• 한국연소학회:학술대회논문집
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• 한국연소학회 2002년도 제25회 KOSCI SYMPOSIUM 논문집
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• pp.25-31
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• 2002

For the better understanding of the stability of turbulent combustion, more researches on extinction and re-ignition are needed. Flame interactions in non-premixed flame have also not been greatly researched. We made a hybrid twin jet flame, the combinations of diffusion flame and partially-premixed diffusion flame, in a twin jet counterflow configuration. The extinction limits of a crossed twin jet counterflow have been extended in comparison with those of a one-dimensional counterflow because of flame interactions through heat transfer and joint ownership of various radicals. Besides, we have obtain ignition $Damk\"{o}hler$ number by experimental method without external ignition source using the extinction characteristic in a crossed twin jet counterflow flame. From results, we can identify the hysteresis between extinction and ignition $Damk\"{o}hler$ number in S-curve.

• 대한기계학회논문집B
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• 제23권1호
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• pp.114-122
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• 1999

Reignition as special cases of acoustic pressure responses of flame are numerically studied by employing methanol droplet flame as a laminar flamelet. Quasi-steady flame responses occur in the range of small amplitude, low frequency oscillation. Reignition phenomena can occur when, by increasing the frequency of large amplitude acoustic pressure, the magnitude of characteristic acoustic time is the same order of that of characteristic reaction time of flames. And more increasing of amplitude of acoustic pressure induces the direct extinction of flame. Flame can sustain its own intensity even under the steady extinction temperature in case of high frequency acoustic oscillation, and this tendency is remarkable with increasing frequency. Reignition regime with respect to amplitude and frequency of acoustic pressure doesn't exist in low frequency($10^2$ Hz, in this study), but broadens with frequency of acoustic pressure.

• 대한기계학회논문집B
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• 제27권10호
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• pp.1401-1411
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• 2003

A two-dimensional direct numerical simulation was performed to investigate the flame structure of CH$_4$$N_2$-air counterflow nonpremixed flame interacting with a single vortex. The detailed transport properties and a modified 16-step augmented reduced mechanism based on Miller and Bowman's detailed chemistry were adopted in this simulation. The characteristic vortex and chemical time scales were introduced to quantify and investigate the extinction phenomenon during a flame-vortex interaction. The results showed that fuel- and air-side vortex cause an unsteady extinction. In this case, the flame interacting with a vortex was extinguished at much larger scalar dissipation rate than steady flame. It was also found that the air-side vortex extinguished a flame more rapidly than the fuel-side vortex. Furthermore, it was noted that the degree of unsteady effect experienced by a flame can be investigated by comparing the above two characteristic time scales, and this analysis could give an appropriate reason for the results of the previously reported experiment.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.130-133
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• 2009

액체 로켓 엔진의 경우 작동초기인 점화와 마지막의 소염시의 추진제 공급 순서는 안정적으로 시스템을 운영하는데 많은 영향을 끼친다. 안정적인 엔진의 작동확인을 위해 점화할 때 공급순서와 소염할 때 추진제의 공급 순서를 바꾸어 가면서 연소 실험을 수행 하였다. 본 연구에 사용된 분사기는 과산화수소와 케로신을 추진제로 사용하는 동축 스월형이며, 점화 방식은 촉매 점화를 방식을 사용하였다. 본 실험을 통해서 액체로켓엔진의 연소 시험을 안정적으로 수행하기 위해 점화와 소염할 때의 최적의 시퀀스를 찾아내었다.

• 한국수소및신에너지학회논문집
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• 제29권6호
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• pp.668-679
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• 2018

Experimental and numerical data were compared through a counterflow burner for the characteristic of basic flame about SNG- C11. In order to use the numerical mechanism accurately, the validation was carried out at strain rate ($a_g=30$, $120s^{-1}$) and the UCSD model showed satisfactory results. The effective Lewis number of the extinction boundary, and the behavior of extinction for the symmetric flames of the SNG-C11, could be explained through the trend of $Le_V$, and the flame of the extinction condition was inspected by the major species, key radicals and the chemical reaction paths. The interactions phenomenon in the merged flames has chemical reaction path for producing $HO_2$ were generated at stagnation point. It can be expected the one of major factors in interaction phenomenon.

• 한국추진공학회지
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• 제23권2호
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• pp.21-26
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• 2019

신속하게 감압되는 환경에 노출되면 연소중인 고체추진제는 소화가 일어난다. 연소되는 중인 고체추진제를 소화하는데 필요한 압력 감소율인 임계감압률을 찾는 실험이 진행되었다. 이를 위해 감압 시점, 감압 속도, 초기 압력, 최종 압력을 조절할 수 있는 감압연소기를 설계 및 제작하였다. 이 실험의 결과는 특정 AP/HTPB 복합고체추진제 조성에서 소화와 비소화 사이의 경계를 결정하는데 사용되었다. 실험 결과 초기 압력과 최종 압력이 소화를 위한 임계감압률에 큰 영향을 미치는 것으로 나타났다.

• 한국수소및신에너지학회논문집
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• 제34권1호
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• pp.47-58
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• 2023

Experimental data conducted by Colson et al. and numerical data conducted in this study were compared through counterflow flames to understand of the characteristic of basic flame about mixture of ammonia/methane. In order to use the suitable numerical mechanism, the validation was performed using total four mechanisms and the Okafor's mechanism showed satisfactory experimental results. The extinction boundary of the stability map could be explained through the effective Lewis number and the trend of LeD. The extinction behavior of the flame was different under the lean and rich symmetric conditions and it was investigated by the major variables, global strain rate (a_g) and mole fraction of ammonia (Ω_NH3).

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2002년도 춘계학술대회 논문집 디스플레이 광소자 분야
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• pp.97-100
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• 2002

We analyzed the excitation coefficients and the extinction ratio as a function of waveguide width, center to center distance, and angle of input waveguide for a directional coupler. The variation of thc difference between excitation coefficients is similar to that of the extinction ratio. Also, the smaller the difference between those is, the better the extinction ratio is. This concept will have application to devices using optical coupling.

• 한국광학회지
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• 제16권5호
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• pp.446-449
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• 2005

방향성 결합기의 각종 설계 구조변경에 대해 소멸비 특성의 변화를 직관적으로 예측하기 쉽지 않으므로 각 구조마다 매번 번거로운 특성 계산의 반복 작업이 수행되었다. 본 논문에서는 방향성 결합기의 설계구조 변수의 조절에 따른 소멸비 특성 변화를 체계적으로 계산하였고, 이 특성변화의 일반적인 경향을 파악하였다. 즉, 도파로 간격을 입력 도파로의 폭으로 규격화하면 이 변화 경향을 일반화하는 특성곡선을 얻을 수 있는 것으로 파악되었다. 이때, 정규화주파수 v와 도파간격비율 d가 큰 구조일수록 소멸비를 높일 수 있었고, d를 동일하게 유지한 여러 경우의 구조에 대해서는 v의 변화에 따른 소멸비 특성곡선이 일치하는 것을 보였다. 이러한 소멸비 특성의 일반화 경향은 높은 소멸비 특성을 유지하면서도 소자를 작게 설계하거나 파장분리기의 설계에 유용하게 활용될 수 있으므로 1310/1550 nm 파장 분리기의 설계와 제작에 적용하여 그 효용성을 확인하였다.

• ETRI Journal
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• 제27권3호
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• pp.267-272
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• 2005

The transmission performance of optical labeling based on a combined frequency shift keying/amplitude shift keying (FSK/ASK) format is studied by numerical simulation. The simulation demonstrates that the bit-error ratio (BER) characteristic of an ASK signal is limited by the extinction ratio, received optical power, and dispersion, simultaneously. However, an FSK signal is mainly limited by the extinction ratio (ER) and received optical power when the peak spectrum, which is used to detect the FSK signal, is relatively narrow.