• Title/Summary/Keyword: 평균액적지름

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The Effects of Barley Tea Concentration and Atomizing Pressure on the Atomization with Two Fluid Nozzle Spray Gun (이류식(二流式) 노즐에서 보리차 추출액(抽出液)의 농도(濃度) 및 분무(噴霧) 압력(壓力)이 분무화(噴霧化)에 미치는 영향(影響))

  • Lee, Jeong-Cheol;Chun, Jae-Kun
    • Korean Journal of Food Science and Technology
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    • v.15 no.4
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    • pp.342-347
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    • 1983
  • The effects of barley tea concentration and atomizing air pressure on the size, homogeneity and distribution of the sprayed droplets were investigated. An equation relating mean diameter (${\overline{D}}$) with the concentration where the coefficient a and b were determined empirically. As the operating air pressure was increased, the mean diameter of the droplets decreased and finally reached the limiting mean diameter, $36{\mu}m$ at 15.7% barley tea concentration. The homogeneity of the droplets increased with the operating air pressure, increase and it was decreased steadily as the soluble solid concentration increased up to 20% and markedly over 20% at every operating air pressure. The distribution ($P_D$) of sprayed droplets related with the droplet size as the following exponential equation; $P_D$ = e 1nD + f where e and f are empirical constants.

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An Experimental Study on Droplet Size Characteristics of Liquid Jets in Subsonic Crossflow (수직분사제트에서 액적크기특성에 대한 실험적 연구)

  • Kim, Min-Ki;Song, Jin-Kwan;Kim, Jin-Ki;Yoon, Young-Bin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.59-63
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    • 2006
  • A direct photograph measurement technique was used to determine the spatial distribution of the spray droplet diameter in subsonic crossflow and it also obtain that SMD distribution by using PLLIF technique. The injector internal flow was classified as three modes such as a normal, cavitation, and hydraulic flip. The objectives of this research are getting a droplet distribution and drop size measurement of normal flow and compare with the other flow effects. Although the study showed visually that drop size were spatially dependent of Air-stream velocity, fuel injection velocity, and normalized distance from the injector exit length.(x/d, y/d) There are also difference characteristics between cavitation, hydraulic flip and the normal flow.

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Effect of Backhole on Spray Characteristics of Swirl Injectors in Liquid Propellants Rocket Engine (액체 추진제용 로켓 엔진 스월 인젝터의 백홀로 인한 분무 특성 연구)

  • 황성하;윤영빈
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.2
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    • pp.23-35
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    • 2003
  • "Backhole" is a new geometric parameter and is defined as an extra empty volume which is located behind the tangential entries at the rear part of the vortex chamber in the swirl injector. Backhole makes a difference to the spray characteristics of swirl injectors such as the spray angle, SMD, the mixing characteristics and so on. To find its characteristics, experiments are conducted by using a stroboscopic photography, a PDPA apparatus and a mechanical patternator. With the backhole, the mass flow rate of the swirl injector is increased and the center region of the injected flow has more large volume than that of without the backhole. Also the cone angle can be controlled by the backhole, so that the mixing efficiencies of swirl injectors are changed. Based on cold-flow tests, the swirl injector with the backhole may improve its performance.rformance.

Spray Characteristics of Fuel Injector in DI Diesel Engine (직접 분사식 디젤 기관 인젝터의 연료 분무 특성)

  • 이창식;김민규;전원식;진다시앙
    • Transactions of the Korean Society of Automotive Engineers
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    • v.9 no.5
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    • pp.75-81
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    • 2001
  • This paper presents the atomization characteristics of single hole injector in the direct injection type diesel engine. The spray characteristics of fuel injector such as the droplet size and velocity were measured by phase Doppler particle analyzer. In this paper, the atomization characteristics of fuel spray are investigated for the experimental analysis of the measuring data by the results of mean diameter and mean velocity of droplet. The effect of fuel injection pressure on the droplet size shows that the higher injection pressure results in the decrease of mean droplet diameter in the fuel spray. The minimum size of fuel spray droplet appears on the location of 40mm axial distance from nozzle exit of diesel injector. Based on the experimental results, the correlation between the droplet diameter and mean velocity of the diesel spray due to the change of axial and radial distance from the nozzle tip were investigated.

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Spray Characteristics of High-Pressure Injector in Direct-Injection Gasoline Engine (직분식 가솔린 기관 고압 인젝터의 연료 무화 특성)

  • 이창식;최수천;김민규
    • Transactions of the Korean Society of Automotive Engineers
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    • v.7 no.8
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    • pp.1-6
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    • 1999
  • An experimental study was carried out to investigate the global spray behavior and spray characteristics of high-pressure fuel injector in the direct-injection goasoline enginet. The atomization characteristics of fuel spary such as mean droplet size, mean velocity , and velocity distribution were measured by the phase Doppler particle analyzer. The spray tip penetration and spray width were investigated by the result fo visualizaiton experiment. The quantitiative spary characteristics of injector spray were measured under various sparay conditions and ambient pressures. The results of experiment show that the increase in ambient pressure have influence on the spray tip penetration and spray development process. Also, the influence of injection pressure and measuring location on the mean velocity and droplet size distribution were discussed.

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Effects of Backhole on Hyraulics of Liquid Rocket Swirl Coaxial Injector (액체로켓 동축형 스월인젝터에서 Backhole에 의한 수력학적 영향)

  • Hwang Seong-Ha;Seol Jaehoon;Jeong Wonho;Han Poongkyu;Yoon Youngbin
    • Proceedings of the KSME Conference
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    • 2002.08a
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    • pp.287-290
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    • 2002
  • 'Backhole' is an extra empty volume where is located behind the tangential entries at the rear par of the vortex chamber in the swirl coaxial injector. With the backhole, there are three major hydraulic characteristics. First, mass flow rate is increased about $15{\%}$ compared with the case without the backhole. Second, with the backhole, the center region of the injected flow has more large volume than that of without the backhole. The last, some range of the cone angle can be controlled by the backhole Experiments are conducted by using a PDPA apparatus, a mechanical patternator, stroboscopic photography and etc. With the backhole, based on cold-flow tests, the model swirl injector has some Improvement in its performance.

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The Effects of Signal Attenuation on Spray Characterization Using Planar Imaging Technique (평면 이미지 기법을 이용한 분무 특성 해석 시 신호 감쇠의 영향)

  • Jeun Jayoung;Kim Dongjun;Koh Hyeonseok;Yoon Youngbin;Koo Ja Ye
    • Proceedings of the KSME Conference
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    • 2002.08a
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    • pp.295-298
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    • 2002
  • In the analysis of the mass distribution and SMD (Sauter Mean Diameter), planar laser imaging technique Is a convenient and useful one when compared to the mechanical patternator or PDPA (Phase Doppler Particle Analyzer). But for the accurate usage of this laser technique, it is required to compensate the signal attenuation and to find the attenuation coefficients. In the present research, we considered effects of the spray distributions on the attenuation coefficient and improved the accuracy of planar laser imaging technique by the reduction of errors issuing from the signal attenuation.

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ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF THE MAIN WING SECTION OF KC-100 AIRCRAFT (KC-100 항공기 주날개의 결빙에 의한 공력 영향성 연구)

  • Lee, C.H.;Sin, S.M.;Jung, S.K.;Myong, R.S.;Cho, T.H.;Jung, J.H.;Jeong, H.H.
    • 한국전산유체공학회:학술대회논문집
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    • 2010.05a
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    • pp.464-467
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    • 2010
  • Ice accretion on aircraft surface in icing condition induces external shape changes that may result in a hazard factor for aircraft safety. In case of aircraft main wing with high lift equipment, ice accretion is observed around leading edge and flap. During the design phase, location of ice accretion and associated aerodynamic characteristics must be investigated. In this study, icing effects on aerodynamic characteristics of the main wing section of KC-100 aircraft are investigated using an Eulerian-based FENSAP-ICE code in various icing conditions.

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An Experimental Study of Discharge Coefficient with Non-Circular Effervescent Type Twin-fluid Nozzle (비원형 Effervescent Type 이유체노즐의 Discharge Coefficient에 관한 실험적 연구)

  • Lee, Sang Ji;Park, Hyung Sun;Hong, Jung Goo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.682-685
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    • 2017
  • An experimental study was carried out to investigate the injection characteristics of non-circular effervescent type twin-fluid nozzles. For this purpose, two types of non-circular nozzles (E1, E2) and one kind of circular nozzle (C) were used. At this time, the Aerorator mounted on the nozzle used three different diameters to match the aspect ratio with the nozzle exit area. Therefore, experiments were performed according to three aspect ratios for each nozzle, and a total experiments were conducted. Experiments were carried out by controlling the amount of air flowing after fixing the flow rate of the liquid, and the nozzle internal pressure and SMD were measured, and the jet image was taken from the nozzle. The discharge coefficients of the three kinds of nozzles were compared with the conventional equation and the Jedelsky's equation, and the Jedelsky's equation was found to be about 4 times larger. The droplet size (SMD) injected from the nozzle was found to be smaller in the non-circular shape than in the circular shape, which is expected to be caused by the difference of the discharge coefficient values.

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The Spray Characterization Using Planar Imaging Technique (평면 이미지 기법을 이용한 분무 특성 해석)

  • Lee, Kyung-Jin;Jung, Ki-Hoon;Yoon, Young-Bin;Jeong, Kyung-Seok;Jeung, In-Seuck
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.24 no.1
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    • pp.93-101
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    • 2000
  • The characteristics of spray nozzle have been quantified with the measurement of fluorescence and Mie scattering images. To correct the attenuation of the incident light sheet, a sequential double-pass light sheet system and the geometrical averaging of two images was implemented. Quantitative mass flux distribution of spray was obtained from fluorescence image. 3-D image is reconstructed using 2-D radial images. Sauter mean diameter (SMD) distribution was determined using the ratio of fluorescence signal intensity and Mie scattering signal intensity and the values were quantified with PDP A data. The measurement of mass flux and SMD using planar imaging technique agee with PDP A data fairly well in the low density region. However, in dense region, there are significant errors caused by secondary scattering. It was found that the planar imaging technique provides many advantages over the point measurement technique, such as PDP A, and can be implemented for quantitative measurement, especially in low density region.