• Journal of the Korean Society of Propulsion Engineers
• /
• v.12 no.1
• /
• pp.16-22
• /
• 2008

The effect of two-phase spray injected into subsonic cross-flow was studied experimentally. External-mixing of two-phase spray from orifice nozzle with L/d of 3 was tested with various air-liquid ratio that ranges from 0 to 59.4%. Trajectory of spray and breakup phenomena were investigated by shadowgraph photography. Detailed spray structure was characterized in terms of SMD, droplet velocity, and volume flux using PDPA. Experimental results indicate that penetration length was increased and collision point of liquid jets approached to nozzle exit and distributions of mist-like spray were obtained by increasing air-liquid ratio.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.8 no.4
• /
• pp.91-101
• /
• 2004

With the mathematic linear model of a combustor which consists of a combustion chamber and injectors, the analysis of low frequency dynamic characteristics of a liquld-propellant rocket engine combustor was performed. Propellant mass flowrate was varied by combustion chamber pressure feedback, therefore low frequency oscillation was appeared. Increasing the time constant of a combustion chamber and injector pressure differences and decreasing combustion time delay increased the combustor system stability. The variation of injector time constant little affected stability. The system was always stable, when there was no combustion time delay. Increasing combustion time delay decreased oscillation frequency and damping ratio, and the system eventually became unstable.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.11 no.5
• /
• pp.31-36
• /
• 2007

Combustion performance characteristics of subscale high-pressure combustor were investigated at 70 bar combustion pressure. All tests were successfully performed without any damage on the combustor. The mixing characteristics and distribution pattern of the injectors were found to have considerable influence on the combustion performance. The characteristic velocity of the combustor was higher in the injector with internal mixing than that of external mixing and in the injector with smaller mass flowrate. The pressure fluctuations at the propellant manifolds and the combustion chamber were measured to be less than 3% of the mean combustion pressure to meet the combustion stability criterion and to prove stable combustion characteristics of the combustor.

• Journal of Navigation and Port Research
• /
• v.34 no.1
• /
• pp.71-75
• /
• 2010

This study is experimented to observe an influence of experimental conditions on production characteristics of slurry ice by injection operating water to cooling plate. And at this experiment it used ethylene glycol-water solution and the concentration is 10 to 20wt%. The experimental apparatus was constructed of ethylene glycol-water solution and slurry ice storage tank, brine tank, pumps for ethylene glycol-water solution and brine circulating, a mass flow-meter, data logger for fluid temperature measuring and a vertical circular tube with single copper plate as test section. The experiments were carried out under various conditions, with mean velocity of fluid at the entry ranging from 1.0 to 2.0m/s and the cooling temperature of $-17^{\circ}C$ to $-10^{\circ}C$.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.24 no.4
• /
• pp.12-24
• /
• 2020

The dual-throat nozzle is an extremely effective method in the thrust vectoring control field, utilizing another convergent section to connect with the divergent part of the conventional convergent-divergent nozzle. In the present research, the numerical simulation is conducted to investigate the effects of the injection angle on thrust vectoring performance in a 3D supersonic nozzle. Five injection angles are discussed and core performance variations are analyzed, including the deflection angle, injected mass flow ratio, system resultant thrust ratio, efficiency, Mach number contour and streamline on the symmetry plane, and Mach number contours at different slices. Meaningful conclusions are offered for fighter jet designers.

• Proceedings of the KAIS Fall Conference
• /
• 2009.12a
• /
• pp.526-530
• /
• 2009

본 연구은 자동차용 가솔린엔진에 장착되는 인젝터의 연료공급 특성에 대한 것으로, 가솔린 엔진의 전자제어식 포트 연료분사는 분무장치와 흡기포트의 최적화 및 분무특성이 우수해야 엔진의 성능 향상 및 배기가스 저감의 목적을 이룰 수 있다. 4홀과 12홀 인젝터의 장착각 변화와 포트 마스킹의 형상변화에 따른 벽유량을 측정?분석하였고 분무가시화 실험을 통하여 분무성장과정과 분사각, 연료미립화 및 분무도달거리를 분석하였다. 벽류측정 실험을 통하여 벽류는 미립화정도와 흡기유동과 유속에 가장 큰 영향을 받는 것으로 판단되며, 12홀 인젝터 대비 4홀 인젝터는 분무압력에 따라 분무특성의 변화량이 크게 나타났다.

• Proceedings of the Materials Research Society of Korea Conference
• /
• 2011.05a
• /
• pp.21.2-21.2
• /
• 2011

에어로졸 데포지션(Aerosol deposition) 기술은 상온에서 초음속 유동을 통해 분사된 미세 입자가 기판에 충돌하면서 강력한 결합을 형성하는 방식으로 코팅이 이루어진다. 이 방법은 별도의 소결과정 없이 상온에서도 조밀하고 균일한 박막을 형성할 수 있다. 또한 세라믹, 금속 재질의 다양한 입자를 사용할 수 있을 뿐만 아니라 금속, 유리 기판등에 적용이 가능하다. 본 논문은 이러한 에어로졸 데포지션 기술을 이용하여 광촉매 효과가 뛰어난 $TiO_2$ 입자를 대면적 코팅에 적용가능한 초음속 노즐을 통해 분사하여 ITO기판 위에 박막을 형성하였다. $TiO_2$ 입자의 크기, 기판의 이송 속도와 왕복횟수, 공급 유량 등이 코팅면의 특성과 조성 등에 미치는 영향을 분석하였다. $TiO_2$ 박막층의 형상과 두께는 주사전자현미경(SEM)을 통해 확인하였고, X-ray diffraction (XRD)를 이용하여 코팅 입자와 박막 층의 조성을 각각 확인하였다. 에어로졸 데포지션을 이용한 $TiO_2$ 코팅층은 염료감응형 태양전지(DSSC), 자정작용(self-cleaning), 살균작용(antibacterial effect) 등의 적용분야에 적용 가능할 것으로 판단된다.

• Proceedings of the KSME Conference
• /
• 2000.11b
• /
• pp.726-731
• /
• 2000

This study was experimentally analyzed to improve the performance and to reduce exhaust emissions in a turbochaged D.I. diesel engine of the displacement 9.4L. In generally, the system of intake port, fuel injection and turbocharger are very important factors which have influence on the engine performance and exhaust emission because the properties in the injected fuel depend on the combustion characteristics. The optimum results which is tested as available factors fur better performance and emission are as follows; the swirl ratio is 2.43, compression ratio is 16, combustion bowl is $5^{\circ}$ re-entrant type, nozzle hole diameter is ${\phi}0.28*6$, injection timing is BTDC $13^{\circ}CA$ and turbocharger is GT40 model which are selected compressor A/R 0.58 and turbine A/R 1.19.

• Transactions of the Korean Society of Automotive Engineers
• /
• v.9 no.6
• /
• pp.76-84
• /
• 2001

Generally fuel injection system using solenoid have some problems between control signal and mechanical movement like as time lag. Main purpose of the present study is to help the design optimization of GDSI for real engine application. We have adopted two different solenoid driving circuit, namely saturation and pick-hold type and have investigated experimentally the current, needle force, needle opening duration and injection quantity. The pick-hold type driving circuit surpassed a saturation type in the response time and pression control of injection quantity. Accordingly, Using characterization data of operating factors such as time constant, driving force and so on, can be evaluated and adjusted to obtain an optimum injector performance.

• Transactions of the Korean Society of Automotive Engineers
• /
• v.17 no.3
• /
• pp.117-126
• /
• 2009

A Common-Rail Direct Injection(CRDI) system for high speed diesel engines was developed to meet reductions of noise and vibration, and emission regulations. In this study, CRDI system analysis model which includes fuel and mechanical sub-systems was developed using commercial software, AMESim in order to predict characteristics for various fuel injection components. Each component which constructs system was modeled and verified by sub-model of AMESim obtained characteristics curves of each components. The parameter sensitivity analysis such as throttle size, injection rate, plunger displacement, supply pressure of fuel injection for system design were carried out by the analysis.