• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.1
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• pp.72-79
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• 2018

An experimental study was performed to investigate the chemiluminescence characteristics in the spray combustion of ultransonically atomized kerosene. The radical intensity of the spray flame was measured using an ICCD camera and the amount of fuel consumed was obtained by a precise flow-rate measurement technique during combustion. Fuel consumption increased linearly with the increase in carrier-gas flow rate, and typical group combustion, which is a characteristic of spray combustion, was observed. It was found from the analysis of chemiluminescence that the maximum emission intensities of OH and CH radicals decrease, and they move downstream resulting in the increase in a vivid reaction zone as the spray flow rate increases.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.39 no.6
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• pp.485-496
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• 2015

The present study presents experimental results on the characteristics of emission spectra of kerosene/air swirl flames. The aviation fuel Jet A-1, which is used for the liquid rocket engines of the Korea Space Launch Vehicle, is used with three different swirlers to investigate the swirl strength effects. The emission spectra from the flames are measured with a spectrometer as the swirl strength and combustion air temperature are varied. Chemiluminescence intensities of $OH^*$, $CH^*$ and $C_2{^*}$ are identified from the spectra. The chemiluminescence intensities from the kerosene flames show sensitivity to the swirl strength and are affected by changes in the combustion air temperature. Among the three radicals of interest, $C_2{^*}$ show the most significant changes in chemiluminescence intensity with the swirl strength and equivalence ratio. The intensity ratios $I_{OH^*}/I_{CH^*}$ and $I_{C_2{^*}}/I_{CH^*}$ are adequate for indicating changes in the equivalence ratio with the air and fuel mass flow rates, respectively.

• Proceedings of the Optical Society of Korea Conference
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• 2003.02a
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• pp.152-153
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• 2003

최근 양자점 (Quantum Dot-QD)에 대한 관심이 기초 물리학뿐만 아니라 광전소자 응용 측면에서 많은 주목을 끌고 있다. 특히, 자발 형성방법으로 성장시킨 양자점 (Self-assembled QD)을 이용하여 Laser Diode와 같은 광소자에 응용한 결과가 발표되고 있다. 이러한 자발형성 방법으로 성장한 양자점을 광통신에 응용하기 위해서는 발광파장을 제어할 필요성이 있다. 따라서 본 연구에서는 단거리 광통신에 응용 될 수 있는 1.3 $\mu$m 영역과 장거리 광통신에 사용하는 1.55 $\mu$m 영역으로 InAs 양자점의 발광 파장을 변조한 결과에 대하여 분석하였다. (중략)

• Electrical & Electronic Materials
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• v.15 no.2
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• pp.21-27
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• 2002

• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.5
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• pp.10-19
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• 2012

To eliminate the onset of combustion instabilities and develop effective approaches for control, flame structure is very important. In this study, we conducted experiments under various operating conditions with a model gas turbine combustor to examine the relation of combustion instability and flame structure by OH chemiluminescence and laser diagnostics of He-Ne laser absorbtion system. The swirling LNG($CH_4$)/air flame was investigated with overall equivalence ratio of 1.2 and dump plane fuel-air mixture velocity 25 ~ 70 m/s. We founded that the combustion instability phenomenon occurs at lower mixing velocity and higher mixing velocity conditions. We also concluded that fluid dynamical vortex frequency has major effects on the combustion instability characteristics at lower mixing velocity condition.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.367-376
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• 2012

To eliminate the onset of combustion instabilities and develop effective approaches for control, flame structure is very important. In this study, we conducted experiments under various operating conditions with a model gas turbine combustor to examine the relation of combustion instability and flame structure by OH chemiluminescence and laser diagnostics of He-Ne laser absorbtion system. The swirling LNG(CH4)/air flame was investigated with overall equivalence ratio of 1.2 and dump plane fuel-air mixture velocity 25 ~ 70 m/s. We founded that the combustion instability phenomenon occurs at lower mixing velocity and higher mixing velocity conditions. We also concluded that fluid dynamical vortex frequency has major effects on the combustion instability characteristics at lower mixing velocity condition.

• Proceedings of the Optical Society of Korea Conference
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• 2000.02a
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• pp.260-261
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• 2000

광결정(photonic crystal)은 빛의 파장 크기 정도의 격자 상수를 지닌 1차원, 2차원, 또는 3차원의 주기적인 구조이다. 광결정에는 광밴드갭(photonic bandgap)이라는 빛의 자발 방출이 억제된 진동수의 영역이 존재하는데, 이 영역을 이용하여 빛의 자발 방출을 조절하고 빛의 흐름을 제어할 수 있다. $^{[1]}$ 지난 10여년간 2차원, 3차원의 광결정 구조에 대한 연구가 많이 이루어져 왔는데, 최근에는 슬랩 도파관(slab waveguide)에 2차원 광결정을 만든 구조에 대한 연구가 활발하게 진행중이다. 이 구조는 평면 방향으로는 광밴드갭 효과로 광모드를 가둘 수 있고 수직 방향으로는 전반사를 이용하여 모드를 가둘 수 있어서 3차원적인 모드 confinement 효과를 얻을 수 있다. [그림 1]의 (a)에 air-bridge 형태의 2차원 광결정 슬랩(photonic crystal slab) 구조를 도식적으로 나타내었고, (b)에는 본 연구실에서 제작한 구조 표면의 scanning electron micrograph을 나타내었다. 현재 몇몇 연구 그룹에서 이와 같은 광결정 슬랩 구조를 이용한 반도체 레이저를 실현하는데 성공하였다.$^{[2,3]}$ (중략)

• 한국연소학회:학술대회논문집
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• 2012.11a
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• pp.29-30
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• 2012

The objectives of this study are to examine the variation of flame chemiluminescence on flame condition and to evaluate the possibility to apply the optical sensor for air/fuel ratio control. Flame chemiluminescence is one of the most important factor to judge the real time flame condition like a air/fuel ratio. In this paper, it is experimentally found that a strong relationship between the air/fuel ratio and optical element output (i.e., photo diode) should be existed. This is verified through the flame spectral analysis for various PD output signal.

• Proceedings of the KSME Conference
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• 2000.11b
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• pp.162-167
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• 2000

Soot formation and oxidation is closely related to the combustion phenomena inside a diesel engine. Laser-based diagnostics provide a means for improving our understanding of diesel combustion, because they have highly temporal and spatial ability. To understand the soot behavior we did preliminary study by taking flame luminosity photographs and 2-D imaging soot distribution using Laser Elastic Scattering(LIS) and Laser-Induced Incandescence(LII). From the data we found that soot concentration was high in the bowl and disappeared from the central region in the late combustion stage.

• 한국연소학회:학술대회논문집
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• 2014.11a
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• pp.227-231
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• 2014