• Journal of Mechanical Science and Technology
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• 제20권2호
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• pp.242-250
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• 2006

Detailed structures of the counterflow flames formed for different inlet fluid temperatures and different amount of additives are studied numerically. The detailed chemical reactions are modeled by using the CHEMKIN-II code. The discrete ordinates method and the narrow band based WSGGM with a gray gas regrouping technique (WSGGM-RG) are applied for modeling the radiative transfer through non-homogeneous and non-isothermal combustion gas mixtures generated by the counterflow flames. The results compared with those obtained by using the SNB model show that the WSGGM-RG is very successful in modeling the counterflow flames with non-gray gas mixture. The numerical results also show that the addition of $CO_2\;or\;H_2O$ to the oxidant lowers the peak temperature and the NO concentration in flame. But preheat of fuel or oxidant raises the flame temperature and the NO production rates. $O_2$ enrichment also causes to raise the temperature distribution and the NO production in flame. And it is found that the $O_2$ enrichment and the fuel preheat were the major parameters in affecting the flame width.

• International Journal of Aeronautical and Space Sciences
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• 제13권3호
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• pp.386-397
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• 2012

The stability and structure of bluff-body stabilized hydrogen flames were investigated numerically and experimentally. The velocity of coflowing air was varied from subsonic velocity to a supersonic velocity of Mach 1.8. OH PLIF images and Schlieren images were used for analysis. Flame regimes were used to classify the characteristic flame modes according to the variation of the fuel-air velocity ratio, into jet-like flame, central-jet-dominated flame, and recirculation zone flame. Stability curves were drawn to find the blowout regimes and to show the improvement in flame stability with increasing lip thickness of the fuel tube, which acts as a bluff-body. These curves collapse to a single line when the blowout curves are normalized by the size of the bluff-body. The variation of flame length with the increase in air flow rate was also investigated. In the subsonic coflow condition, the flame length decreased significantly, but in the supersonic coflow condition, the flame length increased slowly and finally reached a near-constant value. This phenomenon is attributed to the air-entrainment of subsonic flow and the compressibility effect of supersonic flow. The closed-tip recirculation zone flames in supersonic coflow had a reacting core in the partially premixed zone, where the fuel jet lost its momentum due to the high-pressure zone and followed the recirculation zone; this behavior resulted in the long characteristic time for the fuel-air mixing.

• 한국추진공학회지
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• 제21권5호
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• pp.54-60
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• 2017

연소불안정 연구의 일환인 화염전달함수에서 나타나는 gain의 특성을 파악하기 위하여 비연소상태에서의 전달함수를 도입하여 화염전달함수에서의 특성과 비연소전달함수의 특성에 대한 원인을 파악하고자 하였다. 비연소 전달함수를 획득하기 위하여 질소와 이산화탄소를 활용하였으며, 입력값과 출력값을 계측하기 위하여 열선풍속계를 이용하였다. 비연소 전달함수에서의 gain과 주파수의 peak는 비활성기체의 밀도와 유량에 대하여 영향을 받는 것을 확인하였다. 또한 연료공급라인에서의 음향학적 공진주파수가 peak 주파수에 영향을 주는 것을 확인하였다.

• 한국추진공학회지
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• 제4권4호
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• pp.78-86
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• 2000

Mach 1.8의 동축공기를 갖는 수소 난류 화산 화염의 특성을 이해하는 것이 본 연구의 목적이다. 화염길이와 연료유동의 자취에 대한 직접사진, Acetone PLIF, Mie scattering, 수치해석법을 이용하여 화염의 구조를 분석하였다. 연료의 유속를 고정시켰을 때, 공기의 유속 증가에 따른 변화를 측정하였다. 아음속 화염의 길이는 급격히 감소한 반면, 초음속 화염의 길이는 완만하게 증가하였다. 또한 연료 노즐 립의 두께 변화에 따른 화염의 소염 특성을 관찰하였다. 노즐 립의 두께에 따라 화염 안정성이 증가하였는데 이는 초음속 화염의 안정화를 위한 최소 두께 값이 존재함을 나타낸다. 유동장 구조를 분석한 결과, 연료 제트가 고압영역에 가로 막혀서 축방향 모멘텀을 잃고, 저산란 영역이 만들어지는 것을 확인하였다. 또한, 모멘텀을 잃은 연료가 재순환 영역을 따라 순환하면서 긴 체류시간을 갖기 때문에 예혼합 영역이 만들어 졌음이 밝혀졌다.

• 한국안전학회지
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• 제39권1호
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• pp.1-8
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• 2024

Commercial gas stoves feed primary air to the burner and burn the fuel-air mixture in a partially premixed combustion. This mechanism produces carbon monoxide during combustion. In this study, design parameters of a commercial gas stove were optimized by considering the carbon monoxide emission. Gas consumption rate, carbon monoxide emission, and water boiling temperature as a heating performance were determined. Carbon monoxide emission was measured using a Korean Industrial Standards standard collector. Water boiling temperature was measured by first soaking the pot in water for approximately 10 min and then heating the pot filled with water. A thermocouple was installed inside the pot. Carbon monoxide increased as the nozzle diameter was increased and the burner-pot height was decreased. This result was due to the insufficient mixing between the fuel and air. Heating performance was enhanced when the nozzle diameter was increased and the burner-pot height was decreased. However, the heating performance deteriorated when the nozzle diameter was 1.8 mm and the burner-pot height was reduced to 50 mm. This phenomenon was due to the formation of a flame on the side of the pot. A merit factor was defined to find the optimal design parameters to satisfy gas consumption rate, carbon monoxide emission, and heating performance. Optimal design values were established to be a nozzle diameter of 1.5 mm and a burner-pot height of 60 mm.

• 한국항공우주학회지
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• 제44권7호
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• pp.603-610
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• 2016

본 논문에서는 석탄으로부터 생성된 합성천연가스(SNG)의 다양한 연료 조성에 대한 배기가스 배출 특성 및 희석제에 대한 NOx배출 저감에 대해 기술하였다. 예혼합거리가 짧은 부분 예혼합 가스터빈 연소기에서 SNG 연료조성에서의 수소 비율과 입열량, 당량비를 조절해 가며 연소특성을 관찰하였다. 수소 비율에 따른 NOx 배출지수는 유사하게 나타났고, 화염가시화를 통해 화염의 특성을 파악할 수 있었다. CO 배출의 경우 당량비 1 구간에서 특이점이 나타났으며, 이를 화염의 자발광 이미지와 자발광 강도를 통하여 원인을 파악할 수 있었다. 또한 높은 NOx 배출을 저감하기 위하여 질소($N_2$)와 이산화탄소($CO_2$) 희석제를 사용하여 희석제 공급량에 대한 저감 효과를 파악하였다. 이로부터 희석제의 비열과 열용량이 연소로부터 발생한 연소열을 흡수하여 열화에 의한 NOx 배출을 저감하는 효과를 확인하였다.