• 한국연소학회:학술대회논문집
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• 한국연소학회 2005년도 제31회 KOSCO SYMPOSIUM 논문집
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• pp.221-228
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• 2005

The tribrachial flame in laminar coflow jet has been investigated experimentally with unsteady propagating condition. In this experiment, we found that the tribrachial point has an angle of flame surface because the location of tribrachial point is not on the base point of flame but on the inclined surface of flame. This angle of Flame surface at tribrachial point are increasing when the flame is approaching to the nozzle exit. With considering this angle of flame surface, the radial velocity gradient can affect flame propagation speed by increasing flow-stretch effect. The propagation speed of tribrachial flame was calculated with including above stretch effect. The speed decreases with increasing velocity gradient due to the increment of stretch effect.

• 한국방재학회 논문집
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• 제9권5호
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• pp.57-62
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• 2009

경사면에서의 지표 연소물질에 대한 화염확산은 경사각변화에 따라 화염이 경사면과 가까워져 열전달이 많이 이루어져 확산이 빠르게 이루어진다. 기존 연구에서는 경사면에 대한 화염각 변화를 고려하지 않고 일반적으로 경사각의 기울어짐으로 인해 화염이 그 만큼 지표면과 가까워지는 것을 적용하였다. 따라서 본 연구에서는 경사면에서의 실제 화염의 성상에 대해 실험하였다. 그 결과 경사에 따른 화염기울기 산정식을 제안 하였고 경사조건에서의 화염기울기와 화염확산속도와의 관계에 대해 기술하였다.

• 한국화재소방학회논문지
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• 제23권5호
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• pp.90-95
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• 2009

산불의 확산에 있어 바람은 매우 중요한 인자이다. 바람은 또한 지형에 따라 변화되며 이로 인해 다른 확산형태를 가지게 된다. 따라서 산불의 확산속도 해석을 위해 먼저 풍속에 따른 화염각 변화를 살펴볼 수 있다. 이는 바람에 의해 변화된 화염각으로 인해 미연소 지표 대상물에 열전달의 차이를 가져오기 때문이다. 풍속이 증가할수록 화염과 지표면이 가까워짐으로 인해 열전달이 증가되어 미연소물질이 착화온도에 빨리 도달하게 되어 화염의 확산속도가 빨라지게 된다. 따라서 본 연구에서는 바람에 의한 화염각 변화 산정식을 Froude number 관계식을 이용한 수치해석과 실험을 통해 제시하였다. 그 결과, Froude number 계수 A=1.85를 제시하였고 제시된 식에 대한 실험 화염각의 평균 오차각은 약 $3.3^{\circ}$로 다른 모델식에 비해 실험값과 유사한 결과를 나타내었다. 향후, 이 연구를 통해 열전달 수치해석을 통한 화염확산연구에 활용될 수 있을 것으로 사료된다.

• 한국가시화정보학회:학술대회논문집
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• 한국가시화정보학회 2005년도 추계학술대회 논문집
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• pp.74-79
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• 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.

• 한국연소학회지
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• 제12권1호
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• pp.1-10
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• 2007

Analytical investigation of acoustic wave scattering from turbulent premixed flames was conducted to evaluate the acoustic energy amplification/damping. Such acoustic energy change is attributed to the acoustic velocity jump due to flame's heat release. Small perturbation method up to second order and stochastic analysis were utilized to formulate net acoustic energy and the energy transfer from coherent to incoherent energy. Randomly wrinkled flame surface is responsible for the energy transfer from coherent to incoherent field. Nondimensional parameters that govern net acoustic energy were determined: rms height and correlation length of flame front, incident wave frequency, incidence angle, and temperature ratio. The dependence of net acoustic energy upon these parameters is illustrated by numerical simulations in case of Gaussian statistics of flame front. Total net energy was amplified and the major factors that affect such energy amplification are incidence angle and temperature ratio. Coherent (incoherent) energy is damped (amplified) with rms height and correlation length of flame front.

• 한국재료학회지
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• 제32권12호
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• pp.553-559
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• 2022

In this work, the ablation behavior of monolith ZrB₂-30 vol%SiC (Z30S) composites were studied under various oxy-acetylene flame angles. Typical oxidized microstructures (SiO₂/SiC-depleted/ZrB₂-SiC) were observed when the flame to Z30S was arranged vertically. However, formation of the outmost glassy SiO₂ layer was hindered when the Z30S was tilted. The SiC-depleted region was fully exposed to air with reduced thickness when highly tilted. Traces of the ablated and island type SiO₂ were observed at intermediate flame angles, which clearly verified the effect of flame angle on the ablation of the SiO₂ layer. Furthermore, the observed maximum surface temperature of the Z30S gradually increased up to 2,200 ℃ proving that surface amorphous silica was continuously removed while monoclinic ZrO₂ phase began to be exposed. A proposed ablation mechanism with respect to flame angles is discussed. This observation is expected to contribute to the design of complex-shaped UHTC applications for hypersonic vehicles and re-entry projectiles.

• 한국수소및신에너지학회논문집
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• 제23권5호
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• pp.493-502
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• 2012

Syngas laminar burning velocity measurements were carried out at atmospheric pressure and ambient temperature using the Bunsen flame configuration with nozzle burner as a fundamental study on flame stability of syngas fuel. Representative syngas mixture compositions ($H_2$:CO) such as 25:75%, 50:50% and 75:25% and equivalence ratios from 0.5 to 1.4 have been conducted. Average laminar burning velocities have been determined by the stabilized nozzle burner flames using the angle method, radical surface area method and compared with the data obtained from the other literatures. And the results of each experimental methodologies in the various composition ratios and equivalence ratios were coincided with the result of numerical simulation. Especially, it was confirmed that there was necessary to choice a more accurate measurement methodology even the same static flame method for the various composition ratios of syngas fuel including hydrogen. Also, it was reconfirmed that the laminar burning velocities gradually increased with the increasing of hydrogen content in a fuel mixture.

• 한국연소학회지
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• 제8권4호
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• pp.15-23
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• 2003

The zone conditional two-fluid equations are derived and validated against DNS database of a premixed turbulent flame. The conditional statistics of major flow variables are investigated to understand the mechanism of flame generated turbulence. The flow field in burned zone shows substantially increased turbulent kinetic energy, which is highly anisotropic due to reaction kinematics across thin f1amelets. The transverse component may be larger than the axial component for a distributed pdf of the flamelet orientation angle, while the opposite occurs due to redistribution of turbulent kinetic energy and flamelet orientation normal to the flow at the end of a flame brush. The major source or sink terms of turbulent kinetic energy are the interfacial transfer by the mean reaction rate and the work terms by fluctuating pressure and velocity on a flame surface. Ad hoc modeling of some interfacial terms may be required for further application of the two-fluid model in turbulent combustion simulations.

• Composites Research
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• 제23권5호
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• pp.1-7
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• 2010

NBR과 강판의 접착특성을 향상시키기 위해 대기압 화염 플라즈마(APFP) 처리 장치가 사용되었다. 가장 우수한 접착특성을 나타내는 최적 조건을 찾기 위해 다양한 처리 조건(처리속도, 거리)에 따른 효과에 대한 실험적 연구를 하였다. 주어진 조건에서 버너 포트와 강판의 최적 거리는 40mm, 버너 포트의 최적 처리속도는 50m/min였다. APFP 처리 후 접착제를 두 번 도포한 강판의 접착강도는 접착제만 도포한 경우보다 20.5% 증가하였다. 본 연구를 통해서 대기압 화염 플라즈마 처리에 의한 강판의 표면개질이 고무와 강의 접착강도를 증가시키는 적절하면서도 응용이 가능한 방법임을 확인하였다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2006년도 제32회 KOSCO SYMPOSIUM 논문집
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• pp.96-104
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• 2006

In the present paper, the effects of combustion instability on flow structure and flame dynamic with the configurations of burner exit in a model gas turbine combustor are investigated using large eddy simulation(LES). A G-equation flamelet model is employed to simulate the unsteady flame behavior. As a result of mean flow field, the change of divergent half angle(${\alpha}$) at burner exit results in variations in the size and shape of the central toroidal recirculation(CTRZ) as well as flame length by changing corner recirculation zone(CRZ). The case of ${\alpha}=45^{\circ}$ show smaller size and upstream location of CTRZ than that of $90^{\circ}$ and $30^{\circ}$ by the development of higher swirl velocity. The flame length in the case of ${\alpha}=45^{\circ}$ is the most shortest, while that in the case of ${\alpha}=30^{\circ}$ is the longest by the decrease of effective reactive area with the absence of CRZ. Through the analysis of pressure fluctuation, it is identified that the case of ${\alpha}=45^{\circ}$ shows the most largest damping effect of pressure oscillation in all configurations and brings in the noise reduction of 2.97dB, comparing with that of ${\alpha}=30^{\circ}$ having the largest pressure oscillation. These reasons are discussed in detail through the analysis of unsteady phenomena about recirculation zone and flame surface. Finally the effects of flame-acoustic interaction are evaluated using local Rayleigh parameter.