• Journal of Animal Environmental Science
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• v.18 no.sup
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• pp.1-6
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• 2012

This study was conducted to verify the effect of chlorine dioxide ($ClO_2$) on odor reduction at a commercial swine facility consisting of a compost ficility. Compost facility in $NH_3$ concentration was around 550 ppm and less than 78 ppm before and after the $ClO_2$ spraying, respectively, which was over 86% reduction. There was no H2S detection. $NH_3$ concentration was around 420 ppm and less than 35 ppm before and after the $ClO_2$ spraying, respectively, which was over 83% reduction. $H_2S$ concentration was around 210 ppb and less than 32 ppb before and after the $ClO_2$ spraying, respectively, which was over 85% reduction. Hence, $ClO_2$ spraying at windowless barns was compost facility decreased malodor such as $NH_3$.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.04a
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• pp.28-28
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• 2000

가스터빈 연소기의 역방향 이중 스월러의 두 번째 벤츄리 끝단 각도의 변이가 연소실내의 유동 특성에 미치는 영향에 대해 알아보았다. 벤츄리 끝단 각도가 수렴형, 직선형, 발산형의 세 형상에 대해 연료 분무가 없는 경우, 연료 분무는 있으나 연소는 없는 경우, 연소가 일어나는 경우에 대해 수치적 방법으로 연소실 내의 유동 특성에 대해 고찰하였다. 연료의 분무는 분무된 액적들이 갖는 운동량이 유입되는 공기의 운동량에 비해 적으므로 분무에 의한 유동 특성의 변화는 무시할 수 있는 반면 연소가 일어날 때는 유동 특성이 판이하게 달라짐을 확인할 수 있었다. 가스터빈 연소실 내의 유동 특성은 벤츄리 끝단 각의 변이에 따라 민감하게 변하고 있다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.892-895
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• 2017

As a component development of heavy duty industrial gas turbine combustor development program, pressure swirl simplex injector was designed and tested to figure out spray characteristics and performance. Injector flow rate as a function of pressure drop was measured and compared to the design target. Also spray shape was analyzed qualitatively and spray cone angle was measured from spray visualization image using shadowgraph. The flow test result showed that the injector was designed and manufactured correctly according to the design target and spray cone angle was measured from shadowgraph result. As a next step, PDA (Phase Doppler Anemometry) measurement is planned to figure out more specific spray performance and characterization.

• Proceedings of the Materials Research Society of Korea Conference
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• 2008.05a
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• pp.10.2-10.2
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• 2008

• Journal of Power System Engineering
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• v.15 no.3
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• pp.5-11
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• 2011

디젤기관의 경우는 종래부터 직분식이 주류를 이루었고, 근래에는 분사압력의 고압화가 진행중이다. 분사압력의 고압화에 의해 연소효율의 향상 및 배출가스중의 입자상물질(PM:Particulate Matter)의 저감을 유도하고 있으나, 연소가스의 고온화로 인해 질소산화물(NOx:Nitrogen Oxides)은 증가한다. 따라서, 분사기간의 지연(Retard)이나 파일럿분사(Pilot injection)등의 혼합기제어에 의해 질소산화물의 저감을 꾀하고 있다. 이와 같이 디젤기관에 있어서도 혼합기 형성의 최적화에 의한 연소제어를 시도하는 수법이 중시되고 있고, 이를 위해서는 디젤분무 구조에 기초한 혼합기의 형성기구에 대한 규명이 매우 중요하다. 그러므로 본 연구에서는 보다 고도의 혼합기형성 제어를 위한 기초연구로서 고온 고압장에서의 증발디젤자유분무구조를 해석하였으며, 계측영역은 연료와 주위기체와의 혼합이 활발히 진행되는 분무의 하류영역으로 설정하고, 입자화상속도측정법(particle Image Velocimetry:PIV)을 이용한 분무의 유동해석을 기초로 증발 디젤분무의 구조 해석을 행하였다. 실험조건으로서 분사압력을 72MPa, 112MPa로 각각 변화시켰다.

• Transactions of Materials Processing
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• v.14 no.7 s.79
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• pp.587-594
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• 2005

분무성형공정은 급냉응고 및 결정입자 제어에 따른 고품위 소재 개발의 장점과 함께 고밀도 near-net-shape 제품의 제조가 가능한 합금제조기술이다 분무성형체의 미세조직은 적층표면에 도달하는 액적들의 평균 열용량, 즉 고상분율에 의하여 결정되며, 이는 액적의 비행과정에서의 분사가스-액적간의 열전달과 적층표면에서의 열유입과 열유출 속도에 영향을 받는다. 실제 다양한 공정변수들이 복합적으로 미세조직 형성과정에 영향을 미치지만, 균일한 미세조직을 얻기 위하여서는 적층표면에서의 온도와 고상분율을 항상 일정하게 제어하여야만 한다 즉, 적층표면 온도를 분무 성형공정중에 지속적으로 측정하여 이를 공정 제어 시스템에 feedback하여 원하는 적층표면온도를 유지하도록 공정변수를 제어하는 것이 필수적이다. 분무성형에 제조된 성형체는 합금원소의 편석이 없고 미세한 등방성의 결정립으로 이루어진 특징적인 미세조직을 나타낸다 이와 같은 미세조직으로 인하여 분무성형체는 우수한 성형성과 기계가공성을 나타내며, 또한 분무성형-후속가공된 최종 제품은 잉곳주조에 의하여 제조된 것과 비교하여 크게 향상된 기계적 성질을 가진다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.11a
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• pp.381-386
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• 2007

Jet-A spray, evaporation and combustion were numerically analyzed in annular type model combustor using KIVA-3V. Liquid fuel's atomizing was affected by flow field near droplet. When cooling flow was not optimized, SMD was increased, and equivalence ratio was horizontally distributed in combustor's downstream. Flame spread out horizontally and separated in combustors downstream. Flame center was separated by cooling flow. Flame separation made local high temperature in downstream that caused NO increase.

• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.1
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• pp.61-67
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• 2015

The cooling of hot exhaust gas is an important issue for the construction of combustor test facility. Water spray is an effective method for exhaust gas cooling due to its large latent heat in process of evaporation. In this study, 1-D analysis has been performed based on continuity, energy conservation, and saturated vapor property to understand water spray cooling of combustion gas. In the exhaust duct of combustor test facility, the injected water decreases combustion gas temperature, and evaporates in the combustion gas. However, some of the injected water is collected in the sump due to condensation. The evaporation of water helps combustion gas cooling, but causes pressure increase inside the exhaust duct due to increase of vapor pressure. These phenomena has been analyzed by 1-D modeling in this study. From 1-D analysis, the adequate mass flow rate of water spray to cool combustion gas and to avoid excessive pressure rise inside the exhaust duct has been decided.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.285-288
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• 2009

In order to understand spray characteristics with inflowing air from the compressor in the APU gas turbine combustor, we performed spray visualization test by using ND-Yag Laser sheet beam. The sector combustor which size is 1/6 of the real combustor was manufactured. Turbo blower is used as an air supplying device to simulate gas turbine air flow condition. In the case of 75 m/s combustor inlet air flow condition, spray angle way increased and dispersed widely than without airflow condition.

• Journal of ILASS-Korea
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• v.17 no.2
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• pp.77-85
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• 2012

The CFD simulation of diesel spray tip penetrations were compared with 0-D simulation for experimental data obtained with common rail injection system. The simulated four injection patterns include single, pilot and split injections. The CFD simulation of the spray penetration over these injection patterns was performed using the KIVA-3V code, which was implemented with both the standard KIVA spray and original gas jet sub-models. 0-D simulation of the spray tip penetration with time-varying injection profiles was formulated based on the effective injection velocity concept as an extension of steady gas jet theory. Both the CFD simulation of the spray tip penetration with the standard KIVA spray model and 0-D simulation matched better with the experimental data than the results of the gas jet model for the entire fuel injection patterns.