• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제25회 추계학술대회논문집
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• pp.34-39
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• 2005

본 논문에서는 3차원 초음속 노즐 형상 변수에 따른 부분입사형 터빈의 유동 및 성능 특성을 알아보기 위하여 3차원 노즐 형상 변수를 노즐 모양 및 노즐 출구 단면 형상으로 설정하여 전산해석을 실시하였다. 먼저 노즐 모양에 따른 유동 및 성능 특성을 비교해 본 결과, 사각형 노즐이 원형 노즐보다 축방향 간극내에서 발생하는 전압력 손실이 적었으며, 이로 인하여 파워가 약 1.5% 증가하였다. 다음으로 사각형 노즐출구단면의 면적에 따른 유동 및 성능 특성을 비교해 본 결과, 노즐 출구 단면과 로터의 hub/tip 사이의 간극과 노즐간의 간격이 터빈 성능에 크게 영향을 줌을 확인할 수 있었다.

• Journal of Mechanical Science and Technology
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• 제17권4호
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• pp.617-625
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• 2003

Effects of Injector nozzle geometry and operating pressure conditions such as opening pressure, ambient pressure. and injection pressure on the transient fuel spray behavior have been examined by experiments. In order to clarify the effect of internal flow inside nozzle on the external spray, flow details Inside model nozzle and real nozzle were alto investigated both experimentally and numerically. for the effect of injection pressures, droplet sizes and velocities were obtained at maximum line pressure of 21 MPa and 105 MPa. Droplet sizes produced from the round inlet nozzle were larger than those from the sharp inlet nozzle and the spray angle of the round inlet nozzle was narrower than that from the sharp inlet nozzle. With the increase of opening pressure, spray tip penetration and spray angle were increased at both lower ambient pressure and higher ambient pressure. The velocity and size profiles maintained similarity despite of the substantial change in injection pressure, however, the increased injection pressure produced a higher percentage of droplet that are likely to breakup.

• 한국분무공학회지
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• 제12권4호
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• pp.204-210
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• 2007

The worldwide energy problem and global warming cause the need of alternative fuels which feature low carbon-dioxide emission and another energy source. Liquefied Petroleum Gas (LPG) is one of the alternative fuels widely used as domestic and transportational fuel. The third generation LPLi fuel supply system has merits in the increase of engine power and low emissions. The injectors used in LPLi system should overcome a leakage problem and satisfy the durability conditions. Therefore, 1000 hour durability test of the injectors was carried out throughout this research. First, the spray pattern and the penetration length of the selected injectors is graphically shown. Next, the leakage amount with respect to the injection cycle is introduced. Finally, the shapes of nozzle holder and nozzle tip after durability test was investigated by analyzing the microscopic image of the injector tip. The variation in the shape of nozzle tip mainly due to the residue of rubber materials is found to be the reason for leakage.

• International Journal of Automotive Technology
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• 제4권3호
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• pp.119-124
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• 2003

Dimethyl Ether (DME) is an excellent alternative fuel that provides lower particulate matter (PM) than diesel fuel under the same engine operating conditions. Spray characteristical of DME in common rail injection system were investigated within a constant volume chamber by using the particle motion analysis system. The injector used in this study has a single hole with the different orifice diameter of 0.2, 0.3 and 0.4 mm. The injection pressure was fixed at 35MPa and the ambient pressure was varied from 0.6 to 1.5 MPa. Spray characteristics such as spray angle, spray tip penetration and SMD (Sauter mean diameter) were measured. Spray angle was measured at 30d$_{0}$, downstream of the nozzle tip. The measured spray angie increased with increase in the ambient pressure. Increase of the ambient pressure results in a decrease of spray penetration. The experimental result, of spray penetration were compared with the predicted one by theoretical and empirical models. Increase in the ambient pressure and nozzle diameter results in an increase of SMD at a distance 30, 45 and 60d$_{0}$, downstream of the nozzle, respectively.ely.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.662-665
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• 2011

고체 추진기관의 추력 조절의 한 방법인 핀틀 노즐 기술은 초음속 유동장 내부에 핀틀을 위치시키고 핀틀의 위치를 조절하여 노즐 목 면적을 조절함으로써 추력의 크기를 조절한다. 본 연구는 Needle형 핀틀이 초음속 유동장 내부에서 구동될 때 발생하는 핀틀 팁에서의 압력변화와 핀틀노즐의 비정상 유동특성에 대해 분석하였다. 연구 결과 초음속 유동장 내부에서 핀틀이 움직일 때 핀틀팁에서의 압력변화가 발생하고, 이러한 압력변화에 따라 추력변화가 야기됨을 비정상상태 해석으로 확인하였다.

• 한국음향학회지
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• 제37권2호
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• pp.83-91
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• 2018

팁젯 로터의 소음원은 로터 블레이드 소음과 제트 소음으로 분리할 수 있다. 로터 블레이드 소음은 두께 소음, 하중 소음, 비선형 사중극 소음으로 구성되고 제트 소음은 노즐 모멘텀 소음과 제트 방사 소음으로 나뉜다. 로터 블레이드 소음을 해석하기 위해 유동 해석 정보를 전산유체역학(Computational Fluid Dynamics, CFD) 해석으로 얻은 뒤 투과면, 비투과면 FW-H(Ffowcs Williams-Hawkings) 음향 상사법을 동시에 적용하여 각 소음원을 구분하였다. 그리고 제트 소음은 노즐 출구 조건을 활용하여 투과면 FW-H 음향 상사법으로 노즐 모멘텀 소음을 구하고 기존 고정익 제트에 대한 경험식을 활용하여 제트 방사 소음을 얻었다. 검증 기체의 소음 측정값을 기준으로 해석 기법의 신뢰성을 검증하였고 스펙트럼 분석을 통해 팁젯 로터의 독특한 소음 특성을 확인하였다.

• 한국분무공학회지
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• 제4권2호
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• pp.40-46
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• 1999

Experimental investigation of unsteady impinging diesel spray on the flat plate have been carried out using high speed camera and Malvern system. The density ratios of ambient gas to diesel fuel were varied using $N_2$ and Ar gas in the case of 14.9, 21.2, 28.4, 35.1, 40.4, and 50.1. With the increase of gas density ratio, the radial penetration is decreased due to the resistance of the ambient gas. With the increase of the gas density ratio and the distance between nozzle tip and flat plate, the height of spray is increased due to the entrance and circulation. With the increase of gas density ratio, SMD is decreased on the nearby position at the center of flat plate, but SMD is increased on the far position. As the distance between nozzle tip and flat plate is increased, SMD is always decreased.

• 연구논문집
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• 통권25호
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• pp.55-65
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• 1995

Three-dimensional incompressible turbulent flow fields within the passage of the steam turbine nozzle with/without tip clearance have been simulated by solving the Navier-Stokes equations with SIMPLE scheme. The extended k-e model is applied to modeling the Reynolds stresses. Grids in the computational domain are generated by solving the Poisson's equations to improve the smoothness and orthogonality. Flow losses, secondary flow, velocity profiles, and deviation angles are obtained. The computated results without tip clearance show good agreement with the experimental data.

• 한국자동차공학회논문집
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• 제12권6호
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• pp.60-65
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• 2004

Numerical simulations and experiments have been carried out to investigate the effect of fuel injection nozzles on the combustion and NOx formation processes in a medium-speed marine diesel engine. Spray visualization experiment was performed in the constant-volume high-pressure chamber to verify the numerical results on the spray characteristics such as spray angle and spray tip penetration. Time-resolved spray behaviors were captured by high-speed digital camera and analyzed to extract the information on the spray parameters. Spray and combustion phenomena were examined numerically using FIRE code. Wave breakup and Zeldovich models were adopted to describe the atomization characteristics and NOx formation processes. Numerical results were verified with experimental data such as cylinder pressure, heat release rate and NOx emission. Finally, the effects of fuel injection nozzles on the engine performance were investigated numerically to find the optimum nozzle parameters such as fuel injection angle, nozzle hole diameter and number of nozzle holes. From this study, the optimum fuel injection nozzle (nozzle hole diameter, 0.32 mm, number of nozzle holes, 8 and fuel injection angle, $148^{\circ}$) was selected to reduce both the fuel consumption and NOx emission. The reason for this selection could be explained from the highest fuel-air mixing in the early phase of injection due to the longest spray tip penetration and the highest heat release rate after $19^{\circ}$ ATDC due to the increased injection duration.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2010년도 춘계학술대회 초록집
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• pp.58.2-58.2
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• 2010

This paper deals with the simulation of solid particle coating technology via supersonic nozzle in vacuum environment to devote as an aerosol-deposition device. In order to improve efficiencies of nozzle and coating process, effects of shockwave, nozzle geometry, and substrate location were studied computationally under a fixed chamber pressure of 0.01316 bar which is nearly vacuous. Shockwave is the important factor affect to entire flow because shockwave in the jet flow dissipates the kinetic energy of the flow in the supersonic condition. Results show that various nozzle geometries have significant effect on the supersonic flow and we know that the supersonic nozzle should be optimized to minimize the loss of the flow. Another parameter, the distance between substrate and nozzle tip, shows little effect in this study.