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손민,김도헌,구자예,장홍빈,강문중,Son, Min,Kim, Dohun,Koo, Jaye,Chang, Hongbeen,Kang, Moonjung 항공우주시스템공학회 2014 항공우주시스템공학회지 Vol.8 No.3
An inner flow of a porous cylinder with partial slots was visualized to study fluidic phenomena in a solid rocket motor. A high-pressure chamber and an air supply system for high flow rate were used. In order to visualize the inner flow, the smoke generator with a cam-driven pump and heaters and high speed camera were adopted. The results of the cylinder type and the partial slot type were compared. As a result, the injected smoke flow in the partial slot type had circumferential fluctuations unlike the cylinder type. It was found that the circumferential flow induced from the partial slots could be the cause of combustion instability and roll torque.
저비용 우주 발사체 개발 동향 및 이를 위한 차세대 연료에 대한 고찰
배진현(Jinhyun Bae),구자예(Jaye Koo),윤영빈(Youngbin Yoon) 한국항공우주학회 2017 韓國航空宇宙學會誌 Vol.45 No.10
인공위성의 경량화 및 소형화로 인하여 대형발사체보다는 발사 비용이 저렴한 저비용 발사체에 대한 관심이 증가되고 있다. 저비용 발사체의 비용 절감 중 가장 대표적인 방식이 발사체의 재사용이다. 저비용 발사체를 개발하고 있는 대부분의 기업들 역시 발사체 재사용 방식을 채택하고 있다. 이러한 재사용 목적과 더불어 친환경 우주 발사체에 대한 요구가 증가되면서 저비용 발사체에 사용되는 연료의 선택 역시 매우 중요해졌다. 친환경적이면서 발사체의 재사용이 가능하게 하는 연료 중 에너지 밀도 등 다른 요인을 고려했을 때 가장 적합한 것이 메탄이며, 메탄에 수소를 첨가하여 에너지 밀도를 높게 만든 HCNG(hydrogen-enriched compressed natural gas) 역시 적합하다고 판단되었다. 본 연구는 한국형 발사체 개발 이후 국내 우주 개발 방향 설정의 참고자료로써 전 세계 저비용 발사체 동향 및 로켓 연료의 특성에 대해 고찰하였다. Due to the weight reduction and miniaturization of satellites, there is a growing interest in low-cost launch vehicles, which are cheaper to launch than larger launch vehicles. One of the most cost-effective ways to reduce the cost of launch vehicles is the reuse of vehicles. Most companies that are developing low cost launch vehicles are also adopting a vehicles reuse approach. Along with this reuse purpose, the demand for environmentally friendly space launch vehicles has increased, so the choice of fuel used for low cost launch vehicles has also become very important. Methane and hydrogen-enriched compressed natural gas (HCNG), which makes more energy-efficient by adding hydrogen to methane, are considered to be the most suitable when considering other factors such as energy density among the fuels that are eco-friendly and capable of reusing the launch vehicles. This study investigated the trends of low-cost launch vehicle and rocket fuel in the world as a reference for setting up domestic space development after the development of Korea Space Launch Vehicle-II.
열화상카메라를 이용한 초음파 무화 슬릿제트화염의 연소장 가시화
김민성(Min Sung Kim),구자예(Jaye Koo),김희동(Heuy Dong Kim),김정수(Jeong Soo Kim) 한국추진공학회 2016 한국추진공학회지 Vol.20 No.4
An experimental study was performed for the combustion-field visualization of the burner which burns the liquid hydrocarbon fuel atomized by an ultrasonic oscillator. Configurations of the flame and combustion-field were caught by both high-speed camera and thermo-graphic camera, and those images were analyzed in detail through a post-processing. As a result, the combustion-field grew and reaction-temperature rose due to the strengthening of combustion reaction with the increasing flow-rate of carrier-gas. In addition, a phenomenon of flame flickering was discussed through the comparative analysis of the variational behaviors between the visible flame and IR (Infrared) flame-field.
횡단 공기유동장으로 분사되는 저온 에탄올 제트의 침투거리
이종권 ( Jongkwon Lee ),구자예 ( Jaye Koo ) 한국분무공학회지 2020 한국액체미립화학회지 Vol.25 No.2
The jet in crossflow is a spray method used in the various air-breathing engine. In order to understand the spray characteristics in various environments, many prior studies have been conducted. However, there is a lack of understanding of the low-temperature liquid spray characteristics below 273 K. With this in mind, we tried to enhance the knowledge of the lowtemperature liquid spray characteristics by identifying the penetration height of low-temperature ethanol. The experiment was conducted under phase pressure, and 273 K of air and 293, 263, and 233 K of ethanol was used. Shadowgraphy was employed to measure the liquid penetration, and Otsu’s method was used to analyze the penetration height. The heights tend to decrease as the temperature of the liquid jet decreases. A correlation for the penetration height in the experimental conditions was derived and presented.
이건웅,송우석,황주현,황용석,구자예,Lee, Keonwoong,Song, Wooseok,Hwang, Joohyun,Hwang, Yongseok,Koo, Jaye 한국분무공학회 2019 한국액체미립화학회지 Vol.24 No.2
Shear coaxial injectors were commonly used in rocket engine combustor. They showed good combustion performance. However it is not easy to control the thrust. Pintle injectors were not as popular as the coaxial injectors so far, they have a great advantage over the coaxial injectors. That is, it is relatively easy to control the thrust. Spray characteristics of gel type propellant from movable sleeve pintle injector were investigated. Water with 0.05% of Carbopol 940 was used as gel simulant instead of kerosene gel combined with Thixarol ST for academic purpose. Experiments were performed in various temperature, pressure and pintle opening condition. The results were compared with neat liquid spray. It is also verified that the capabilites of the injector by adjusting the pintle opening.
횡단 유동장으로 펄스 분사된 액체 제트의 분무 구조 및 단면 분포 특성
이인철(Inchul Lee),구자예(Jaye Koo) 한국추진공학회 2009 한국추진공학회지 Vol.13 No.2
Present studies of these experiments was conducted to using water, over a range of cross-flow velocities from 42 to 136 m/s, with injection frequencies from 35.7 to 166.2 Hz. In cross-flow field, main parameters of liquid jet for secondary breakup were cross-flow drag rather than pressure pulse frequency. As oscillation of the periodic pressure, liquid jet was moved up and down. Also, a bulk of liquid jet puff was detected at upper field of liquid surface. Because of pressure pulsation frequency, an inclination of SMD for the structured layer was evanescent. Cross-sectional characteristics of SMD at downstream area were non-structured distributions. The tendency of volume flux value for various frequency of pressure pulse was same distribution. And volume flux was decreased when the frequency of pressure pulse increasing.
SiO<sub>2</sub> 계열 젤화제에 따른 케로신 젤 연료의 유변학적 특성 연구
김재우,전두성,강태곤,장석필,구자예,문희장,Kim, Jaewoo,Jun, Doosung,Kang, Teagon,Jang, Seok Pil,Koo, Jaye,Moon, Heejang 한국추진공학회 2012 한국추진공학회지 Vol.16 No.6
본 연구에서는 $SiO_2$ 계열 젤화제로 알려진 Aerosil(R) R972, Silica 230, Silica 530을 사용하여 케로신 기반 젤 연료를 제작하였다. 케로신 계열 연료로는 Jet A-1을 사용하였으며 젤화(gelification) 여부를 확인하기 위한 전단박화(shear thinning) 현상은 멱법칙(power-law) 모델을 이용하여 검증하였고 제작된 모든 젤 연료는 전단박화 효과와 함께 $SiO_2$ 젤화제의 함유량이 증가할수록 젤의 점도가 높게 형성됨을 확인하였다. 본 연구에서 사용된 젤화제 중 Aerosil(R) R972를 첨가한 젤 연료의 점성계수가 전단률 전 영역에 걸쳐 멱법칙 모델을 따르는 것이 확인되었으며 상대적으로 Silica 230과 Silica 530을 첨가한 젤 연료는 전단률 150 [1/s] 근방 이하에서 멱법칙이 유효하지 않음을 알 수 있었다. 또한, 젤화제 함유량이 증가할수록 vortex 혼합법과 수동 혼합법 간의 유변학적 특성이 크게 차이 나는 것이 관찰되었다. Present work deals three families of $SiO_2$ gelling agents which have been used to produce gel fuel based on Kerosene. Jet A-1 is chosen as fuel where power-law rheological model is used to confirm whether or not the gelification is achieved depending on the %wt of gellant. It was confirmed that the produced jelly-like substance have shear-thinning effect, and that its apparent viscosity increases as $SiO_2$ concentration increases. Compared to other gellants, gel with Aerosil(R) R972 fits most to the power-law model, while gels with Silica 230 and Silica 530 deviate from the power-law model. The rheological characteristics behaved differently depending on the mixing method(vortex mixing and manual mixing) when gellant concentration is increased.
이수지(Suji Lee),구자예(Jaye Koo),윤영빈(Youngbin Yoon) 한국추진공학회 2017 한국추진공학회지 Vol.21 No.4
As the interest in lunar exploration increases, a throttleable engine is regarded as a important technology. Variable area injectors have been identified to be the most reliable throttling method. Pintle injector is a representative injector of the variable method. It has a simple design and inherent combustion stability. Therefore, it is necessary to research the pintle injector. The present study investigates the concept of the injector, the design factors, and the latest development trends for pintle injector design.