 위해 인젝터 리세스와 추진제 공급유량에 따른 연소실험이 수행되었다. 연구 결과, 추진제 운동량 플럭스 비가 증가함에 따라 높은 산화제 레이놀즈 수 구간에서도 안정적인 부착화염이 관찰되었으며, 인젝터 리세스는 화염의 형태와 가연한계에 큰 영향을 미치지 않음을 확인하였다. 자발광 기법을 통해 가시화된 부착화염은 추진제 분사조건이 변함에도 불구하고 항상 일정한 지점에서 최대 OH 라디칼 방사강도를 나타내었으며, 그 강도는 리세스에 의해 심하게 감소함을 확인하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제32권4호
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• pp.506-513
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• 2008

The engine containing a radical injector has been studied to improve the performances of efficiency and to reduce the exhaust emissions recently. The engine is far different from general compression ignition engines or spark ignition engines for the concept of combustion process. The inflow characteristic from main chamber into radical chamber during compression stroke is important because the radical chamber must have enough fresh air to generate appropriate radicals. The numerical simulation is performed in each specific shape and the engine speed by using KIVA code. The result shows that the fresh air inflow from main chamber into the radical chamber is the best at 45 degree of the hole angle.

• 한국추진공학회지
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• 제23권1호
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• pp.1-8
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• 2019

스월/전단 동축형 인젝터를 통해 형성된 기체메탄-기체산소 확산화염의 동역학적 거동 및 구조분석을 위해 다양한 추진제 분사조건에 따른 연소실험이 수행되었다. 연구결과, 자발광 기법을 통해 가시화된 확산화염의 $OH^*$ 방사강도는 추진제 공급유량 및 운동량 플럭스 비 증가에 따라 높은 값을 나타내고 있으며, 스월을 가지는 화염은 그렇지 않은 것에 비해 더 우수한 반응성을 보였다.

• 대한기계학회논문집B
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• 제27권9호
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• pp.1309-1316
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• 2003

A premixed-compression-ignition engine has been studied to improve the efficiency and to decrease exhaust emissions. However those systems have some difficulties for controlling combustion process. Radical is an activated chemical species formed by a chemical chain reaction between reactant and product. When the chain reactions occur, the energy bond of species is broken easily by the released radicals. The combustion chamber of the premixed-compression-ingnition engine is consist of a main chamber with lean premixture and a subchamber with rich premixture. Those are connected by narrow cylinderical connections. With ignition start in the subchamber, many different kinds of radical is jetted into the main chamber. The premixed gas in main chamber is quickly burned up by the radical ignition in multi-pionts. In this paper, the combustion phenomena in a constant volume combustor having a radical injector are numerically analyzed. The some constants in the reaction rate equation are adjusted by the experimental results tested in the same geometrical chamber. The code is applied on the two combustors in a wide range of equivalence ratio. The results show that the burning time is much shorter in the combustor having radical injector.