• 제목/요약/키워드: Shadowgraph

검색결과 105건 처리시간 0.028초

축소형 액체로켓엔진에서 기체산소/케로신 및 기체아산화질소/에탄올 연소 분무의 비교 (Comparison between GOx/Kerosene and GN2O/Ethanol Reactive Spray in a Subscale Liquid Rocket Engine)

  • 최송이;신봉철;이건웅;김도헌;구자예;박동근
    • 한국추진공학회지
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    • 제19권4호
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    • pp.61-68
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    • 2015
  • 초임계 연소에 대한 기초연구로써 축소형 액체 로켓 엔진에서 기체산소/케로신, 기체아산화질소/에탄올 추진제 조합의 정상상태 연소의 분무를 관찰하고 비교하였다. 분무의 가시화에는 shadowgraph 기법을 사용하였으며 실험결과를 분석하기 위해 shadowgraph를 후처리하여 밀도구배강도 이미지를 사용하였다. 정상상태 연소압력이 동일한 조건에서 기체산소/케로신 추진제의 액체 제트 표면의 굴곡이 심하고 분사기 팁 근처에서 급격한 밀도구배를 보이는 것이 관찰되었다. 밀도구배강도의 평균 이미지에서 분무 중심 길이를 도출하였으며 더 낮은 운동량 플럭스 비 조건에서도 기체산소/케로신의 분무중심 길이가 더 짧은 것으로 나타났다.

고압조건에서 n-Butanol 예혼합화염의 화염속도 (Flame Speeds of Premixed n-Butanol Flames at High Pressures)

  • 이기용;박기덕
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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    • pp.87-89
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    • 2014
  • Spherically expanding flames are used to measure flame speeds, which are derived the corresponding laminar flame speeds at zero stretch. Flame speeds of n-butanol at high pressure are studied over an extensive range of equivalence ratios. The classical shadowgraph technique is used to detect the reaction zone. In analytical methodology the optimization process using least mean squares is performed to extract the laminar flame speeds. Laminar flame speeds are compared with results obtained from numerical work.

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고압에서 DME-Air 혼합기의 화염속도 측정 (Measurement of Laminar Flame Speeds of Dimethyl Ether-Air Mixtures at High Pressure)

  • 이수각;이기용
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2013년도 제46회 KOSCO SYMPOSIUM 초록집
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    • pp.103-105
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    • 2013
  • Spherically expanding flames are used to measure flame speeds, which are derived the corresponding laminar flame speeds at zero stretch. Dimethyl Ether-Air mixtures at high pressure are studied over an extensive range of equivalence ratios. The classical shadowgraph technique is used to detect the reaction zone. In analytical methodology the optimization process using least mean squares is performed to extract the laminar flame speeds. Laminar flame speeds are compared with results reported in the literature.

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초저온 질소 분사 핀틀 인젝터 분무의 가시화 (Visualization of Cryogenic Nitrogen Spray from a Pintle Injector)

  • 이건웅;손민;신동수;윤영빈;김정수;구자예
    • 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.

Visualization of Diesel and GTL Spray Combustion and Soot Formation in a Rapid Charging Combustion Vessel with Shadowgraph Method

  • Kim, Ki-Seong;Azimov, Ulugbek;Lee, Yong-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • 제32권7호
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    • pp.1019-1029
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    • 2008
  • In this study, visual investigation of sprays and flames has been performed and soot formation in Diesel and GTL fuels has been compared in a specially designed Rapid Charging Combustion Vessel (RCCV) under various ambient gas $O_2$ concentrations and two injection pressures. It has been concluded that soot in the mixing-controlled combustion of Diesel and GTL fuels has similar tendency to be formed in the leading portion of the jet boundaries. Auto-ignition delay for GTL fuel is shorter than that for diesel fuel. The temporal and special variation of soot concentration in the diesel flame jets at various $O_2$ concentrations was correlated with the heat release rate. Soot concentration appears in the regions when diffusion combustion starts, and its concentration reaches maximum at the peak of heat release curve and then decreases due to oxidation. Visualization by shadowgraph method showed that soot decreases with lower $O_2$ concentration, and higher injection pressure.

마랑고니 대류에 미치는 불응축성가스의 영향 (Noncondensable Gas Effects on the Marangoni Convection)

  • 이동호
    • 설비공학논문집
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    • 제8권4호
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    • pp.510-518
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    • 1996
  • The study presents experimental and theoretical analysis focusing on the infulence of a noncondensable gas upon the absorption enhancement that is obtained by Marangoni convection generated by the addition of the surfactant. The shadowgraph method is adopted in this visualization. As a result of absorption phenomena with shadowgraph photos, the different patterns of Marangoni convection cells are observed in accordance with the various amounts of noncondensable gas. Furthermore, non dimensional number K(Ma/Ra) is introduced to calculate the value of surface tension difference theoretically for the comparison with the various amount of non condensable gas in absorber.

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직접분사식 수소연료의 분무 및 연소특성에 관한 연구 (A Study on the Characteristics of Injection and Combustion with Directly Injected Hydrogen Fuel)

  • 이성욱;기완수
    • 한국자동차공학회논문집
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    • 제15권5호
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    • pp.24-29
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    • 2007
  • This study aims to provide a fundamental data for directly injected hydrogen fuel engines. Spray, ignition and combustion characteristics of hydrogen were studied using constant volume chamber. For spray visualization, hydrogen was vertically injected into a combustion chamber at various condition, for example, injection pressure, ambient pressure. And an argon laser was used for the shadowgraph photography by applying optical method. Also, to investigate heat-release rate and flame propagations, spark was ignited on hydrogen injected at the different time after injection and the duration of injection was also changed. Processes of ignition and combustion were analyzed by heat-release rate calculated by pressure history and were observed by shadowgraph photography The results gave much knowledge of spray, ignition and combustion characteristics of hydrogen.

초임계 환경으로 분사되는 극저온 제트의 분열 (Disintegration of Cryogenic Jet in Super-critical Environment)

  • 이건웅;김도헌;구자예
    • 한국분무공학회지
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    • 제18권3호
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    • pp.140-145
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    • 2013
  • Sub/supercritical spray experiments were conducted, and cryogenic nitrogen and gaseous argon were selected for simulants. liquid nitrogen and gaseous argon were injected in subcritical case, and supercritical nitrogen and near-critical gaseous argon were injected in near-critical/supercritical cases. shadowgraph method was used to visualize spray, and analyzed about the breakup length. The breakup length was measured from numbers of Instantaneous shadowgraph Images from each case, and they were compared with momentum flux ratios and density ratios. It was observed that the relation between breakup length and momentum flux ratio was fitted into former experiment results. and the reasonable constant was suggested about the relation between breakup length and density ratio.

가솔린 직분식 압축착화 엔진 저부하 영역 디젤/가솔린 분무의 쉴리렌, 쉐도우그래프, 미산란법적 가시화 (Schlieren, Shadowgraph, Mie-scattering Visualization of Diesel and Gasoline Sprays under GDCI Engine Low Load Condition)

  • 박성산;김동훈;배충식
    • 한국분무공학회지
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    • 제20권3호
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    • pp.187-194
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    • 2015
  • In this study, three visualization methods, Schlieren, Shadowgraph, and Mie-scattering, were applied to compare diesel and gasoline spray structures. Fuels were injected into a high pressure/high temperature constant volume chamber under the same ambient pressure and temperature condition of low load in gasoline direct injection compression ignition (GDCI) engine. Two injection pressures (40 and 80 MPa), two ambient pressures (4.2 and 1.7 MPa), and two ambient temperatures (908 and 677 K) were use. The images from the different methods were overlapped to show liquid and vapor phases more clearly. It was found that the gasoline fuel is more appropriate to form a lean mixture.

Shear Layer and Wave Structure Over Partially Spanning Cavities

  • Das, Rajarshi;Kim, Heuy Dong;Kurian, Job
    • 한국가시화정보학회지
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    • 제11권2호
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    • pp.46-54
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    • 2013
  • Study of the wave structure and shear layer in the vicinity of a wall mounted cavity is done by time averaged colour schlieren and time resolved instantaneous shadowgraph technique in an M=1.7 flowfield. Effect of change of cavity width on flow structure is investigated by using constant length to depth (L/D) ratio cavity models with varying length to width (L/W) ratio of 0.83 to 4. The time averaged shock wave structure was observed to change with change in cavity width. Dependence of the shock angle at the leading edge on the shear layer width is also evident from the images obtained. Unsteadiness in the flow field in terms of shear layer dynamics and quasi steady nature of shock waves was evident from the images obtained during instantaneous shadowgraph experiments. Apart from the leading and trailing edge shocks, several other waves and flow features were observed. These flow features and the associated physical phenomena are discussed in details and presented in the paper.