• 한국가스학회지
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• 제14권3호
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• pp.46-52
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• 2010

삼지화염의 화염안정화 메커니즘 중 중요한 한 가지는 화염전파속도이다. 화염전파속도의 정량적인 규명을 위해 Bilger는 층류 유동이론에 근거하여 혼합분율 기울기에 비선형적으로 연관된 삼지화염전파속도를 제시하였다. 그러나 지금까지의 연구에서는 화염의 곡률 반경과 스칼라소산율에 따른 삼지화염 전파속도에 관하여 논의된 바가 없으며, 본 논문에서는 수치해석을 통해 화염전파속도에 따른 화염의 곡률반경과 스칼라소산율의 관계를 살펴보았다. 본 논문의 결과로 연료의 노즐 출구속도에 따라 화염전파속도가 거의 선형적으로 변화됨을 알 수 있었다. 또 화염전파속도에 따라 스칼라소산율은 비선형적인 감소를 보였으며, 곡률반경은 거의 선형적인 변화를 보임을 알 수 있었다. 또 스칼라소산율에 따른 곡률 반경의 경우 비선형적인 감소를 보였다. 따라서 화염전파속도와 스칼라소산율 및 화염의 곡률반경 사이에 직접적인 연관성이 있는 것을 확인하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제33권4호
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• pp.466-475
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• 2009

A numerical analysis of reactive flow in a liftoff flame is accomplished to elucidate the characteristics of flame propagation velocity and volume integral of reaction rate with the variation of fuel injection velocity at the fuel rich region, fuel lean region and diffusion flame region. The increase of fuel injection velocity enhances flame propagation velocity, but its effect on the flame propagation velocity is not much greater under 4%. The increase of fuel injection velocity affects directly and linearly on the flame surface area in the fuel rich region and so enhances volume integral of reaction rate to accommodate the increment of fuel.

• 한국가스학회지
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• 제15권2호
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• pp.47-56
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• 2011

삼지화염의 화염안정화 메커니즘 중 중요한 한 가지는 화염전파속도이다. 화염전파속도의 정량적인 규명을 위해 Bilger는 층류 유동이론에 근거하여 혼합분율 기울기에 비선형적으로 연관된 삼지화염전파속도를 제시하였다. 그러나 지금까지의 연구에서는 화염의 곡률 반경과 스칼라소산율 및 삼지화염의 화염전파속도에 관한 직접적인 관계에 관하여 제시된 바가 없었다. 본 논문은 실험과 수치해석에 따른 수치해석 결과를 검증하고, 수치해석을 통해 스칼라소산율에 따른 화염전파속도를 확인하였다. 그리고 화염스트레치 분석을 통하여 화염전파속도의 곡률반경 및 스칼라소산율에 따른 의존도를 명확히 하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제34권2호
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• pp.250-258
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• 2010

부상화염에서 노즐직경과 연료유량을 변화하면서 화염전파속도와 연료과농영역, 연료희박영역, 확산화염 영역에서의 체적연소반응속도의 변화 특성을 수치해석을 통하여 살펴보았다. 본 연구에서 사용한 3가지 연료노즐 직경(d=0.25, 0.30, 0.35mm)에서 연료분출속도를 증가시키면 화염전파속도가 증가하지만 변화폭은 4.3%를 넘지 않는다. 연료분출속도를 증가함에 따른 연료량 증가는 직접적이고 선형적으로 체적연소반응속도에 연관되어 있음을 알 수 있었고, 따라서 부상화염에서 연료량의 증가는 화염전파속도 보다 체적연소반응속도가 연료량 변화에 대응함을 알 수 있었다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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• pp.75-76
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• 2015

Lifted flame stabilization mechanism can be explained with constant Schmidt number from the equation of $H^{\ast}_L/d^2_o=const{\times}v_e^{(2Sc-1)/(Sc-1)}$. In this research, a method of local Schmidt number was applied in order to measure edge flame propagation velocities, and edge flame propagation velocity was calculated from the trend between lift-off height and nozzle flow rate.

• 한국가스학회지
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• 제13권3호
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• pp.33-42
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• 2009

부상화염에 대한 연소반응 유동 수치해석을 수행하여 부상높이에 대한 기존 연구 결과들과 비교를 통하여 수치해석 결과의 신뢰성을 검정하였다. 화염전파속도를 결정하는 유동방향변환점을 기존의 연구에서처럼 연료분출속도에 상관없이 일률적인 위치로 선정할 경우 많은 오차를 유발하기 때문에 본 연구에서는 부상화염에서 이론당량비선을 따라 유동속도와 스칼라 소산율 특성을 살펴보았고 화염전파속도를 선정하는 유동방향변환점을 타당하게 선정하는 방법을 정립하였다. 이를 토대로 화염전파속도와 스칼라소산율의 관계식을 도출하여 부상화염에서 화염전파속도 특성을 규명하였다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2004년도 제28회 KOSCO SYMPOSIUM 논문집
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• pp.102-111
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• 2004

Partial quenching structure of turbulent diffusion flames in a turbulent mixing layer is investigated by the method of flame hole dynamics to develope a prediction model for the turbulent lift off. The present study is specifically aimed to remedy the problem of the stiff transition of the conditioned partial burning probability across the crossover condition by adopting level-set method which describes propagating or retreating flame front with specified propagation speed. In light of the level-set simulations with two model problems for the propagation speed, the stabilizing conditions for a turbulent lifted flame are suggested. The flame hole dynamics combined with level-set method yields a temporally evolving turbulent extinction process and its partial quenching characteristics is compared with the results of the previous model employing the flame-hole random walk mapping. The probability to encounter reacting' state, conditioned with scalar dissipation rate, demonstrated that the conditional probability has a rather gradual transition across the crossover scalar dissipation rate in contrast to the stiff transition of resulted from the flame-hole random walk mapping and could be attributed to the finite response of the flame edge propagation.

• 한국연소학회지
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• 제9권2호
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• pp.18-29
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• 2004

Partial quenching structure of diffusion flames in a turbulent mixing layer has been investigated by the method of flame hole dynamics in oder to develope a prediction model for the phenomenon of turbulent flame lift off. The present study is specifically aimed to remedy the shortcoming of the stiff transition of the conditioned partial burning probability across the crossover condition by employing the level-set method which enables us to include the effect of finite flame edge propagation speed. In light of the level-set simulation results with two models for the edge propagation speed, the stabilizing conditions for turbulent lifted flame are suggested. The flame hole dynamics combined with the level-set method yields a temporally evolving turbulent extinction process and its partial quenching characteristics is compared with the results of the previous model employing the flame-hole random walk mapping based on three critical scalar dissipation rates. The probability to encounter reacting state, conditioned with scalar dissipation rate, demonstrated that the conditional probability has a rather gradual transition across the crossover scalar dissipation rate. Such a smooth transition is attributed to the finite response of the flame edge propagation.

• Journal of Mechanical Science and Technology
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• 제18권11호
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• pp.2058-2065
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• 2004

A light collecting probe named Multi-color Integrated Cassegrain Receiving Optics (MICRO) is applied to spark-ignited spherical spray flames to obtain the flame propagation speed in freely falling droplet suspension produced by an ultrasonic atomizer. Two MICRO probes are used to monitor time-series signals of OH chemiluminescence from two different locations in the flame. By detecting the arrival time difference of the propagating flame front, the flame propagation speed is calculated with a two-point delay-time method. In addition, time-series images of OH chemiluminescence are simultaneously obtained by a high-speed digital CCD camera to ensure the validity of the two-point delay-time method by the MICRO system. Furthermore, the relationship between the spray properties measured by phase Doppler anemometer (PDA) and the flame propagation speed are discussed with three different experimental conditions by changing the fuel injection rate. It was confirmed that the two-point delay-time method with two MICRO probes is useful and convenient to obtain the flame propagation speed and that the flame propagation speed depends on the spray properties.

• 한국안전학회지
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• 제19권3호
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• pp.20-25
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• 2004

In order to obtain the flame Propagation speed in freely falling droplet suspension Produced by an ultrasonic atomizer, a light collecting probe named Multi-color Integrated Cassegrain Receiving Optics (MICRO) is applied to spark-ignited spherical spray flames. Two MICRO probes are used to monitor time-series signals of OH chemilumine-scence from two different locations in the flame. The flame propagation speed is calculated by detecting the arrival time difference of the propagating flame front. In addition, time-series images of OH chemiluminescence are simultaneously obtained by a high-speed digital CCD camera to ensure the validity of the MICRO system. Furthermore, relationship between the spray properties measured by phase Doppler anemometer (PDA) and the flame propagation speed are discussed with k different experimental conditions by changing the fuel injection rate. It was confirmed that the MICRO probe system was very useful and convenient to obtain the flame propagation speed and that the flame propagation speed was different depending on the spray properties.