• 제목/요약/키워드: 분무속도

검색결과 251건 처리시간 0.02초

저속 충돌제트에 의해 형성되는 액막의 속도 분포에 관한 연구 (A study on the Velocity Distribution of the Liquid Sheet Formed by Two Impinging Jets at Low Velocities)

  • 추연준;강보선
    • 한국분무공학회지
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    • 제5권1호
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    • pp.41-48
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    • 2000
  • In this research, the velocity distribution of the liquid sheet formed by two impinging jets at low velocities are measured using LDV. The spatial distribution of the sheet velocity as well as the effects of impinging anlge and jet velocity on the sheet velocity are examined. The sheet velocity is highest along the sheet axis and it decreases with the increase of the azimuthal angle. With the increase of the impinging angle, the average sheet velocity is decreased due to the increased impact momentum. The average sheet velocity is proportional to the jet velocity but it is always higher than the jet velocity. This result is against the fact that the sheet velocity can be assumed to be equal to the jet velocity in the previous researches.

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충돌분류에 의한 액적의 크기 및 속도특성에 관한 실험적 연구 (An Experimental study on the drop size and velocity characteristic of drop by impinging jets)

  • 한재섭;김선진
    • 한국분무공학회지
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    • 제4권4호
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    • pp.30-37
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    • 1999
  • The breakup characteristics of liquid sheet formed by the liquid rocket injector has a close relation with the combustion efficiency. In this paper, basic characteristics of droplet size and velocity distribution were measured with PDPA for the Like Doublet Impinging Injector. Test variables were the angle of impact, the diameter of orifice and jet velocity. Water was used as test fluid. As a result, for impingement angle less than 90 degree, following correlations were obtained between drop size and design parameters : $D_{32}({\mu}m)=295.0{\times}V^{-0.09}\times(2\theta)^{-0.1}{\times}d^{0.072}$. For impingement angle greater than 100 degree, drop sizes were increased but eventually converged to a certain limiting value.

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미세물분무 작동에 대한 FDS 예측 성능 평가 (Estimation of FDS Prediction Performance on the Operation of Water-Mist)

  • 고권현
    • 한국산학기술학회논문지
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    • 제15권8호
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    • pp.4809-4814
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    • 2014
  • 본 논문은 미세물분무 작동에 따른 화재 거동 및 제압 특성을 예측하는 데 있어서 FDS(Fire Dynamic Simulator)의 예측 성능을 평가하는 것을 목적으로 한다. 미세물분무의 초기액적분포 입력을 위해 Rosin-Rammler /log-normal 분포를 사용하였으며 모델 상수의 영향을 살펴보았다. 또한 미세물분무의 분사압력에 따른 화재 제압특성을 이전의 실험 결과와 비교함으로써 해석 모델을 검증하고 열유동 특성 및 가스 농도 변화를 분석하였다. 결과로부터 동일한 평균입경을 갖는 미세물분무도 액적분포의 특성에 따라 하부 위치에서의 액적 크기 및 속도에 큰 영향을 받고 있음을 확인할 수 있었다. 분무특성에 대한 실험결과와의 비교를 통해 적절한 초기입경분포를 결정하였으며 이를 이용하여 화재 시뮬레이션을 진행하였다. FDS 화재 시뮬레이션 결과는 온도의 변화 및 화재 제압 특성에 대하여 실험 결과와 좋은 일치를 보여주었다. 또한 미세물분무의 작동압력에 따른 열유동장 변화, 가스상 농도 변화의 예측에 있어 유용한 데이터를 제공할 수 있음을 확인하였다.

정전분무법을 이용한 YSZ 박막 제조 (Preparation of Thin YSZ Film by Electrostatic Spray Deposition)

  • 권병완;김진수;박정훈
    • 공업화학
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    • 제19권1호
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    • pp.117-121
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    • 2008
  • 본 연구에서는 정전분무법을 이용하여 YSZ 박막을 제조하였다. 제조된 박막은 제조시 전구체 용액, 지지체 온도 등에 크게 영향을 받았으며, 특히 지지체 온도가 $400^{\circ}C$일 때 치밀한 YSZ 박막을 형성할 수 있었다. 최적조건 하에서 정전분무법을 활용하면 약 $12{\mu}m/h $의 속도로 치밀한 YSZ 박막을 형성할 수 있었다. 제조된 박막은 XRD, FE-SEM, EDX 등을 이용하여 분석하였다.

가솔린 기관용 인젝터의 분무 구조에 관한 실험적 연구 (An Experimental Study on the Spray Structure of a Gasoline Engine Injector)

  • 조병옥;이창식;임경수
    • 한국자동차공학회논문집
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    • 제3권1호
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    • pp.118-130
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    • 1995
  • Fuel spray in a gasoline engine is a significant factor for the decision of engine power, pollutant emission and the design of intake manifold system. Three kinds of fuel which has other physical properties are chosen in this study, and it is observed using an image processing method that the mechanism and structure of free fuel spray with a throttle type gasoline injector, and the detailed characteristics of droplet size and velocity distributions are obtained by macro and micro-scopic measuring method respectively. It is verified that the initial breakup behaviors are depended on We like the result of Reitz's study, and also observed that the spray of octane and solvent with Re of 210~330 and 270~330 respectively are better than ethanol which has relatively high density and viscosity.

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홀로그래피를 이용한 분무 액적의 3차원 속도 측정 (Measurements of Three-Dimensional Droplet Velocities Using the Holographic System)

  • 오대진;추연준;강보선
    • 한국분무공학회지
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    • 제6권4호
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    • pp.31-38
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    • 2001
  • The Holographic Particle Velocimetry system can be a promising optical tool for the measurements of three dimensional particle velocities. In this study, the holographic panicle velocimetry system was used to measure the sizes and velocities of droplets formed by a commercial full cone spray nozzle. Uncertainty analysis was performed to identify the sources of all relevant errors and to evaluate their magnitude. The droplet velocities ranged from 10.3 to 13.3 m/s with average uncertainty of ${\pm}1.6m/s$, which is ${\pm}14%$ of the mean droplet velocity. Compared with relatively small uncertainties of velocity components in the normal direction to the optical axis, the uncertainty of the optical axis component is ${\pm}3.6m/s$. This is due to the long depth of field of droplet images in the optical axis, which is inherent feature of holographic system using forward-scattering object wave of particles.

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PDPA와 고속카메라에 의한 액상부탄 간헐분무 특성 연구 (The Characteristics of a Transient Liquefied Butane Spray using PDPA and High Speed Camera)

  • 윤준규;임종한;김종현
    • Journal of Advanced Marine Engineering and Technology
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    • 제28권3호
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    • pp.466-474
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    • 2004
  • The characteristics of liquefied butane spray are expected to be different from conventional diesel fuel spray, because a flash boiling spray is expected when the surround pressure is below the saturated vapor pressure of the butane(0.23MPa 98K). The axial velocities. radial velocities. and size distributions in butane sprays were measured with PDPA(Phase Doppler Particle Analyzer) system. Sprays were macroscopically observed by using the high speed camera in case that the surround pressure is 0.37MPa and 0.15MPa. respectively. Compared with the conventional spray. the reversed results were investigated when the surround pressure is below the saturated vapor pressure of the butane.

충돌 제트로 형성되는 분무의 속도 특성에 대한 연구 (A Study on the Velocity Characteristics of the Spray Formed by Two Impinging Jets)

  • 추연준;오대진;강보선
    • 한국분무공학회지
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    • 제6권2호
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    • pp.1-8
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    • 2001
  • In this study, the velocity characteristics of liquid elements formed by two impinging jets is analysed using double pulse image capturing technique. For the droplets formed by low speed impinging jets, the droplet velocities are higher with smaller azimuthal and impingement angle. The maximum droplet velocities are about 25 % lower than jet velocity. With an increase of azimuthal angle, the shedding angles increases but remains lower than azimuthal angle. The velocities of ligaments formed by high speed impinging jets gradually decreases with an increase of azimuthal angle. The maximum ligament velocities are about 40% lower than jet velocity. Higher impingement angles produce lower ligament velocities. The shedding angles of ligament almost increases with the same value of azimuthal angle, which implies that the moving direction of ligaments is radial from the origin as the impingement point.

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노즐부근에서의 비정상분무 거동 (Observations on the Near-Nozzle Behavior of an Unsteady Fuel Spray)

  • 구자예;정흥철
    • 한국자동차공학회논문집
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    • 제2권4호
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    • pp.100-111
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    • 1994
  • Observations on the near-nozzle behavior of an unsteady fuel spray through single cylindrical hole nozzle were made by phase Doopler anemometer and microphotographs. At the edge of the spray, droplet velocity peaked during needle opening and closing. Droplet sizes tended to be small on the edge of spray. The near-nozzle spray angle taken from the microphotographs was time-dependent, even though it increased with gas-to-liquid density ratio as expected. The near-nozzle spray angle was the greatest on the initial stage and decreased to a relatively constant value after about one third of the total injection duration regardless of the ambient gas conditions, even in the near-vaccum condition. The wider near-nozzle spray angle in the early stage is due to the flow characteristics inside the nozzle rather than aerodynamic interactions. However, once the spray was established, aerodynamic interactions are essential in the near-nozzle atomization.

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연소실내 연료와 산화제의 분무 연소에 관한 수치적 해석 (Numerical Analysis for Spray Combustion of Fuel and Oxidizer in Combustion Chamber)

  • 성형건;노태성
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제23회 추계학술대회 논문집
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    • pp.255-258
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    • 2004
  • 연소기 설계에 유용한 자료를 제공하기 위해 저속의 질소 가스가 흐르는 연소실내에서 연료와 산화제의 분무 연소에 관한 수치적 해석을 수행하였다. 점화를 위해 고온 질소가 흐르게 하였다. 연료와 산화제의 특성에 의한 연소실내 온도분포와 속도분포를 조사하였다.

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