• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2010년 춘계학술대회논문집
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• pp.252-257
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• 2010

The availability of the thermal energy has been deeply recognized recently to encourage the cascade usage of thermal energy from combustion. Within the frame work, a 1 kW class Stirling engine based cogeneration system has been proposed for a unit of a distributed energy system. The capacity has been designed to be adequate for the domestic usage, which requires high compactness as well as low emission and noised. To develop a highly efficient system with satisfying these requirements, a premixed slot flame burner has been proposed and a series of numerical simulation has been performed to establish a design tool for the combustion chamber. The thermal radiation model has been found to highly affect the computational results and a proper resolution to analyze the heat transfer characteristics of the high temperature heat exchanger. Finally, the combustion characteristics of the premixed flame with the metal fiber type burner has been studied.

• 대한기계학회논문집B
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• 제21권6호
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• pp.822-829
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• 1997

A catalytic burner was studied which can be used as a heater operated in medium temperature. Noble metal catalysts (Pd/NiO) were used, which were supported on alumina wash coated honeycomb. The maximum heat-resisting temperature of the catalyst is about 900.deg. C. Combustion efficiency of the catalytic burner reached more than 99.5 % at the excess air ratio above 1.25.NOx emissions were lower than 1.0 ppm at all operation conditions. The operation condition for a stable catalytic combustion was obtained. It was dependent on the catalyst thickness. The 30 mm thick catalyst showed the widest stable catalytic combustion region. Stable catalytic combustion region of 30 mm thick catalyst was the operation condition of excess air ratio 1.25 - 1.75 and heat flux 7 - 14 kcal/h center dot cm$^{2}$.

• 한국가스학회지
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• 제15권4호
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• pp.44-50
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• 2011

폭발한계는 가연성물질의 화재 및 폭발위험성을 결정하는데 주요한 특성치 가운데 하나이다. 본 연구에서, 에테르류의 폭발하한계와 상한계에 대해 연소열과 화학양론계수를 이용하여 예측하였다. 제시된 예측식에 의한 예측값은 문헌값과 적은 오차범위에서 일치하였다. 제시된 방법론을 사용하여 다른 에테르류의 폭발한계 예측이 가능해졌다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2012년도 제44회 KOSCO SYMPOSIUM 초록집
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• pp.253-255
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• 2012

This study has numerically investigated the combustion processes in the bilayer porous media. To account for the velocity transition and diffusion influenced by solid matrix, porosity effects are included in the governing equations. Heat transfer coefficient is calculated by Nusselt number to reflect the effect of gas velocity, pore diameter, and material properties. Numerical results indicate that the present approach is capable of the essential features of the premixed combustion in the porous burner, in terms of the precised flame structure, pollutant formation, and flame stabilization. It is also found that heat transferred from the downstream flame zone is conducted to the upstream flame region through the solid matrix and the preheated mixture. By increasing the inlet velocity, the solid temperature of upstream is cooling down.

• 한국연소학회지
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• 제8권3호
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• pp.31-37
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• 2003

The objective of this work is to investigate the effect of swirl, injection pressure and pilot injection on D.I.Diesel combustion by using a transparent engine system. The test engine is equipped with common rail injection system to obtain high pressure and to control injection timing and duration. In this study, the combustion analysis and steady flow test were conducted to estimate the heat release rate from in-cylinder pressure and pilot injection was investigated by using LII technique. As the results, high injection pressure was found to shorten ignition delay as well as enhance peak pressure and heat release rate was greatly affected by injection timing and pilot injection. In addition, the results showed that the period of soot formation corresponded to the diffusion flame.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2001년도 제17회 학술발표회 논문초록집
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• pp.61-67
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• 2001

Hybrid propulsion systems provide many advantages in terms of stable operation and safety. However, classical hybrid rocket motors have lower fuel regression rate and combustion efficiency compared to solid propellant rocket motor. The recent research efforts are focused on the improvement of volume limitation and regression rate in the hybrid rocket engine. The present study has numerically investigated the combustion processes in the hybrid rocket engine. The turbulent combustion is represented by the eddy breakup model and Hiroyasu and Nagle and Strickland-Constable model are used for soot formation and soot oxidation. Radiative heat transfer is modeled by finite volume method. To reduce the uncertainties for convective heat transfer near solid fuel surface having strong blowing effect, the Low Reynolds number k-$\varepsilon$ turbulent model is employed. Based on numerical results, the detailed discussion has been made for the turbulent combustion processes in the vortex hybrid rocket engine.

• 한국연소학회지
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• 제19권1호
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• pp.1-10
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• 2014

An analytical study on performance evaluation of superdetonative mode ram accelerator was conducted for understanding the experimental result. The quasi-one dimensional continuum, momentum, energy equations were solved under the assumption of inviscid flow. It would be noticeable that experimental result could be analytically simulated with the assumptions of inlet shockwave, temperature dependent specific heat, and additional aluminum combustion due to ablation of aluminum projectile in superdetonative operation mode. The acceleration of ram accelerator was comparable to experimental result with the consideration of the additional aluminum combustion energy by ablation of projectile. As result, the experimental result with the aluminum projectile could be affected by heat of aluminum.

• 한국화재소방학회논문지
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• 제29권6호
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• pp.13-19
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• 2015

이 연구에서는 인(P)-질소(N)의 첨가제로 처리된 리기다 소나무의 연소성을 시험하였다. 15 wt%의 인-질소 첨가제 수용액으로 리기다 소나무에 3회 붓칠하여 실온에서 건조시킨 후, 콘칼로리미터(ISO 5660-1)를 이용하여 연소성을 시험하였다. 그 결과, 인-질소 첨가제로 처리한 시험편은 피로인산/암모니움이온 첨가제로 처리한 시험편을 제외하고, 처리하지 않은 시험편에 비하여 착화시간이 90~148 s으로 길었다. 또 불꽃소멸시간은 556~633 s으로서 길게 측정되었다. 그러나 인-질소 첨가제로 처리한 시험편은 무처리 시험편에 비해 각각 12.5~43.4% 정도 높은 평균열방출률과 11.8~43.1% 정도 높은 총열방출률을 나타내었다. 특히, 인-질소 첨가제로 처리한 시험편의 유효연소열은 15.60~18.37MJ/kg으로서 순수 리기다 소나무 시험편에 비하여 2.9~17.5% 낮게 나타났다. 따라서 인-질소 첨가제로 처리한 시험편은 순수 리기다 소나무 시험편에 비하여 연소 억제성을 부분적으로 향상시켰다.

• 한국화재소방학회논문지
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• 제21권3호
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• pp.41-46
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• 2007

본 연구에서는 지표화의 연소물질인 소나무와 굴참나무 낙엽에 대해 일정한 외부 복사열에 의한 연소특성을 분석하였다. 일정한 외부 복사열에 노출된 낙엽의 착화시간, 착화온도, 임계열유속, 질량감소속도를 측정하기 위해 낙엽의 종류별로 5개의 시료를 사용하였으며, 낙엽에 복사열을 노출시키기 위해 Mass loss calorimeter를 사용하였다. 시료 용기의 크기는 $100\;mm{\times}100\;mm{\times}12\;mm$로 소나무와 굴참나무 낙엽을 건조 후 분쇄하여 사용하였다. 연구결과, 소나무 낙엽과 굴참나무 낙엽의 시료에서 외부 복사열이 $9\;kW/m^2$ 미만에서는 착화가 발생하지 않았다. 또한, 연소시간 동안 표면온도 변화는 굴참나무 낙엽에 비해 소나무 낙엽이 더 오랜 시간동안 고온을 유지함을 알 수 있었으며, 최대질량감소속도와 평균질랑감소속도에 있어서는 굴참나무 낙엽이 소나무 낙엽 보다 더 빠르게 진행됨을 알 수 있었다. 향후, 연소특성에 대한 구체적인 연소반응 특성에 대한 실험연구가 필요할 것으로 판단된다.

• 공업화학
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• 제22권4호
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• pp.439-443
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• 2011

수산화마그네슘이 첨가된 저밀도 폴리에틸렌-에틸렌 비닐 아세테이트 혼합물의 연소성을 시험하였다. 저밀도 폴리에틸렌-에틸렌 비닐 아세테이트에 수산화마그네슘을 40~80 wt% 첨가하여 용융 혼합하고 성형 후 콘칼로리미터(ISO 5660-1)를 이용하여 그의 연소성을 시험하였다. 수산화마그네슘을 첨가한 시험편은 첨가하지 않은 시험편에 비하여 그의 연소성이 감소하였다. 이것은 순수한 저밀도 폴리에틸렌-에틸렌 비닐 아세테이트에 첨가한 수산화마그네슘의 흡열 분해 때문에 연소 억제성이 향상된 것으로 생각된다. 수산화마그네슘을 첨가한 시험편은 첨가하지 않은 시험편에 비해 낮은 최대열방출률과 낮은 유효연소열을 나타내었고, 수산화마그네슘 함량이 증가할수록 착화시간은 길어지고, 최대열방출률은 감소하였다.