• 한국추진공학회지
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• 제21권2호
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• pp.41-47
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• 2017

모사추진제로 초저온 액체질소와 기체 질소를 사용하여 핀틀의 개도 및 모사추진제 공급 조건이 초저온 분무에 끼치는 영향을 정성적으로 연구하였다. 액체 공급압력을 고정하고, 핀틀의 개도와 기체 질소의 공급 압력을 변화시켜 실험을 진행하였다. 이미지 가시화는 CCD 카메라를 이용한 Shadowgraph 기법이 사용되었으며, 이미지 후처리를 통해 실험 조건에 따른 분무의 차이를 비교하였다. 액체 질소 단독 분사의 경우 개도가 늘어날 때, 분사속도가 줄어들고 챔버에서의 벤트 압력은 커져 액체질소 시트가 중앙으로 모이는 현상이 관측되었다. 액체질소/기체질소 분무의 경우 이미지 후처리를 통해 서로 실험 조건이 다르지만 Shadowgraph 이미지가 유사하게 나타나는 경우도 분석할 수 있음을 보였다.

• 한국추진공학회지
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• 제24권6호
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• pp.1-9
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• 2020

케로신/액체산소를 추진제로 하는 직사각형 2열 오리피스를 갖는 1.5톤급 액체-액체 핀틀 분사기를 설계 및 제작하여 액체로켓엔진의 실운용 조건인 초임계 상태에서 핀틀 분사기의 연소성능 및 연소 안정성 검증 연소시험을 수행하였다. 연소시험결과 연소실 내부의 고혼합비 재순환 영역에서 생성되는 고온의 연소가스에 핀틀 팁이 손상되었다. 핀틀 팁으로 전달되는 열유속 또는 하중에 대한 냉각 성능을 증가시키기 위해 핀틀 분사기 내부에 인서트 노즐을 설치하였다. 연소시험 결과 인서트 노즐의 설치, AR 및 BF가 핀틀 팁 냉각 성능에 큰 영향을 주는 인자로 확인되었다.

• 한국항공우주학회지
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• 제48권12호
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• pp.1033-1033
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• 2020

• 한국분무공학회지
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• 제20권2호
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• pp.114-120
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• 2015

Effects of injection conditions on a pintle injector which is proper to recent liquid rocket engines requiring low cost, low weight, high efficiency and reusability were studied. The pintle injector with a typical moving pintle was used for atmospheric experiment using water and air. Injection pressures of water were considered 0.5 and 1.0 bar, 0.1 to 1.0 bar for injection pressures of air and 0.2 to 1.0 mm for pintle opening distance. Sauter mean diameters (SMD) of spray was measured at 50 mm distance from a pintle tip and SMD was treated as a representative parameter in this study. As a result, because of shape characteristics of the pintle injector, there was a transient region between the pintle opening distances of 0.6 and 0.7 mm and this region affected to mass flow rates and SMDs. Also, Reynolds numbers for gas, Weber numbers and momentum ratios were adopted as major non-dimensional paramters and the momentum ratio has strong correlation with SMD.

• 한국분무공학회지
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• 제3권2호
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• pp.24-33
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• 1998

The characteristics of liquefied butane spray are expected to be different from conventional diesel fuel spray, because a kind of flash boiling spray is expected when the back pressure is below the saturation vapor pressure of the butane(0.23MPa at $25^{\circ}C$). An accumulator type pintle injector and its fuel delivery system has been simulated in ruder to give injection pressure, needle lift and rate of fuel injected. The governing equation were solved by finite difference metho. The injection duration was controlled by solenoid valve. Spray behaviors such as a transient spray tip penetration, spray angle and SMD were calculated based on the empirical correlations in case that the back pressure is both above the vapor pressure of the butane and below that of butane. When the back preassure is below the vapor pressure of the fuel, conventional correlation is modified to represent the effect of flash boiling.

• 한국분무공학회지
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• 제4권3호
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• pp.15-23
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• 1999

The use of LPG as clean fuel for Diesel engine is very attractive way to reduce soot and NOx emission. In this study, a numerical study has been done to know the transient behavior of LPG fuel in chamber pressures which is held at a pressure above (0.37MPa)and below(0.15MPa)the fuel vapor pressure. Results show that the vortex formed within the start of injection at the leading edge of the spray cone and was most apparent for 0.15MPa chamber pressure case. The high speed photographs and model results showed a narrower cone angle during the quasi-steady spray period at the 0.37MPa chamber pressure compared to the 0.15MPa case. And it can be shown that more realistic vaporization process is necessary to predict the spray length well.