• 제목/요약/키워드: liquid drop size

검색결과 132건 처리시간 0.032초

Experimental Studies on Self-Oscillation of a Swirl Coaxial Injector

  • Kim, Dongjun;Wonho Jeong;Jihyuk Im;Youngbin Yoon
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.228-233
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    • 2004
  • The spray and acoustic characteristics by the self-oscillation of a swirl coaxial injector were experimentally studied. The self-oscillation of a swirl coaxial injector is defined as pressure and flowrate oscillations by a time-delayed feedback between liquid and gas phase and has strong influences on atomization and mixing processes. Hence the occurrence and effect of the self-oscillation are measured using shadow photography technique, acoustic test and PDPA. The occurrence of self-oscillation largely depends on the injection conditions, such as pressure drop of liquid phase and relative momentum ratio. From the experimental results, self-oscillation occurs when the momentum of gas phase is enough large and the smaller the pressure drop of liquid phase is, the better self-oscillation occurs at the same momentum ratio. The self-oscillation is also affected by injector geometries, increasing the recess length results in the expansion of self-oscillation region and the increase of sound pressure level. The self-oscillation of a swirl coaxial injector accompanies a high intensity scream and this scream may provide harmful disturbances to combustion processes. Self-oscillation leads to strong changes in the drop size distribution and smoothly varies the slope of radial SMD distribution.

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소형 로켓 엔진 연소의 성능 예측 및 실험결과 평가 (Performance Prediction of Smal I Rocket Engine Combustion And Estimation of Experimental Results)

  • 박정;김용욱;김영한;정용갑;조남경;오승협
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 1999년도 제19회 KOSCO SYMPOSIUM 논문집
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    • pp.209-217
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    • 1999
  • A model for depicting the rocket engine combustion process is presented and basic experiments near a design point are provided with a FOOF type of unlike impinging injector for RP-I fuel and liquid-oxygen. The model is based on the assumption that the vaporization is the rate-controlling combustion process. The effects of initial drop size and initial drop velocity are systematically shown and discussed. It is seen that in the midst of considered parameters the change of initial drop size is more sensitive to the performance. The proposed model describes qualitative trends of combustion process well despite of its simplicity.

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Y-Jet 노즐에서의 혼합관 길이변화에 따른 분무특성 연구 (Change of Spray Characteristics with Mixing Port Length of Y-Jet Atomizers)

  • 송시홍;이상용
    • 대한기계학회논문집
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    • 제18권11호
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    • pp.3021-3031
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    • 1994
  • Experiments have been performed to find out the effect of the mixing port length of Y-jet atomizers on the spray performance, using air and water as the test fluids. Water and air flow rates and drop sizes were measured at each injection pressure condition for different mixing port length. The air flow rate was almost unaffected by the change of the mixing port length. However, the water flow rate was relatively susceptible to the change of the mixing port length. The mixing point pressure was very much influenced by the mixing port length. Variations of spatial distribution of Sauter Mean Diameter (SMD, $D_{32}$) and the cross-section-averaged SMD ($D_{32,m}$) with different mixing port length and air/water mass flow rate ratio were examined. Generally, when the mixing port length was reduced, the mean drop size decreased and became spatially even.

로켓 엔진의 연소 성능 예측 및 시험 (Performance Prediction of Rocket Engine Combustion and Estimation of Experimental Results)

  • 박정;김용욱;김영한;정용갑;조남경;오승협
    • 대한기계학회논문집B
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    • 제24권5호
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    • pp.718-724
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    • 2000
  • A model for depicting the rocket engine combustion process is presented and several experiments near a design point are provided with a FOOF type of unlike impinging injector for a propellant combination of Jet A-1 fuel and liquid-oxygen. The model is based on the assumption that the vaporization is the rate-controlling combustion process. The effects of initial drop size and initial drop velocity are systematically shown and discussed. It is seen that in the midst of considered parameters the change of initial drop size is more sensitive to the performance. The proposed model describes qualitative trends of combustion process well despite of its simplicity.

Experimental Investigation of Electrostatic Dripping and Atomization Mode through Non-MEMs based Nozzle Design

  • Choi, Kyung-Hyun;Dang, Hyun-Woo;Rehmani, M.A. Ali
    • 한국재료학회:학술대회논문집
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    • 한국재료학회 2009년도 춘계학술발표대회
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    • pp.13.2-13.2
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    • 2009
  • Electrostatic printing either it is drop-on-demand or continuous has immense applications in non-contact printing systems such as solar cells, flexible printed circuits, RFIDs and bio applications. In this paper a laboratory manufactured nozzle has been designed for the experimental investigation of electrostatic dripping and atomization of liquid. Dripping and atomization conditions such as voltage, nozzle tip diameter, distance between counter electrode and flowrate has been indentified for the designed nozzle. Furthermore it is also demonstrated that the diameter of a generated droplet could be reduced from a significantly large size to a narrow size distribution which can be controlled by volumetric flow rate and applied voltage. This study will help in classify the conditions between different electrostatic dripping mode such as drop-on-demand formation, jet mode and finally the atomization mode based on the laboratory fabricated nozzle head.

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

  • 김민기;송진관;김진기;윤영빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제27회 추계학술대회논문집
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    • pp.59-63
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    • 2006
  • 횡단류 아음속유동장에서 연료의 수직 분사시 나타나는 액적영역의 액적들을 직접사진촬영으로 측정하고 PLLIF 실험을 통하여 얻은 강도 값으로 SMD분포를 측정하였다. 본 연구의 목적은 정상유동에서의 액적들의 크기 및 분포를 관찰하고, 캐비테이션 및 수력튀김 현상에 대한 액적들의 차이를 확인하는 것이다. 실험을 통하여 정상유동의 액적들은 분사차압, 공기의 유속, 침투거리, 인젝터 지름에 대한 하류방향 거리비(x/d)에 의하여 결정되며, 캐비테이션에 의한 난류강도, 유효지름에 따라 차이가 있음을 확인하였다.

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소형 액체로켓엔진 인젝터 분무의 연료분사압력 변이에 따른 액적의 공간분포 특성 (Spatial Distribution Characteristics of Small LRE-injector's Spray-droplet According to the Variation of Fuel-injection Pressure)

  • 정훈;김정수
    • 한국추진공학회지
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    • 제12권5호
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    • pp.1-8
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    • 2008
  • 소형 액체로켓엔진 인젝터 분무의 공간분포 특성 규명을 위해 이중모드 위상도플러속도계(DPDA)를 이용한다. 분사압력 및 분무확산방향 이동거리를 변화시켜 분무액적의 크기, 속도 등을 측정하고, 산술평균직경(AMD), Sauter 평균직경(SMD), 수밀도, 스팬(span of drop size distribution), 그리고 체적 유속(volume flux) 등의 분무 매개변수를 도출하여 인젝터 분무의 분열특성을 고찰한다. 분사압력이 증가함에 따라 분무액적의 수밀도, 스팬, 그리고 체적 유속은 증가하지만, AMD는 감소하였다.

Atomization Characteristics of a Double Impinging F-0-0-F Type Injector with Four Streams for Liquid Rockets

  • Kang, Shin-Jae;Rho, Byung-Joon;Oh, Je-Ha;Kwon, Ki-Chul
    • Journal of Mechanical Science and Technology
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    • 제14권4호
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    • pp.466-476
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    • 2000
  • This paper presents atomization characteristics of a double impinging F -0-0- F type injector with four streams. A phase Doppler particle analyzer was employed to measure the droplet-size and water was used as the inert simulant liquid instead of reactive propellant liquids. The droplet mean diameter (SMD) and size distribution were measured to investigate the effects of the momentum ratio and pressure drop variations. This experimental results can be used during the preliminary design stage of a impinging stream type injector for liquid rockets.

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SELF-PULSATION CHARACTERISTICS OF A SWIRL COAXIAL INJECTOR WITH VARIOUS INJECTION AND GEOMETRIC CONDITIONS

  • Im, Ji-Hyuk;Kim, Dong-Jun;Yoon, Young-Bin;Bazarov, V.
    • 한국분무공학회지
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    • 제10권3호
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    • pp.29-37
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    • 2005
  • The spray and acoustic characteristics of a gas/liquid swirl coaxial injector are studied experimentally. The self-pulsation is defined as a pressure and flow rate oscillations by a time-delayed feedback between liquid and gas phase. Self-pulsation has strong influences on atomization and mixing processes and accompanies painful screams. So. the spray and acoustic characteristics are investigated. Spray patterns are observed by shadow photography technique in order to determine the onset of self-pulsation. And self-pulsation boundary with Injection conditions and recess length is get. To measure the frequency of the spray oscillation. oscillation of the laser intensity which passes through spray is analyzed by Fast Fourier Transform. For acoustic tests, a PULSE System was used. Acoustic characteristics of a swirl coaxial injector are investigated according to the injection conditions. such as the pressure drop or the liquid and gas phase. and injector geometries. such as recess length and gap size between the inner and outer injector. Front the experimental results. the increase of recess length leads to the rapid increase of the sound pressure level. And as the pressure drop of the liquid phase increases. the frequency of the self?pulsation shifts to the higher frequency. The frequency of spray oscillations is the same as that of the acoustic fields by self-pulsation.

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핀치이론의 수정 모델을 이용한 스프레이 모드의 해석 (Analysis of Spray Mode Using Modified Pinch Instability Theory)

  • 박아영;;김선락;유중돈
    • Journal of Welding and Joining
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    • 제27권5호
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    • pp.88-93
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    • 2009
  • While the pinch instability theory (PIT) has been widely employed to analyze the spray transfer mode in the gas metal arc welding (GMAW), it cannot predict the detaching drop size accurately. The PIT is modified in this work to increase the accuracy of prediction and to simulate the molten tip geometry to be more physically acceptable. Since the molten tip becomes a cone shape in the spray mode, the effective wire diameter is formulated that the effective diameter is inversely proportional to current square. Modifications are also made to consider the finite length of the liquid column and current leakage through the arc. While the effective diameter influences drop transfer significantly, the current leakage has negligible effects. The effects of modifications on drop transfer are analyzed, and the predicted drop diameters show good agreements with the experimental data of the steel wire.