• Journal of Powder Materials
• /
• v.14 no.6
• /
• pp.415-421
• /
• 2007

• Fire Science and Engineering
• /
• v.31 no.4
• /
• pp.20-25
• /
• 2017

In the present study, the temperature distribution of droplet diffusion flames was predicted from the measurements of radiative emissions of soot particles formed. In order to predict the temperature distributions, the radiative emissions from soot particles filtered at both 700 nm and 900 nm were measured using CCD cameras and local emission distributions within the flame deconvoluted with Abel transformation were plugged into a two color method. The experimental results obtained from the present study demonstrate that the two color method as tool for temperature measurements is feasible but can introduce approximately 2% maturement errors in a deconvolution process depending on intervals for the line of sight. The estimated error in temperature measurements was found to be within 18 K at 2000 K.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2011.04a
• /
• pp.157-163
• /
• 2011

Combustion of magnesium dust particle were fabricated test devices and combustion experiments were carried out. The ignition delay time were measured in change of magnesium particle mass flow rate in premixed flame. According to increasing magnesium particle mass flow rate, ignition delay time were more shorter. In addition, magnesium dust combustion temperature were measured different particle sizes and o/f ratio by two wavelength pyrometry. Dust combustion flame temperature is almost similarly, through to equivalence ratio, confirm the combustion flame temperature range characteristics.

• Transactions of the Korean Society of Mechanical Engineers
• /
• v.15 no.1
• /
• pp.355-365
• /
• 1991

New definition for the interaction of flames is introduced and interacting turbulent diffusion flames issuing from two rectangular nozzles are investigated on the basis of the definition. Theoretical study through numerical model is carried out and experiment for validation is conducted. The characteristics of interaction due to the variation of major parameters such as nozzle spacing, Reynolds number and nozzle aspect ratio are studied. Results show that strong interaction occurs for small nozzle spacing, small Reynolds number and large aspect ratio. In order of their magnitude, the intensity of interactions on the individual transport mechanism is momentum, heat and mass. It is also found that interaction makes flames longer, tilted and finally merged. Increase of velocities and temperature, decrease of oxygen concentration and depression of turbulence are occurred in the region between flames.

• Journal of the Korean Society of Safety
• /
• v.19 no.3 s.67
• /
• pp.124-129
• /
• 2004

To evaluate the numerical method in simulation of diffusion flames and to see the effects of strain rate and fuel concentration on the flame radius and thickness, the nonpremixed methane-air counterflow flames in microgravity were simulated axisymmetrically by using the MST Fire Dynamics Simulator (FDS). The $1000^{\circ}C$ based flame radius and thickness were investigated for the mole fraction of methane in the fuel stream, $X_m=20,\;50,\;and\;80\%$ and the global strain rates $a_g=20,\;60,\;and\;90s^{-1}$ for each mole fraction. The flame radius increased with the global strain rate while the flame thickness decreased linearly as the global strain rate increased. The flame radius decreased as the mole fraction increased, but it was not so sensitive to the mole fraction compared with the global strain rate. Since there was good agreement in the nondimensional flame thickness obtained with OPPDIF and FDS respectively, it was confirmed that FDS is capable of predicting well the counterflow flames in a wide range of strain rate and fuel concentration.

• 한국가시화정보학회:학술대회논문집
• /
• 2005.12a
• /
• pp.74-79
• /
• 2005

The tribrachial flame in laminar coflow jet has been investigated experimentally with unsteady propagating condition. With adopting various visualization techniques, including OH-PLIF, Rayleigh Scattering technique, it was confirmed that the location of tribrachial point is on the inclined surface of flame and the propagation speed of tribrachial flame was significantly affected by the velocity gradient.

• 한국가시화정보학회:학술대회논문집
• /
• 2005.04a
• /
• pp.61-83
• /
• 2005

연소현상의 가시화를 위한 몇 가지 레이저 진단기법의 응용 예를 소개한다. 이에는 유동 가시화를 위한 반응성 Mie 산란, 주화학종의 계측을 위한 Rayleigh 및 Raman 산란, 미소화학종 계측을 위한 레이저유도 형광법, 온도계측을 위한coherent anti-Stokes Raman 산란법 및 매연계측을 위한 광 소멸/산란법 등이 포함된다. 이러한 기법들이 확산화염, 층류 및 난류 부상 화염, 비예혼합 와도 내의 화염전파, 매연생성 등의 연구에 적용되어 물리적 메커니즘을 이해하는데 유용하게 적용된 사례를 보고한다.

• Transactions of the Korean Society of Mechanical Engineers
• /
• v.14 no.4
• /
• pp.899-906
• /
• 1990

본 연구에서는 자동차엔진에 대한 응용의 일환으로써 밀폐된 축대칭 연소실내 의 정지하고 있는 공기에 분사에 의해 형성된 분무액적들을 점화원을 이용하여 화염을 생성시키고 그에 따른 화염전파 및 낮은 마하수에서의 유동현상과 이상간의 물리적 관 계를 다차원 유한차분법에 의한 물리적인 지배방정식의 동시해법인 ALE(Arbitrary La- ngrangian Eulerian)방법으로 구성되어 있는 CONCHAS-code를 이용하여 해석하고, 연료 액적의 분사각도, 크기 및 연소실내 기체유동의 각속도의 변화에 의한 분무연소의 과 도적특성을 고찰하고자 한다.

• Korean Journal of Optics and Photonics
• /
• v.10 no.6
• /
• pp.468-472
• /
• 1999

평면 레이저 유도 형광법을 사용하여, 가시와 엔진내부에서 연소 과정이 진행되느 동안 OH라디칼 분포에 대한 2차원 영상을 계측하였다. Rayleigh 산란광을 차단하기 위해서 광대역 필터인 UG11을 사용하였으며, OH 형광 영상은 ICCD카메라로 수집하였다. OH라디칼 은 Q1(11)과 P2(8) 파장으로 여기하였다. 엔진 연료로는 iso-octane을 사용하였으며, 이 연료에서는 자체 형광이 발생하지 않았다. 난류를 암시하는 주름진 화염 경계면을 명확하게 관측하였으며, 어떤 영상에서는 화염 섬(flame island)이 나타나기도 한다.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.34 no.8
• /
• pp.761-766
• /
• 2010

The estimation method of the interchangeability in a partial premixed appliance about various compositions of natural gases using equivalent gases, experimentally. The results of the experiment in which equivalent gases were used compared with those obtained in experiments in which natural gases were used; Images of flames, lift-off limits, CO emissions, and incomplete combustion indices in KS standard for the domestic gas range were considered. From the comparison, it was observed that the length and color of the flame of the equivalent gases were almost the same as those of imported natural gases. Further, in the case of gases with Wobbe indices greater than 51 MJ/$m^3$, the KS standard for lifting limits was satisfied. Furthermore, in the case of gases with Wobbe indices less than 56.3 MJ/$m^3$, the CO mole fractions are in the range 95-100 ppm. Hence, the range of Wobbe indices 51-56.3 MJ/$m^3$ was proposed to be the range for interchangeability from the points of view of lifting limits and incomplete combustion, as prescribed in the domestic gas range in the case of imported natural gases.